Hobart 60CU20 Operation And Maintenance Manual With Illustrated Parts List

Page 1
OM-2226
ITW GSE Group
U.S.A.
05/02/2013 – Original
Operation and Maintenance Manual
Illustrated Parts List
for
60CU20
60 kVA, 3 Phase, 115/200 Volt,
400 Hz. Generator Set
Series 500062
Hobart Ground Systems Palmetto, Florida 34221
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Page 3
Warranty
PALMETTO, FL 34221
Data Sheet 165
Index: 990223
WARNING: AT ALL TIMES, SAFETY MUST BE CONSIDERED AN IMPORTANT FACTOR IN THE
QUALIFIED PERSO NNEL SHOULD ALWAYS BE EMPLOYED FOR SU CH TASKS.
HOBART GROUND POWER
1. Hobart Brothers Company (hereinafter called HOBART) warrants that each new and unused Hobart Ground Power
Equipment, (hereinafter called the PRODUCT) is of good workmanship and is free from mechanical defects, provided that (1) the PRODUCT is installed and operated in acco rdance with the printed instructions of HOBART, (2) the PRODUCT is used under the normal operating conditions for which it is designed, (3) the PRODUCT is not subjected to misuse, negligence or accident, and (4) the PRODUCT receives proper care, lubrication, protection, and mainte nance under the supervision of trained perso nnel.
2. This warranty expires 15 months after ship ment by HOBA RT to the first user, o r 12 months after installation,
whichever first occurs.
3. This warranty does not apply to: primary and secondary switch contacts, cable connectors, carbon brushes, fuses,
bulbs, and filters unless found to be defective prior to use.
4. Hobart DOES NOT WARRANT THE FOLLOWING COMPONENTS: Engines, engine components; such as:
starters, alternators, regulators, governors, etc., and cable retrieving devices. Many of the foregoing components are warranted directly by the manufacturer to the first user and serviced by a worldwide network of distributors and others authorized to handle claims for component manufacturers. A first user’s claim should be presented directly to such an authorized component service outlet. In the event any component manufacturer has warranted its component to HOBART and will not dea l directly with a first user then HOBART will cooperate with the first user in the presentation of a claim to such manufacturer. Under NO circumstances does HOBART assume any liability for any warranty claim against or warranty work done by or in behalf of any manufacturer of the foregoing components.
5. This warranty is extended by HOBART only to the purchaser of new PRODUCTS from HOBART or one of its
authorized distributors. The PRODUCTS purchased under this warranty are intended for use exclusively by the buyer and his employees and by no other persons and, therefore, there shall be no third party beneficiary to this warranty.
6. A claim of defects in any PRODUCT covered by this warranty is subject to HOBART factory inspection and
judgment. HOBA RT’S liability is limited to rep a ir of any de fects found by HOBART to exist, or at H O BART’S option the replacement of the defective product, F.O.B. factory, after the defective product has been returned by the purchaser at its expense to HOBART’S shipping place. Replacement and exchange parts will be warranted for the remainder of the original Warranty, or for a period of ninety (90) days, whichever is greater.
7. UNDER NO CIRCUMSTANCES whatsoever shall HOBART and its authoriz e d distributors be liable for any
special or consequential damages, whether based on lost goodwill, lost resale profits, work stoppage impairment of other goods or otherwise, and whether arising out of breach of any express or implied warranty, breach of contract, negligence or otherwise, except only in the case of personal injury as may be required by applicable law.
8. Continued use of the PRODUCT(S) after discovery of a defect VOIDS ALL WARRANTIES.
9. Except as authorized i n writing, t his warranty does not cover any equipment that has been altered by any party
other than H OBART.
10. THERE ARE NO WARRANTIES WHICH EXTEND BEYOND THE DESCRIPTION ON THE FACE HERE
OF. HOBART MAKES NO WARRANTIES, EXPRESSED OR IMPLIED, OF MERCH ANT ABILITY OR FITNESS FOR A PARTICULAR PURPOSE.
11. HOBART neither assumes nor authorizes any person to assume for HOBART any liability in connection with the
PRODUCTS sold, and there are no oral agreements or warranties collateral to or affecting this written Warranty. This warranty and all undertakings of HOBART thereunder shall be governed by the laws of the State of Ohio, United States of America.
Replaces: 980601
INSTALLATION, SERVICING AND OPERATION OF THE PRODUCT, AND SKILLED, TECHNICALLY
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Revision Log
Page 1
Record of Change
Rev.
No.
Release Date
By
Description
0
May 2, 2013
MLJ
This is a spec roll from OM-2175A (500061A) for release of STD and DLX configurations.
Note: the 60 kVA is similar to the 90 kVA with the following differences:
Air cleaner and related air intake components
AC Ammeter (different ranges)
ID Resistor (different Power Module Panel assembly)
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Safety War nings
Page 1
Safety Warnings and Cautions
ELECTRIC SHOCK can KILL. Do not touch li ve electr ic al parts .
attached equipment.
WARNING
ELECTRIC ARC FLASH can injure eyes, burn skin, cause equipment damage, and
ignite combustible material. DO NOT use power cables to break load and prevent tools from causing short circuits.
IMPROPER PHASE CONNECTION, PARALLELING, OR USE can damage this and
IMPORTANT
WARNING
Protect all operating personnel. Read, understand, and follow all instructions in the Operating/Instruction Manual before installing, operating, or servicing the equipment. Keep the manual available for future use by all operators.
CALIFORNIA PROPOSITION 65 - DIESEL ENGI N ES . Diesel engine exhaust and some of its constituents are known to the State of California to cause cancer, birth defects and other reproductive harm.
1) General
Equipment that supplies electrical power can cause serious injury or death, damage to other equipment or property. The operator must strictly observe all safety rules and take precautionary actions. Safe practices have been developed from past experience in the use of power source equipment. While certain practices below apply only to electrically powered equipment, other practices apply to engine-driven equipment, and some practices to both.
2) Shock Prevention
Bare conductors, terminals in the output circuit, or ungrounded, electrically live equipment can fatally shock a person. Have a certified electrician verify that the equipment is adequately grounded and learn what terminals and parts are electrically HOT. Avoid hot spots on machine. Use proper safety clothing, procedures, and test equipment.
The electrical resistance of the body is decreased when wet, permitting dangerous currents to flow through it. When inspecting or servicing the equipment, do not work in damp areas. Stand on a dry rubber mat or dry wood, and use insulating gloves when dampness or sweat cannot be avoided. Keep clothing dry, and never work alone.
a) Installation and Grounding of Electrica lly Powered Equipment
This equipment must be installed and m aintai ned in ac cor danc e with the Nat ion al Electrical Code, ANSI/NFPA 70, or other applicable codes. A power disconnect switch or circuit breaker must be located at the equipment. Check the nameplate for voltage, frequency, and phase requirements. If only 3-phase power is available, connect any single-phase rated equipment to only two wires of the 3­phase line. DO NOT CONNECT the equipment grounding conductor (lead) to the third live wire of the 3-phase line, as this makes the equipment frame electrically HOT, which can cause a fatal shock.
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Safety War nings
Page 2
Always connect the grounding lead, if supplied in a power line cable, to the grounded switch box or building ground. If not provided, use a separate grounding lead. Ensure that the current (amperage) capacity of the grounding lead will be adequate for the worst fault current situation. Refer to the National Electrical Code ANSI/NFPA 70 for details. Do not remove plug ground prongs and use correctly mating receptacles.
b) Output Cables and Terminals
Inspect cables frequently for damage to the insulation and the connectors. Replace or repair cracked or worn cables immediately. Do not overload cables. Do not touch output terminal while equipment is energized.
3) Service and Maintenance
This equipment must be maintained in good electrical condition to avoid hazards stemming from disrepair. Report any equipment defect or safety hazard to the supervisor and discontinue use of the equipment until its safety has been assured. Repairs should be made by qualified personnel only. Before inspecting or servicing this equipment, take the following precautions:
a) Shut off all power at the disconnecting switch, or line breaker, or by disconnecting battery, before
inspecting or servicing the equipment.
b) Lock switch OPEN (or remove line fuses) so that power cannot be turned on accidentally. c) Disconnect power to equipment if it is out of service. d) If troubleshooting must be done with the unit energized, have another person present who is trained
in turning off the equipment and providing or calling for first aid.
4) Fire And Explosion Prevention
Fire and explosion are caused by electrical short circuits, combustible material near engine exhaust pipes, misuse of batteries and fuel, or unsafe operating or fueling conditions.
a) Electrical Short Circuits and Overlo ads
Overloaded or shorted equipment can become hot enough to cause fires by self-destruction or by causing nearby combustibles to ignite. For electrically powered equipment, provide primary input protection to remove short circuited or heavily overloaded equipment from the line.
b) Batteries
Batteries may explode and/or give off flammable hydrogen gas. Acid and arcing from a ruptured battery can cause fires and additional failures. When servicing, do not smoke, cause sparking, or use open flame near the battery.
c) Engine Fuel
Use only approved fuel container or fueling system. Fires and explosions can occur if the fuel tank is not grounded prior to or during fuel transfer. Shut unit DOWN before opening fuel tank cap. DO NOT completely fill tank, because heat from the equipment may cause fuel expansion overflow. Remove all spilled fuel IMMEDIATELY, including any that penetrates the unit. After clean-up, open equipment doors and blow fumes away with compressed air.
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Safety War nings
Page 3
EMERGENCY
FIRST AID
5) Toxic Fume Prevention
Carbon monoxide - Engine exhaust fumes can kill and cause health problems. Pipe or vent the exhaust fumes to a suitable exhaust duct or outdoors. Never locate engine exhausts near intake ducts of air conditioners.
6) Bodily Injury Prevention
Serious injury can result from contact with fans or hot spots inside some equipment. Shut DOWN such equipment for inspection and routine maintenance. When equipment is in operation, use extreme care in doing necessary troubleshooting and adjustment. Do not remove guards while equipment is operating.
7) Medical and First Aid Treatment
First aid facilities and a qualified first aid person should be available for each shift for immediate treatment of all injury vict ims. Electric shock victims should be checked by a physician and taken to a hospital immediately if any abnormal signs are observed.
Call physician immediately. Seek additional assistance. Use First Aid techniques recommended by American Red Cross until medical help arrives.
IF BREATHING IS DIFFICULT, give oxygen, if available, and have victim lie down. FOR ELECTRICAL SHOCK, turn off power. Remove victim; if not breathing, begin
artificial respiration, preferably mouth-to-mouth. If no detectable pulse, begin external heart massage. CALL EMERGENCY RESCUE SQUAD IMMEDIATELY.
8) Equipment Precautionary Labels
Inspect all precautionary labels on the equipment monthly. Order and replace all labels that cannot be easily read.
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Safety War nings
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Table of Contents
Page 1
Chapter 1
Description/Operation
Chapter-Section/Page#
Section 1
Description
1-1/1
General
1-1/1
Optional Equipment - Appendix A
1-1/1
Orientation
1-1/1
Specifications
1-1/3
Special Features
1-1/5
Canopy
1-1/5
Engine and Generator
1-1/5
Control Box Assembly
1-1/11
Power Module Panel Assembly
1-1/22
Cold Weather Start System
1-1/24
Transformer-Rectifier (T-R) Assembly
1-1/25
Section 2
Preparation for Use, Storage or Shi p p ing
1-2/1
Preparation For Use
1-2/1
Preparation for Storage
1-2/5
Preparation for Shipment
1-2/6
Section 3
Operation
1-3/1
General
1-3/1
400 Hz. Operation Procedure
1-3/1
DC Operation Procedure
1-3/6
Simultaneous AC and DC Operation
1-3/6
Chapter 2
Servicing / Troubleshooting
Chapter-Section/Page#
Section 1
Maintenance Inspection/Check
2-1/1
General
2-1/1
Maintenance Schedule
2-1/1
Inspection / Check
2-1/3
Table of Contents
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Table of Contents
Page 2
Section 2
Maintenance Procedures
2-2/1
General
2-2/1
Servicing the Air Cleaner
2-2/6
Engine Fuel
2-2/7
Engine Cooling System
2-2/11
Drive Belt
2-2/14
Section 3
Adjustments / Tests
2-3/1
Testing the 400 Hz. Generator Set
2-3/1
Generator Set Adjustments
2-3/12
Diode Test
2-3/16
Testing the Transformer-Rectifier
2-3/16
Section 4
Troubleshooting Procedures
Equipment for Troubleshooting
2-4/1
Parts Replacement
2-4/1
Check Connections and Leads
2-4/2
Engine Troubleshooting
2-4/2
Connection and Schematic Diagr ams
2-4/2
GPU Control Monitoring
2-4/3
…Engine Controls
2-4/10
…Generator Excitation Circuits
2-4/13
…Protective Circuit
2-4/16
…Generator
2-4/18
Troubleshooting Tables – GPU Commands
2-4/21
Troubleshooting Tables – GPU Faults
2-4/22
Engine Lubrication
Engine Fuel System
Generator Maintenance
General
Generator and Exciter Test
Adjusting the Transformer-Rectifier
General
2-2/2
2-2/8
2-2/14
2-3/1
2-3/15
2-3/18
2-4/1
Normal Operation
Illustrations
2-4/2
2-4/2
Troubleshooting Charts 2-4/10
…Load Contactor Operating Circuits
…T-R Controls and Components
2-4/14
2-4/19
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Table of Contents
Page 3
Chapter 3
Overhaul / Major Repair
Chapter-Section/Page#
Section 1
Exciter Armature
3-1/1
General
3-1/1
Exciter Armature
3-1/2
Exciter Armature Replacement
3-1/3
Exciter Armature Installation
3-1/6
Section 2
Dual Bearing Flexible Coupling
General
3-2/1
Disassembly
3-2/1
Coupling Service
3-2/4
Coupling Installation
3-2/5
Reassemble Engine and Generator
3-2/6
Run-in and Periodic Check
3-2/7
Section 3
Generator Assembly
General
3-3/1
Generator Assembly Removal
3-3/1
Generator Assembly Installation
3-3/2
Chapter 4
Illustrated Parts List
Chapter-Section/Page#
Section 1
Introduction
4-1/1
General
4-1/1
Purpose
4-1/1
Arrangement
4-1/1
Explanation of Parts List
4-1/1
Section 2
Manufacture's Codes
4-2/1
Explanation of Manufacture's (Vendor) Code List
4-2/1
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Table of Contents
Page 4
Section 3
Illustrated Parts List
4-3/1
Explanation of Parts List Arrangement
4-3/1
Figure 1: General Assembly
4-3/2
Figure 2:Trailer / Frame Assembly
4-3/4
Figure 4: Canopy Assembly
4-3/8
Figure 5: Internal Components
4-3/10
Figure 7: Control Box Interior Components
4-3/14
Figure 8: Control Switch Panel Components
4-3/16
Figure 10: Engine Cooling System As s emb ly
4-3/20
Figure 11: Engine Ground Plate and Battery Disconnect Switch
4-3/22
Figure 13: Engine Exhaust Compone nts
4-3/26
Figure 14: 12 VDC Battery System
4-3/28
Figure 16: Engine Components
4-3/32
Figure 17: Engine Electrical Panel Com pon ents
4-3/34
Figure 19: Transformer-Rectifier Assembly – Part 1
4-3/38
Figure 20: Transformer-Rectifier Assembly – Part 2
4-3/40
Section 4 Numerical Index
4-4/1
Explanation of Numerical Index
4-4/1
Chapter 5
Manufacture's Literature
Appendix A Options/Features
Wet Stacking
Unusual Service Conditions
Symbols and Abbreviations
Figure 3: Canopy Frame Assembly
Figure 6: Control Box and Door Assembly
Figure 9: 400 Hz. Power Module Assembly
Figure 12: Engine Fuel Filter and Fuel Lines
Figure 15: Engine Air Intake Assembly
Figure 18: Generator Assembly
4-3/1
4-3/6
4-3/12
4-3/18
4-3/24
4-3/30
4-3/36
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Introduction
Page 1
Introduction
This manual contains operation and maintenance information for a diesel engine-generator manufactured by Hobart Ground Systems, Palmetto, Florida 34221.
This manual, including all informa tion contained thereon, is exclusive and confidential property of Hobart Ground Systems. This manual is not to be copied, reproduced, or delivered or disclosed to others, in whole or in part, except with e xpress written permission of Hobart Ground Systems.
This manual is not intended to be a textbook on electricity or electronics. Its primary purpose is to provide information and instructions to experienced operators, electricians, and mechanics that have never operated this equipment. It is the intent of this manual to guide and assist operators and maintenance personnel in the proper use and care of the equipment.
Use of the manual should not be put off until trouble or a need for help develops. Read the instructions before starting the unit. Learn to use the manual and to locate information contained in it. Its style and arrangement are very similar to commercial aircraft manuals.
The manual is divided into five chapters plus an appendix. Each chapter is divided into as many sections as required. Each new section starts with page 1. Each page is identified by chapter, section and page number, which are located in the lower, outside corner.
When information located in another portion of the manual is referred to, a chapter, section, and paragraph or figure number identify its location. For example: “(see Section 2-3, Paragraph 1.a.)” refers to information located in Chapter 2, Section 3, Paragraph 1.a. If a chapter and section are not indicated in a reference, the referenced material is located in the same section as the reference, for example: “(see Paragraph 1.a.).”
The appendix is the last section. It contains a list of available options that may be purchased or have been purchased with that unit. Items on the list with check marks next to them have been added to the standard unit per the customer’s order. Literature for each option follows. The appendix will help control the information in the manual making it unique to the unit purchased.
In addition to operation and maintenance instructions, the manual contains an illustrated parts list in Chapter 4 and a collection of manufacturer’s literature and supplemental information in Chapter 5.
Contents of the manual are arranged as follows:
Chapter 1 Description/Operation Chapter 2 Servicing/Troubleshooting Chapter 3 Overhaul/Major Repair Chapter 4 Illustrated Parts List Chapter 5 Manufacturer’s Litera tu re Appendix A Options
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Introduction
Page 2
If you have any questions concerning your Hobart Ground Power equipment, immediately contact our Service Department by mail, telephone, FAX, or E-Mail.
Write: Hobart Ground Systems Service Department 11001 US Highway 41, North Palmetto, FL 34221 U.S.A.
Call Inside U.S.A.: (800) 899-1841 (Parts) (877) 874-5322 (Service)
Call From Foreign Countries: (941) 721-1025 (Parts) (941) 721-1092 (Service)
FAX Inside U.S.A. (800) 367-4945 FAX From Foreign Countries: (937) 332-5121 E-Mail :
service@hobartsystems.com
Web Page :
www.hobartsystems.com
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 1
Chapter 1
Description/Operation
Section 1
Description
Part & Dash
Number
Fuel
Tank
Exhaust
Mounting
AC
Outputs
28.5 DC Output
500062-STD
Composite
Vertical
Trailer
Single
---
500062-DLX
Composite
Vertical
Trailer
Single
---
500062TR-STD
Composite
Vertical
Trailer
Single
Yes
500062TR-DLX
Composite
Vertical
Trailer
Single
Yes
1) General
The basic generator set covered in this manual, manufactured by ITW GSE Group, Hobart Ground Systems is rated at 60 kVA and is designed to produce and deliver 115/200-volt, 400 Hz, 3-phase AC power to a parked aircraft or other load. Some generator models with the TR option also provide 28.5 volts DC for aircraft having those requirements.
The number 500061 identifies the model or series of the GPU. The part number is followed by a different dash number that separates the basic units available. Figure 1 uses the part number to identify the variations covered in this manual.
Table 1: Series 500062 Generator Set Part Number Descriptions
2) Optional Equipment - Appendix A
Chapters 1 through 5 of this Operation and Maintenance Manual identify only the stripped down vers io n of the 60CU20 generator set. A list of optional equipment appears in Appendix A.
3) Orientation
For purpose of orientation when designating RIGHT and LEFT throughout this manual, the radiator is considered to be at the FRONT of the unit and the generator and controls are at the REAR. RIGHT and LEFT are determined by standing at the REAR facing the machine. As an example, the fuel filler neck is mounted on the LEFT REAR side of the unit.
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 2
11 2 3 4
1 5 6 7 9 9 10
12
13
14
8
1. Fuel Filler Neck
2. Operator’s Control Panel
3. Output Cable Trays
th
4. 5
Wheel Assembly
5. Rear Drop Axle Assembly
6. Emergency Stop Switch (S28)
7. Exhaust Stack Outlet
8. Engine Air Intake
9. Lift Off Access Doors
10. CAC/Radiator End
11. Generator End
12. Cable Rollers (optional)
13. Block Heater Receptacle (optional)
14. Forklift Pockets (optional)
Figure 1: General Assembly of Generator Set
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 3
Basic Unit (Fixed Mount)
Length
74 in. (1880 mm)
101 in. (2570 mm) w/ tow bar up
Width
67 in. (1702 mm)
67 in. (1702 mm)
Height
59 in. (1499 mm)
67 in. (1702 mm)
Weight
4000 lb. (1814 kg.)
4300 lb. (1950 kg.)
Weight with 28.5 VDC T-R
4300 lb. (1950 kg.)
4600 lb. (2087 kg.)
Output power rating
60 kVA (48 kW)
Output voltage
115 / 200 VAC
Rated load capacity
174 Amps
Frequency (at not load and rated load)
Power factor
0.8
Duty Cycl e
100%
Operating speed
2000 RPM
Overload capacity 125% rated load
218 Amps
Output cable size
2/0
Condition
Trip Point
Time Delay
Over voltage
126 volts
1-second
140 volts
160 milliseconds
180 volts
50 milliseconds
Under voltage
any voltage below 100 volts
7 seconds
Over frequency 420 Hz to 480 Hz
5 seconds
above 480 Hz
immediate
Under frequency
380 Hz. or less
7-seconds
Output overload
125% load of 60 kVA on either or both outputs
approximately 5 minutes 150% load
30 seconds
200% load
10 seconds
4) Specifications
a) Physical Specifications
Physical
b) AC Generator Specifications
With Trailer
400 Hz. ± 2 Hz.
c) AC Generator Protective System Speci fications
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 4
Output Power Rating
17.1 kW
Output Voltage
28.5 VDC
Load Capacity (Continuous)
600 A
Current Limiting Capability
100 to 2500 A
Condition
Trip Point
Time Delay
Over Voltage
32-34 VDC
2 seconds
2700 A
2 seconds
2000 A
10 seconds
1500 A
30 seconds
1200 A
90 seconds
750 A
600 seconds
Manufacturer and Model
Cummins Engine Company / QSB4.5
Type
4 cylinder, 4 cycle diesel, electronic controlled
Bore and Stroke
4.21 in. x 4.88 in. (107 mm x 124 mm)
Displacement
275 in3 (4.5 L)
Horsepower
109 hp (81 kW)
Idle speed
1000 ± 50 rpm
Normal governed speed
2000 rpm
Firing Order
1-3-4-2
Electrical system
12 VDC
Lubricating oil capacity (w/ filter)
11.6 quarts (11 liters)
Coolant capacity system
20 quarts (18.9 liters)
Engine oil pressure (warm and at rated speed 2000 RPM)
45 to 90 PSI (445 to 621 kPa).
Engine coolant temperature (normal operation)
160 to 200º F (71 to 93º C).
d) DC Output Specifications (with optional TR unit)
Peak/Starting Load Capacity 2000 A for 10 seconds Output cable size 4/0
e) DC Protective System Specifications
Output Overload
f) Engine Specifications
g) Normal Operating Characteristics
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 5
5) Special Features
The generator set has special features that are described more fully under the assemblies in which they appear.
a) Protective Monitoring
The protective monitoring system receives signals from the fault sensing components in the generator output circuit and functions to cause the load to be disconnected from the generator if an abnormal condition of voltage, frequency, or load develops.
b) Voltage Regulator
A microprocessor-type, adjustable voltage regulator provides automatic voltage regulation at the aircraft. The regulated out is also adjustable for a variety of output cable sizes and lengths.
c) Engine Electronic Control Module
The engine is equipped with an electronic control module that monitors, records, and controls engine performance.
d) Battery System Disconnect Switch
The generator set is equipped with a battery disconnect switch inside the unit on the LEFT side. The disconnect switch can be placed in the off position during long periods of shutdown.
6) Canopy
A sheet metal enclosure, identified as a canopy, provides protection for the engine, generator and electrical controls. The canopy is designed to reduce the operational noise level in the immediate area of the machine.
7) Engine and Generator
The engine and generator comprise the principal components of the generator set. They are mounted on a welded steel frame chassis. Some of the following figures are showing the locations of all major components and sub-assemblies.
a) Diesel Engine
The diesel engine is a fuel injection, 4-cylinder, electronically controlled engine rated at 155 horsepower. See Figure 3 for specifications and capabilities.
b) Engine Manufacturer’s Components
As received from the engine manufacturer, the engine includes some of the following components, which are more fully described in the engine manufacturer’s manual.
(1) Elec trical System
The 12 VDC electrical generating and starting system includes an alternator and starter with solenoid switch.
.
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OM-2226 / Operation and Maintenance Manual
60CU20 / Series 500062 / 400 Hz. Generator Set
May 2, 2013
Chapter 1-1
Page 6
manufacturer’s manual for approved fuels.
(2) Lubricity Additive Fuel Filter
The fuel filter is a spin-on disposable type located on the inside near the eng ine’s fuel pump. The fuel filter’s primary function, other than remove contaminants from the fuel, is to automatically add a lubricity additive to the fuel. Although, the engine manufacturer does not recommend low lubricity fuels, this additive can extend the life of the fuel pump.
CAUTION
The use of low lubricity fuels can shorten life and/or damage the engine’s fuel pump. Only diesel fuel is recommended by the engine manufacturer. Refer to engine
(3) Oil Filter
The engine oil filter is a spin-on, full-flow type, located on the right side of the engine near the front.
(4) Pre-programmed Electronic Control Module (ECM)
The ECM is a pre-programmed engine control module, mounted directly to the engine block.
c) Factory Installed Components and Protective Systems
This generator set is assembled at with the following components and protective s ystems: (1) Shutdown/Reset Systems
Emergency Shutdown / Reset Switch (S28) The emergency shutdown switch has two purposes. One is to reset the starting circuit
following a failed starting sequence. The other is to provide instant manual shut off of the generator set by disconnecting power to the ECM through the control box. It is located on the rear of the generator set under the control box.
To operate the EMERGENCY SHUTDOWN/RESET SWITCH:
Push button in until engine stops or until button travel stops
Pull the button back out to reset
Coolant high temperature shutdown system
The coolant temperature shutdown system consists of a factory supplied temperature switch. This switch is monitored by the microprocessor on the EIB (Engine Interface Board) PC Board, which will stop the engine if the temperature reaches 210º F (99º C).
Low coolant shutdown system The low coolant shutdown system consists of an engine manufactured supplied switch.
This switch is mounted in the radiator top tank and monitored by the engine’s ECM, which will stop the engine when a low coolant level is reached.
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Air Restriction
Oil pressure shutdown system
The oil pressure shutdown system consists of a factory supplied oil pressures switch. This switch is monitored by the microprocessor on the EIB (Engine Interface Board) PC Board, which will stop the engine if the oil pressure is under 12 PSI (82.7 kPA).
Low fuel shutdown system
The low fuel shutdown system monitors the fuel level in the fuel tank. When the fuel tank level reaches approximately
1
/4 tank the word fuel is displayed on the fault code gauge signifying that it is time to put fuel in the tank. Once the fuel level reach approximately the engine will shutdown.
(2) Radiator and Char g e-Air-Cooler (CAC)
The radiator and charge-air-cooler is a two-piece type designed for long periods of operation without servicing. Refer to Section 2-1 for servicing procedure.
(3) Engine-cooling fan
The engine fan is designed to blow air outward through the radiator, rather than pulling the air inward as a conventional fan does.
(4) Master [Battery] Disconnect Switch (MD1)
The master disconnect switch is designed to isolate the batteries from the entire electrical system to eliminate the possibility of battery current draw by the engine ECM or any other components between long periods of no operation. The switch can also be used to prevent starting of the equipment for maintenance conditions.
(5) Air cleaner
1
/8 tank
Indicator
Figure 2: Air Cleaner
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Engine Fault Condition
Over temperature or
Shuts down the engine, and appropriate fault code.
a) Press the engine stop button to reset the b) Or use E-STOP button for immediate reset.
Low fuel warning and
Turns on the low fuel
shutdown at 1/8 tank.
a) The low fuel fault indicating
b) Or use E-STOP button for immediate reset.
Clogged air cleaner
inlet.
Turns on the air cleaner
a) Press the engine stop button. The
b)
The diesel engine air cleaner is so constructed that air enters through its cylindrical body, and then is filtered before being passed into the engine turbo-charger assembly. An air cleaner service indicator device is mounted on the air cleaner assembly to monitor the airflow into the air cleaner. As the air cleaner becomes filled with dust, dirt, and carbon, the intake system airflow becomes increasingly restricted. This restriction causes a diaphragm inside the indicator to move toward an electrical contact. When the maximum allowable restriction level is reached, the circuit closes and the air cleaner indicator fault appears on the control panel fault display to warn the operator that the air cleaner must be changed. The electrical indicator automatically resets when the restriction level drops sufficiently.
d) Engine faults
The following is a table listing faults, which may occasionally occur. Column two of the table explains what happens in the engine’s circuitry when the fault occurs, and column three tells how to return the generator set to service once the problem is solved. Refer to Chapter 2 for more details on all other faults.
What Occurs How To Reset
ENGINE FAULTS
low oil pressure
shutdown
or other restriction in the combustion air
e) Generator
exciter AC output to DC for excitation of the generator revolving fields. The exciter DC output to the generator fields, and consequently the generator output, is controlled by the voltage regulator PC board (REG). A centrifugal, radial-blade fan draws cooling air over all internal windings. Air enters at the exciter end and is discharged at the drive end. The complete generator assembly is bolted to the engine’s flywheel and housing.
will be indicated will
indication on the fault code meter. The GPU is programmed at the factory to warn at
1
/4 tank and to
restriction indicating fault code.
fault code and reset the protective system.
function must be reset by pressing the engine stop button Fuel must be added prior to attempting another engine start.
restriction must be removed prior to attempting another engine start.
Or use E-STOP button for immediate reset.
The 400 Hz generator is a brushless, dual bearing, revolving fiel d, three-phase, alternating current type. The front end of the rotor shaft extends forward beyond the front bearing and is coupled to the engine flywheel by a flexible coupling assembly. The rear end of the rotor shaft extends rearward beyond the rear bearing and into the exciter stator housing. The exciter rotor is mounted on this shaft extension with a key and is secured by a washer and 1/2-13 thread cap screw. A rectifier has six diodes mounted on the exciter rotor and converts
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1 2 3 4 5 6 8
7 9 10
11
12
1. 28.5 VDC Con tac tor (optio nal)
2. Cummins QSB4.5 Engine
3. Air Filter Assembly
4. Operator’s Control Panel (back side)
5. Engine Fuel Filter (behind support leg)
6. Engine Oil Filter
Figure 3: Main Components of Generato r Set (Right Side)
7. 12 VDC Batteries (incase in housing)
8. Generator
9. Turbo Exhaust Pipe / Exhaust Outlet
10. Engine Alternator
11. Battery Disconnect Switch
12. Engine ECM Connector
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1 2 3 4 5 6 7
8
1. 28.5 VDC Transformer-Rectifier (optional)
2. Lubric it y Addit i ve Fuel Pre-Filter
3. Engine Electronic Fuse and Relay Panel
4. Engine Control Module (ECM)
Figure 4: Main Components of Generato r Set (Left Side)
5. Engine Oil Level Check
6. Engine Air Intake Heater
7. Charge-Air-Cooler Piping
8. Power Module / Contactor Panel (back side)
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8) Control Box Assembly
The control box is a sheet metal enclosure that houses and provides mounting facilities for engine and generator controls, as well as, monitoring device and circuits.
a) Operator Controls
The control system is divided into three sections. On the left side of the control panel, as one faces it, are engine meters. On the right side of the control panel are generator meters. Below the control panel are pushbutton switches for operating the engine and generator.
(1) Engine Monitoring Section
Engine coolant temperature gage (M24) The temperature gage is an electrical type that is connected by a wire to a water temperature
sensor installed in the engine cooling system. The gage indicates engine coolant temperature in the range of 100-280 º F (38-138º C).
Engine hour meter (M4) The hour meter is electrically driven from the 12 VDC battery system. The hour meter
measures and records the engine’s running time and will record up to 9999.9 hours on five revolving drums. It is only functional when the engine is running.
Engine voltmeter (M5) The voltmeter indicates the voltage across the 12 VDC batteries. The meter scale is
graduated 10 V to 16 V.
Engine fuel gage (M13) An electric fuel gauge receives its controlling signal from a sending unit in the fuel tank. 12
VDC operating power is supplied to the fuel gauge when the ENGINE START pushbutton switch is pressed. The fuel leve l can also be checked when the unit isn’t running by pressing the panel light LAMPS pushbutton switch.
Engine oil pressure gage (M25) The oil pressure gage is an electrical type that is connected by a wire to an oil pressure
sensor installed in the engine lubricating system. The range is 0 to 125 PSI (0 to 862 kPA).
(2) Generator Monitoring Section (shown with analog meters)
Frequency Meter (M3) The frequency meter is an analog type and indicates the frequency of the generator output
alternating current in the range of 360 to 440 Hz (cycles per second).
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1. Engine Coolant Temperature Gauge (M24)
2. Running Time Meter (M4)
3. Battery Voltmeter (M5)
4. Fuel Gauge (M13)
5. Oil Pressure Gauge (M25)
6. Frequency Meter (M3)
13. Panel Light Switch (S74)
14. Air Intake Heater Switch (S79)
15. Engine Start Switch (S24)
16. AC Output No. 1 Switch (S75)
17. AC Output No. 2 Switch (S275)
7. AC Generator Voltmeter (M2)
8. AC Generator Ammeter (M1)
9. Fault Code Meter (M6)
10. DC Voltmeter [Optional with TR]
11. DC Ammeter [Optional with TR]
12. Front LED Display (A5)
18. DC Output Switch (S430) [Optional with TR]
19. DC Starting Current Switch (S431) [Optional with TR]
20. Engine Stop Switch (S76)
21. Test/Reset Switch (S77)
22. Meter Selector Switch (S3)
Figure 5: Operator Controls
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AC Voltmeter (M2) The voltmeter indicates the generator output voltage in each phase-to-neutral (A-N, B-N and
C-N) or phase-to-phase (A-B, B-C and C-A) as selected by the METER SELECT switch. The voltmeter has a scale of 0 to 300 V.
AC Ammeter (M1) The ammeter indicates the generator output current in each phase (A, B and C) as selected
by the METER SELEC T switch. The ammeter has a scale of 0 to 520 A.
Fault Code meter (M6) The function of the fault code meter is to indicate to the operator, that an abnormal condition
of over voltage, under frequency, etc. occurred, which caused the protective monitoring system to function. When one of the circuits are activated, it shows the code on the fault code meter. The fault will remain on for a short period or until the TEST/RESET switch is pressed. Pressing the TEST/RESET switch can also test the fault code meter operation. A meter test should be performed only when disconnected from a load, as the contactor(s) will open during the test cycle.
Front LED Display (A5) The front LED display indicates which voltage (A-N, A-B, etc…) and amperage are shown on
the meters and whether EF BY-PASS is present or bypassed. This EF BY-PASS indicator serves to warn the operator that if the plug interlock system was by-passed any exposed cable may be live.
DC Voltmeter [Optional with TR] The voltmeter monitors and displays the transformer-rectifier’s output voltage. The voltmeter
is an analog type and indicates the output voltage from 0 to 50 VDC.
DC Ammeter [Optional with TR] The ammeter monitors and displays the transformer-rectifier’s output current. The ammeter is
an analog type and indicates the output voltage from 0 to 2500 A.
(3) Operator Pushbutton Switch Section
LAMPS switch (S74) The LAMPS switch controls the lights. Meters are lighted from inside the control panel.
ENGINE HEATER switch (S79) The ENGINE HEAT ER switch activates the standard cold starting aid (manifold air intake
heater), which is totally controlled by the engine’s ECM. Once the heater is activated, the engine’s ECM will control the operation. The heater typically stays on for a period of approximately 30 seconds, which is indicated by the light on the push-button. When the light goes out, the engine is ready to start. Starting a cold engine without first warming the engine will lead to excessive white smoke exhaust and the engine may be hard to start.
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ENGINE START switch (S24) The ENGINE START switch, when pressed, connects 12 VDC power to the starter solenoid
coil, which actuates the solenoid switch to connect power to the engine starting motor. The 12 VDC power is supplied directly to the engine ECM and the oil pressure shutdown switch is bypassed (This bypass is necessary for engine starting because the low oil pressure switch is CLOSED until the engine is running normally). When the engine is running at idle speed, a green indicating light, within the ENGIN E START push button switch, flashes at a rate of 1 second on, 1 second off.
When pressed a second time, this switch provides a signal to the ECM to adjust the engine speed to 2000 RPM. The green indicator light glows continuously. At the same time, a ground signal is provided to the regulator, enabling the generator to build up voltage for 400­Hz generator output. Pressing the switch once more removes these signals and the engine reverts to idle speed with a blinking green indicator light.
OUTPUT switch(s) [Yellow # 1 and/or Orange # 2] (S75, S275) The load contactor push button switch, when pressed, closes the output contactor and turns
on the respective indicating light within contactor control switches (OUTPUT NO. 1 and or OUTPUT NO. 2), indicating that power is available at the plug. When the load contactor opens for any reason, the light is turned OFF.
ENGINE STOP switch (S76) When the ENGINE STOP switch is pressed, the red indicator will blink. Then a 3 to 5 minute
delay will occur to permit the turbo and other engine components to cool evenly. After the delay, power is disconnected from the engine ECM causing the engine to shut down.
TEST/RESET switch (M6, S77) The function of the fault code meter is to indicate to the operator, that an abnormal condition
of over voltage, under frequency, etc. occurred, which caused the protective monitoring system to function. When one of the circuits is activated, it shows the code on the fault code meter. The fault will remain on for a short period of time or until the TEST/RESET switch is pressed. Pressing the TEST/RESET switch can also test the fault code meter operation. A meter test should be performed only when disconnected from a load, as the contactor(s) will open during the test cycle.
STARTING CURRENT Switch (S431) [Optional with TR] Each time the STARTING CURRENT switch is pressed, the BLUE indicator will glow. The
present current limiting amperage setting will be displayed on the fault code meter for a short time delay, before incrementing, at 100 A increments, up to 2500 A. Once 2500 A has been reached, the incrementing will start over from the beginning.
DC OUTPUT Switch (S430) [Optional with TR] Each time the DC OUTPUT switch is pressed, the BLUE indicator will glow when the circuit is
energized, indicating that power is available at the plug. When the load contactor opens for any reason, the light is turned OFF.
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b) Control Box Interior Components
1. Control Box Wrapper
2. Engine Specific PC Board [ESB] (A1)
3. Engine Interface PC Board [EIB] (A2)
4. Digital Control PC Board [CTL] (A3)
5. Voltage Regulator PC Board [REG] (A4)
6. Transformer-Rectifier PC Board [TRB] (A404) {Optional}
Figure 6: Control Box Interior Comp o n ents
7. +5, -12 VDC Power Supply (PS1)
8. Circ uit Breaker Support Bracket
9. Marker Lights Circuit Breaker, 10 A (CB1)
10. Engine Circuit Breaker, 10 A (CB4)
11. Controls Circuit Breaker, 5 A (CB7)
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Figure 7: Engine Specific PC Board
(2) Engine Specific PC Board [ESB] (A1)
The ESB is the primary interface between the control system and the engine’s electronic control module. The ESB is unique to the specific engine model. When the CTL senses the engine start button has been pressed it signals to the ESB, which then communicates to the engine control module what mode of operation is required (idle or rated speed).
The ESB controls the FREQUENCY ADJUST switch that is used to enable the FREQUENCY ADJUST ENABLE/DISABLE potentiometer to test the over/under frequency fault limits of the generator set system. The ESB also controls the DATA REQU EST button and diagnostic indicator light to read the engine’s ECM diagnostic error codes.
(3) Engine Interface PC Board [EIB] (A2)
The EIB is common between all engine models and monitors coolant temperature, oil pressure, battery voltage, and fuel tank level monitoring. The EIB is also responsible for the monitoring the warning switches for high coolant temperature, low oil pressure, high air restriction, and low coolant level (optional). The warning switches signal the EIB when a fault occurs, which then the EIB relays this information to the CTL. The CTL will issue the command to the system that fits the fault event.
The EIB also controls the power distribution in the control system, hour meter, lights, and the engine starter operation.
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Figure 8: Engine Interface PC Board
(4) Digital Control PC Board [CTL] (A3)
The digital control PC board is the center for all communications throughout the entire control system. This board monitors the push-button switches on the control panel and issues appropriate commands to the other PC boards in the control system. The digital control PC board also controls the real time clock, monitors the over/under voltage and overload protection, controls the push-button panel indicator lights, controls the generator output meters, monitors the EF bypass switches, and communicates with the optional service tool.
EF Bypass switches (located on CTL) The EF bypass swit ches, EF1 BYPASS for OUTPUT 1 (or EF2 BYPASS for OUTPUT 2, if
applicable), provide a means of bypassing the 28 VDC interlock circuit for the contactor when supplying power to a load bank or to an aircraft not equipped with a plug interlock system.
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Figure 9: Digital Control PC Board
(5) Voltage regulator PC board [REG] (A4)
This voltage regulator PC board is designed to provide voltage regulation for a three-phase, four­wire, 115/200-volt, 400-Hz brushless alternator. This regulator provides field excitation power as required to meet varying alternator load conditions to hold the alternator voltage constant. In addition, the voltage regulator PC board circuitry provides line-drop compensation. Any deviation of the alternator voltage from its set, regulated level is sensed at the voltage regulator PC board. The sensing signal is compared to a reference signal, and, with associated circuitry, varies the field power supplied to the rotary exciter.
When the machine is started, and the engine is at rated speed, the rotary exciter is excited from alternator residual magnetism through the half-wave rectifier-bridge, located on the voltage regulator PC board assembly. As the rotary exciter voltage increases, alternator excitation increases and the alternator voltage builds up. The sensing circuit of the voltage regulator PC board then compares the input voltage to a reference voltage and adjusts the field power of the rotary exciter to bring the voltage into regulation limits.
When the alternator is loaded, its terminal voltage decreases, lowering the rectified three- phase voltage of the voltage sensing circuit. The sensing voltage is low in respect to its reference voltage, causing the voltage regulator PC circuitry to increase the power to the field of the rotary exciter. The alternator voltage increases until the voltage returns to its regulated value.
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When a load is removed from the alternator, the alternator voltage rises. The rectified three- phase voltage-sensing signal increases, causing this signal to be higher than the reference signal. The associated voltage regulator circuitry causes the field power of the rotary exciter to decrease, lowering the alternator voltage until the voltage returns to regulated value.
The line-drop voltage compensation circuit consists of a current transformer on each phase of the load circuit, and fixed resistance in parallel with each current transformer. The current transformers detects the magnitude of current flowing through the power cables from the alternator to its load and feeds a signal into the voltage regulator PC board. The PC board processes this signal to change the output voltage proportional to the current draw. The regulator output increases slightly so that the alternator output voltage is equal to the regulated voltage plus the voltage drop in the lines. The line-drop compensation potentiometer may be adjusted to match exactly the voltage drop of the power cables carrying the load current.
The under/over frequency protection, EF signal, and lost neutral detection are also monitored by the REG and will signal the CTL when a fault has occurred. The CTL issues the appropriate command that corresponds to the fault.
Figure 10: Voltage Regulator PC Board
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Regulated-diagnostic switch (located on the REG) When the REGULATED/DIAGNOSTIC switch is in the REGULATED (down) position, the
generator output voltage is regulated by the PC board for 115/200 VAC output to an aircraft. When this switch is placed in the DIAGNOSTIC (up) position, 12 VDC is applied to the generator exciter with the engine running at rated RPM, in order to check the operation of the generator. This is done to determine if a particular power output malfunction is caused by a defective generator or by a defective voltage regulator. When this switch is in the MAINTENANCE position, no current is supplied to the generator exciter. In this condition, a low-level, unreg ul ated voltage of approximately 30 VAC will be produced at the generator output terminals due to the residual magnetism of the exciter.
(6) Transformer-Rectifier PC Board [TRB] (A404) [Optional with TR]
The TRB PC Board is only used when the optional 28.5 VDC transformer-rectifier assembly is installed. The TR monitors the output voltage, output current, controls the input and output contactors, and monitors all fault events associated with the DC output. When a fault event does occur the TRB relays this information to the CTL. The CTL will issue the command to the system that fits the fault event.
Figure 11: Transformer-Rectifier PC Board
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Breaker Number
Breaker
Name
Rating
(Amps)
System Protected
CB4
Engine
10
12 VDC engine electrical and fault circuits
CB7
Control 5 12 VDC control system
CB1
Marker Lights
10
12 VDC lighting system
(7) +5, -12 VDC Power Source (PS1)
Supplies the internal power distribution of +5 VDC and –12 VDC into the control system.
Figure 12: Control System Power Source
(8) Circuit Breakers (CB1, CB4, CB7)
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9) Power Module Panel Assembly
The power module panel assembly sometimes referred to as the contactor panel, is located at the rear of the machine under the control box. The panel assembly provides a means of connecting and disconnecting generator output to and from the aircraft.
a) Load contactor (K1 and K201)
Each load contactor contains a magnetic operating coil and four sets of contacts. The three larger contacts conduct three-phase AC generator output. A small contact set is connected to the Digital Control PC Board (CTL) to activate the protective monitor circuit. Three-phase, 40 0-Hz generator output power is distributed to the load contactor by 2/0 cables that pass through current transformers.
b) Current transformers (CT1-CT3 and CT4-CT6)
On each individual output a set of current transformers are used to monitor and control the line-drop compensation, ammeter, and overload circuit.
(1) Line-Drop Compensation
The current transformers detect the magnitude and power factor of current flowing from generator to load. They feed a signal to the voltage regulator that interprets the signal and alters the exciter field current as required to maintain a constant predetermined voltage at the load.
(2) Ammeter
The current transformers convert a current signal to a voltage signal, which is sent to the Voltage Regulator PC Board (REG). The ammeter is really a voltmeter graduated and numbered in amperes to show current proportional to the voltage signal received.
When there is overload on the output for more than 5 minutes (load exceeding 326 amperes per output or 125% of rated load), the main overload sensing circuit sends signals the load the contactor circuit to open the load contactor.
(3) Overload, No 1 and/or No. 2 output
On each individual output the current transformers converts a current signal to a voltage signal. The voltage signal is sent to the ammeter and to the overload monitoring circuit for that output. The overload monitoring circuit will open the contactor when the output current reaches 125% of the normal rated output current. The monitoring circuit monitors each individual output, as well as, the overall current for a dual output machine.
The following is a list of overload module characteristics:
At 125% load the module will function in 5 minutes.
At 150% load the module will function in 30 seconds.
AT 200% load the module will function in 10 seconds.
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Output # 1 Contactor, Current
Transformers and Cabling
Output # 2 Contactor
Location
Generator Lead Connection
Point and Neutral
Hobart Generator
Exciter End
Figure 13: Output Power Module Components
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Air Intake Heater
10) Cold Weather Starting System (BH1)
The intake air heater, located on the intake manifold, is used for starting the engine at very cold temperatures and reduces the white smoke associated with a cold start. This cold weather starting system is fully automatic once engaged by the operator (Chapter 1, Section 3). The intake air heater (or grid heater) is energized or de-energized from a power relay controlled by the ECM. The amount of time the air intake heaters stay on, in the preheat phase, is a function of the intake manifold temperature at start up. (The pre-heat time increases with colder intake manifold temperatures). The maximum duration of the pre-heat phase is around 30 seconds. During cranking, the intake air heater is turned off to allow maximum current to be used by the starter.
CAUTION
Never use an ether start system in conjunction with the air intake heater.
Figure 14: Air Intake Heater
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11) Transformer-Rectifier (T-R) Assembly
The T-R provides a regulated output voltage of 28.5V DC. Input power is provided to the DC components from the 115/200 volt, 400 Hz generator set, through an input contactor. The output contactor provides DC power to the load. If during DC operation, AC power is required, the DC output voltage will no longer be regulated once the AC output contactor is closed. The AC voltage regulator will take over regulating the AC output voltage. The DC voltage will drop during full load applications when the simultaneous operation is used.
a) Transformer Assembly (T401)
This transformer assembly steps down the generator’s output (115/200 VAC, 3 phase, 400 Hz) to 25 VAC. The smaller voltage is rectified by the six diode rectifiers, located on the heat sink assembly.
b) Heat Sink / Diode Assembly (CR402-CR407)
This assembly rectifies the AC voltage from transformer assembly, providing unfiltered 28.5V DC. A DC shunt connected to the heat sink assembly measures the DC output current.
c) Input Contactor (K401)
The input contactor applies the generator output power to the input of the transformer assembly.
d) Output Contactor (K402)
The output contactor connects the output of the 28.5 VDC power supply to the output cables. The contactor is located on the right side under the T-R Assembly.
e) DC Inductor / Filter Assembly (L401)
The DC inductor filters the raw 28.5 VDC from the diode assembly and provides low ripple 28.5 VDC output.
f) Pre-Load Resistors (R402-R404)
The three 10-ohm, 100-Watt pre-load resistors provide a minimum output load on the DC output.
g) Capacitor PC Board (A401)
The DC capacitor PC board works with the DC inductor as a filter to produce a low ripple 28.5 VDC output voltage.
h) Control Interlock Kit (Optional)
This optional assembly is used for applications requiring a safety interlock signal being sent back from the aircraft before closing the output contactor to delivery power to the load. See Chapter 4, Section 3 for details of the assembly and Chapter 5 for schematics and connection diagrams.
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1. Transformer Assembly (T401)
2. Heat Sink / Diode Assembly (CR402-CR407)
3. Input Contactor (K401)
4. Output Contactor (K402)
5. DC Inductor / Filter Assembly (L401)
6. Pre-Load Resistors (R402-R404)
7. Capacitor PC Board (A401)
8. Shunt (R401)
Transformer-Rectifier Components
Figure 15
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Section 2
Preparation for Use, Storage, or Shipping
Lubricating oil capacity (w/ filter)
11.6 quarts (11 liters)
Coolant capacity system
20 quarts (18.9 liters)
1) Preparation for Use
a) Inspection/Check
Inspect the unit thoroughly prior to operation. (1) Remove blocking, banding, ties, and other securing material. (2) Inspect exterior for shipping damage such as broken lights, damaged sheet metal, etc. (3) Open all canopy doors and inspect interior for foreign material such as rags, tools, shipping
papers, etc.
(4) Check fuel, coolant, oil hoses and connections for visible leaks. Visually inspect the compartment
floor and ground surface under the unit for signs of leakage. Correct any leaks by tightening hose
clamps, tube fitting, etc., as required. (5) Check security of generator set retaining components. (6) Check the fuel level. Press the LAMPS pushbutton switch to energize the fuel gauge when the
engine is stopped. Fuel is supplied from a customer-furnished source.
NOTE: For recommended fuel specifications, refer to the Engine Manufacturers Operation and
Maintenance Manual provided with this manual.
(7) Check the engine coolant. Remove the radiator cap to check coolant level. Coolant level should
be at the bottom of the filler neck.
CAUTION
NOTE: For antifreeze protection, use a solution of 50% permanent antifreeze (Ethylene glycol)
Be sure the cooling system antifreeze solution is adequate to protect below the lowest temperature expected.
and 50% clean water.
Figure 1: Engine Oil and Coolant Capacities
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Oil Fill Cap
Dip Stick
(8) Check the engine lubricating oil level. The oil gauge rod has H high mark and L low-level marks to
indicate the operating lubrication oil supply. Oil level should be kept as near the high mark as
possible, without going over it. See Figure 1 for capacity.
CAUTION
NEVER operate the engine with oil level below the L level mark or above the H level
mark.
NOTE: See the Engine Manufacturer’s Operation Maintenance Manual for oil recommendations.
(9) Check the batteries. Inspect the batteries for proper connection of the terminals and check the
electrolyte level (if possible). Service or replace if necessary.
Figure 2: Oil Fill and Oil Level Check Locations
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Chapter 1-2
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b) Installing Three-Phase AC Output Cables
The generator set may be shipped without aircraft cables. The output cables connect to the load contactors, which are located on the power module assembly (left side of the unit beneath the engine control panel).
The conductor size recommended for AC output cables is 2/0 AWG. Use No. 12 size for control (E and F) terminals. Large cables (A, B, C, and N) should be equipped with terminals having at least a 3/8-inch diameter mounting hole. Mounting hole in small leads (E and F) should be at least 1/4-inch diameter.
To install AC output cables proceed as follows: (1) Open the control box door of the generator set and remove the lower panel. (2) Remove the Plexiglas cover in front of the power module assembly. (3) Remove the cover panel on the cable tray covering the cable clamps. (4) Loosen the screws on the cable clamps. (5) Route the cables through cable clamps, and up to the load side of the load contactor(s). (6) Connect the phase cable terminal lugs to the appropriate terminal studs on the contactor(s): cable
lug A to terminal stud A, B to B, and C to C. (7) Connect the cable’s neutral terminal lug securely to the neutral (ground) stud on the power
module assembly. (8) Connect the E and F cables to the E and F studs on the power module assembly. (9) Tighten the clamp screws securely, but avoid damage to the c ab le insul ati on. (10) Replace the Plexiglas cover panel and lower panel and close the c ano p y door .
c) Installing the DC Output Cable (optional)
(1) The DC output cable is not normally supplied unless specifically ordered. For normal aircraft
service, use cable assem bly MS90347 with 4/O size cables having a positive and negative
connection. (2) The output cable is extended through the canopy via the supplied hole and bracket in the frame
assembly (See Figure 3). (3) The cables will be connected to the output contactor, located under the TR assembly on the right
side (See Figure 4).
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Page 4
DC Output Cables
DC Cable and Clamp
Figure 3
Output Cable Connections
Figure 4
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2) Preparation for Storage
When a generator set is to be stored or removed from operation, special precautions should be taken to protect the internal and external parts from rust, corrosion, and gumming in the engine fuel system.
a) General
Pull all circuit breakers and/or disconnect battery negative terminal. (1) The unit should be prepared for storage as soon as possible after being removed from service. (2) The unit should be stored in a building which is dry and which may be heated during winter
months. (3) Moisture-absorbing chemicals (Hobart Part No. 76A1354-001) are available for use where
excessive dampness is a problem; however, the unit must be completely packaged and sealed if
moisture-absorbing chemicals are to be effective.
b) Temporary Storage
When storing the unit for 30 days or less, prepare as follows: (1) Lubricate the unit completely in accordance with instructions in Section 2-2. This will include
changing engine oil, and all filter elements. (2) Start the engine and operate for about two minutes so that all internal engine components will be
coated with new oil.
NOTE: Do not drain the fuel system or crankcase after this run. (3) Make certain the cooling system antifreeze solution is adequate to protect below the lowest
temperatures expected during the storage period. Be sure the solution is thoroughly mixed. (4) Clean the exterior of the engine. Dry with clean rags and compressed air. (5) Seal all engine openings. Use a waterproof, vapor proof material that is strong enough to resist
puncture damage from air pressures.
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c) Long Time Storage (Over 30 Days)
To protect the generator and other electrical components, the complete unit should be packaged using moisture proof packaging material and sealing material. Place containers of moisture­absorbing chemicals (Hobart Part No. 76A-1354-001) in the unit before packaging. The unit may be stored for long periods with no special preparation if it is possible to operate the engine once each week. When starting once a week proceed as follows:
(1) Make certain the cooling system is adequately protected.
WARNING
(2) Start the engine and operate under full load until coolant temperature has reached at least 176ºF
(80ºC). (3) While the engine is running, ensure that normal operating controls are in good working condition
before shutdown and storage. If weekly operation is not possible, contact the nearest engine
manufacturer distributor for instructions.
ENSURE adequate ventilation bef ore star ti ng the eng i ne.
3) Preparation for Shipment
a) Disconnect battery negative terminal before shipping. b) During long shipments, vibration, jolting, etc may loosen the generator set retaining hardware.
CAUTION
NOTE: It is suggested that strong banding be used to secure the generator set, or a strong steel bar
be either welded or bolted across the front of the generator set frame.
When shipping the unit, provide sufficient retaining materials to ensure the generator set cannot roll out or off the vehicle in which it is being transported.
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Page 1
Section 3
Operation
1) General
This section contains information and instructions for the safe and efficient operation of the equipment. Operating instructions are presented in step-by-step sequence of procedures to be followed in supplying 400-Hz power.
NOTE: Read ALL of the operating instructions before attempting to operate the equipment.
WARNING
Ear protection equipment may be necessary when working close to this equipment.
2) 400 Hz. Operating Procedure
a) Pre-start Inspection
(1) Be sure the fuel shutoff valve on the unit is open. (2) Ensure 12 VDC po wer is ava ilabl e to the engin e starti ng s ystem . (3) Check the engine and generator compartments to make certain they are free of rags or other
foreign materials. (4) Make certain there is sufficient lubricating oil and coolant in the engine. (5) Check that all circuit breakers are reset. (6) Make certain the “STARTER ENABLE/DISABLE” switch is enabled, and the “FREQUENCY
ADJUST” switch is disabled.
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Page 2
1. Engine Coolant Temperature Gauge (M24)
2. Running Time Meter (M4)
3. Battery Voltmeter (M5)
4. Fuel Gauge (M13)
5. Oil Pressure Gauge (M25)
6. Frequency Meter (M3)
13. Panel Light Switch (S74)
14. Air Intake Heater Switch (S79)
15. Engine Start Switch (S24)
16. AC Output No. 1 Switch (S75)
17. AC Output No. 2 Switch (S275)
7. AC Generator Voltmeter (M2)
8. AC Generator Ammeter (M1)
9. Fault Code Meter (M6)
10. DC Voltmeter [Optional with TR]
11. DC Ammeter [Optional with TR]
12. Front LED Display (A5)
18. DC Output Switch (S430) [Optional with TR]
19. DC Starting Current Switch (S431) [Optional with TR]
20. Engine Stop Switch (S76)
21. Test/Reset Switch (S77)
22. Meter Selector Switch (S3)
Figure 1: Operator Controls
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b) Normal Engine Starting Procedures
Engine starting procedures are outlined below. The engine’s operating controls and monitoring instruments are illustrated in Figure 1.
CAUTION
CAUTION
CAUTION
Refer to operating instructions in the engine manufacturer’s operation manual, when starting engine for the first time.
NOTE: The engine manufacturer’s operation manual is provided with this manual. (1) If illumination is required, press “LAMPS” push-button switch one time. Pressing this button
switch also activates the fuel gauge. (2) On days when the ambient temperatures are below 60° F, press the “ENGINE HEATER” push-
button to engage the air intake heater prior to starting the engine. The light in the button will
illuminate when the intake heater is engaged (if the light does not illuminate, the engine is ready
to start) and will go off when the intake heater is disengaged, thus signifying the engine is ready
to start.
Never use an ether start system in conjunction with the air intake heater.
(3) Press the green “ENGINE START” push-button switch and hold until engine starts. The engine
will start at idle speed, and the green light in the “ENG IN E START” push-button switch will flash
to indicate that power is available to the engine’s ECM circuit.
Do not attempt to bring to rated speed for at least 5 seconds after engine starts. Damage to the starter and flywheel will result.
CAUTION
If the engine fails to start, the control system will automatically disable the starting motor and indicate a low oil pressure fault. The emergency stop switch must be pressed to reset the control system and allow another starting attempt. If the engine fails to start after four attempts, an inspection should be made to determine the cause.
If the engine fires sufficiently to disengage the starter gear, but does not start, allow the starting motor to come to a complete stop before attempting to engage the starter again, then press the start pushbutton switch.
(4) Check oil pressure to make certain that it is normal and observe all other engine instruments for
normal operation. (5) Allo w engin e to idle and wa rm for 3 - 5 minutes before bringing it up to rated speed.
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CAUTION
To eliminate the possibility of wet stacking (See Appendix A), DO NOT allow the engine to idle for long periods.
c) Failed Starting Procedure
CAUTION
To prevent damage to the starting motor, do not engage the starting motor for more than 30 seconds. Wait two (2) minutes between each attempt to start.
In the event that the engine fails to start, the circuitry must be reset before the next attempt. To do this:
(1) Push the red “EMERGENCY STOP/RESET BUTTON” on the control box door to the right of the
control panel. (2) Pull the red “EMERGENCY STOP/RESET BUTTON” back out before the next attempt to start
the generator set.
d) Power Delivery
(1) Press “ENGINE START” pushbutton switch a second time to bring engine from idle speed to
rated speed. The ECM will immediately increase engine speed to 2000 RPM and maintain it.
The voltage build-up will occur automatically. In addition, the green indicating light in the
“ENGINE START ” push-button switch will glow continuously. (2) Observe generator instruments. The frequency meter should indicate exactly 400 Hz. With the
“METER SELECT” pushbutton switch set to read any line-to-neutral position, (A-N, B-N, or C-N),
the voltmeter should read 115 volts. With the “METER SELECT” pushbutton switch set to any
line-to-line position, (A-B, B-C, or C-A), the voltmeter should read 200 volts. (3) The final step in delivering power is closing one or both of the load contactors. When the
instruments indicate satisfactory frequency and voltage values, close either load contactor (or
both load contactors) by momentarily pressing the load contactor(s) (“OUTPUT NO. 1” or
“OUTPUT NO. 2”) pushbutton switch. The yellow or orange indicating light of the pushbutton
switch that is pressed will glow continuously, indicating that the load contactor is closed and
power is available at the aircraft. (4) Early in the power delivery run it is recommended that the operator check output voltage and
current in each of the three phases. Use the “METER SELECT” pushbutton switch to select the
either the line-to-line or line-to-neutral voltage. If the load is changing, observe the instruments
until load conditions stabilize.
CAUTION
NEVER press the test/reset pushbutton switch while power is being delivered.
The contactors will open and power to the aircraft will be suddenly interrupted.
(5) A condition of over-voltage, under-voltage, under-frequenc y, over-frequency, or overload in the
output circuit will automatically open the load contactor and display a fault code to signal the
operator which of the above faults caused the protective monitor system to operate. After the
fault has been corrected, press the “TEST/RESET” push-button switch to reset the protective
relay system. Proceed with power delivery by operating the load contactor pushbutton switch.
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WARNING
NEVER disconnect the output cable while power is being delivered. Output
contactors must be open prior to removal of the cable from the aircraft.
CAUTION
The generator set must be shut down so that the failed power delivery problems can be diagnosed. Only licensed technicians should work on this generator set.
e) Failed Power Delivery
If the contactor indicating light goes out approximately two seconds after the output pushbutton switch is released, and the fault code meter shows an EF1 or EF2 fault code, this indicates that the aircraft is not supplying the 28.5 VDC interlock signal to the plug interlock circuit. Correct the condition and again press the output pushbutton switch.
The “REGULATED/DIAGNOSTIC” switch (located on the voltage regulator PC board) must be set to “NORMAL” for power delivery.
If the aircraft (or load bank) does not have the 28.5 VDC signal, set the EF Bypass ON/OFF switch (located on the digital control PC board) to the “ON” position.
See “Load Contactor Operating Circuits” in Section 2-4 for other for additional troubleshooting procedures.
f) Discontinue Power Delivery with Unit Shutdo wn
(1) Normal conditions
a Push the “OUTPUT (No. 1 or No. 2) pushbutton switch to open the output load contactor.
The indicating light (yellow or orange depending on the contactor used) on that switch will go OFF immediately to indicate that the load contactor has opened and power is no longer being delivered to the aircraft. The engine will remain at rated speed.
b Push the red “ENGINE STOP” pushbutton switch once to bring the engine down to idle
speed. This will begin the automatic shutdown sequence to shut off the engine, gauges, lights, etc., after approximately 3 - 5 minutes.
c Disconnect output cable from aircraft after engine is at idle speed only. (2) Emergency conditions
a Depress the “EMERGENCY STOP BUTTON” located on the control box door to the right of
the control panel. When pushed this button instantly shuts the generator set off. Pull the button back out to reset it before restarting the generator set.
CAUTION
Do not use the “EMERGENCY STOP BUTTON” button as a normal shutdown device. Damage to the engine turbo charger may result without proper cooling time. Use the “ENGINE STOP” push-button for all normal engine shutdowns.
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3) DC Operating Procedure (optional)
This section describes the operation of the optional DC unit. The DC output voltage value, which is controlled by a potentiometer on the Transformer-Rectifier Board (TRB), need only be set once. The voltage level will remain the same for all future operations, even when the unit is shut down or the battery is disconnected. It may, however, be changed as often as desired.
Note: The DC output voltage is only regulated when operating DC alone without an AC output. If AC
and DC are operated together, only the AC voltage is regulated.
a) Normal Power Delivery
(1) Connect the output cable plug connector to the aircraft receptacle. Be sure connector is mated
fully and securely. (2) The engine should be running at rated speed (2000 RPM) and generating 115/200 VAC. If not,
reference the engine starting procedure above. (3) Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp glows to indicate that DC power is being delivered to the aircraft.
b) Current Limiting Power Delivery
If current limiting is required for starting an aircraft, set the current limit as follows: (1) Press the “STARTING CURRENT” push button to activate and view the present current limiting
value. Continue to hold the button down to increase the setting. (2) Each time the “STARTING CURRENT ” push button is pressed the current limiting will be viewed
and increased by 100 A until it reaches the maximum setting of 2500 A. At that time the current
limiting will reset to the beginning and start the 100 A increments again. Set the current limit to
the desired setting.
c) Discontinue Power Delivery
(1) Press “DC OUTPUT” push button to open the DC output contactor. The blue “DC OUTPUT
lamp turns off to indicate that DC power has been removed from the aircraft. (2) Disconnect the output cable connector from the aircraft receptacle and store properly in the
GPU’s cable tray.
4) Simultaneous AC and DC Operation
If both 28.5 VDC and 400-Hz AC power must be delivered at the same time, the operation of the controls remains the same. However, the DC output voltage will not be regulated when the AC voltage contactor is closed and is supplying power.
When both AC and DC are being used and a fault condition occurs, the system’s response to the fault is given priority over all operations.
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Chapter 2-1
Page 1
Chapter 2
Service and Troubleshooting
Section 1
Maintenance Inspection/Check
60CU20 / Series 500062 / 400 Hz. Generator Set
1) General
To make certain the generator set is always rea dy for operation, it must be inspected and maint ai ned regularly and systematically so that defects may be discovered and corrected before they result in serious damage to components, or failure of the equipment.
WARNING
STOP operations at once if a serious or possibly dangerous fault is discovered.
2) Maintenance Schedule
a) General
A periodic maintenance schedule should be esta bli shed and maintained. A suggested schedule is provided in Figure 1 on the following pages. It may be modified, as required to meet varying operating and environmental condition s. It is suggested that generator set and vehicle inspections be coordinated as much as possible.
b) Maintenance Schedule Check Sheet
It is strongly recommended that the customer use a maintenance schedule check sheet such as t he one in engine manufacture’s operation manual. T he check sheet will provide a record and serve as a guide for establishment of a schedule to meet the customer’s maintenance requirements for his specific operation.
c) Time Intervals
The schedule is based on both hours of operation and calendar intervals. These two intervals are not necessarily the same. For example, in normal o peration the oil change period, based on hours of operation, will be reached long before the three months calendar period. The calendar period is included to make certain services are performed regularly when the equipment is stored, or being operated infrequently. Lubricating oil standi ng in engines that are stored, or used very littl e, may tend to oxidize and may require changing although it is not dirty. Perform all services on whicheve r-comes­first basis.
d) Identification of Interval Periods
Each interval period is identified by a letter A, B, C, etc. For example, services under B schedule should be performed at the end of each 250 hours of operation, or every three months, BR service is performed during the BREAK IN period (first 50-150 hours ) and AR service is performed AS REQUIRED.
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Hourly Interval
AR
50-150
10
250
500
1000
1500
2000
Calendar Interval
Once
Daily
3 Mo.
6 Mo.
1 Yr.
1.5 Yr.
2 Yr.
Symbol
AR
BR A B C D E F
Engine
Change Air Cleaner Cartridge
X Check Coolant Hose and Clamps
X
Check Crankcase Oil Level
X
Drain Fuel PreFilter Elements
X
Check Coolant Level
X
Check for Leaks and Correct
X X Check Air Cleaner Indicator
X
Check Exhaust System
X X
Charge-Air-Cooler (CAC) and Piping
X Change Lubricity Fuel Filter Element
X X
Check Fuel Pump
X
Check Radiator Core and Hoses
X Check Oil Pressure and Record
X
Change Crankcase Oil
X X
Change Oil Filter Element
X X
Check Engine and Generator Mounts
X X
Check Coolant, Additive-Concentration
X X
Check Fan Hub and Drive Pulley
X Check Hose Clamps on Air Intake Side
X X
Check Belts Conditions and Tensioner
X
Check and/or Adjust Valve Clearance
X
Check Water Pump
X X
Steam Clean Engine
X X
Clean Fuel System
X
Check Alternator
X
Check Cranking Motor
X
Check Vibration Damper
X
Check Cooling and CAC systems
X
60CU20 / Series 500062 / 400 Hz. Generator Set
Maintenance Schedule
Figure 1 (Sheet 1 of 2)
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Chapter 2-1
Page 3
Hourly Interval
AR
50-150
10
250
500
1000
1500
2000
Calendar Interval
Once
Daily
3 Mo.
6 Mo.
1 Yr.
1.5 Yr.
2 Yr.
Symbol
AR
BR A B C D E F
Engine (continued)
Flush and Change Coolant
X
Check Fan Mounting
Spring & Fall
Clean Cooling System
Spring & Fall
Check Hoses
Spring & Fall
Clean Electrical Connections
Spring & Fall
Check Thermostats and Seals
Fall
Electrical (12 VDC System)
Check All Lights
X
Check Alternator Charging Rate
X Check Battery and Fluid Level
X
Clean Battery Terminals
X X
Check Wiring and Connections
X Check All Engine Meters
X
Electrical (400-Hz System)
Check E-F By-Pass Operation
X
Check Output Cable and Connectors
X
Check Volt, Amp & Frequency Meters
X
Check and/or Adjust Output Voltage
X X Inspect Wiring and Connectors
X
Clean and Inspect Generally
X
60CU20 / Series 500062 / 400 Hz. Generator Set
3) Inspection/Check
a) General
See Section 2-2 for detailed maintenance procedures. See Section 2-3 for adjustment and test procedures.
Maintenance Schedule
Figure 1 (Sheet 2 of 2)
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60CU20 / Series 500062 / 400 Hz. Generator Set
b) “AR” Checks and Operations (As Required)
(1) Engine
a Change Air Cleaner
Replace the air filter when the fault code meter shows the “air” code. These filters should not be washed because washing breaks down the mate rial inside the filters.
b Check and tighten, as required, all coolant hose clamps, air intake hose clamps and exhaust
clamps. Check all coolant hoses, air intake hoses and exhaust pipes for leaks.
(2) Electrical System (12 VDC) – Check Battery Terminals
Anytime the compartment doors are opened for any reason, visually check battery cable
connectors and battery posts. If corrosion is observed, disconnect cables and clean battery posts
and connectors with a wire brush or special battery post-cleaning tool. Coat posts and
connectors with a light film of petroleum lubricant before reconnecting cables. (3) Electrical (400 Hz System) -- Check Output Voltage
Check the output voltage and be sure it is set for 115 VAC ± 1 V. Adjustment can be made using
the fine adjustment located on the Voltage Regul ator PC Board (REG).
c) “BR” Checks and Operations (Break-In Period, Once After 50-150 hrs.)
The following procedures are precautionary m easures taken on most new engines. If a problem occurs with any of the following issues, be sure to recheck it after the next 50-150 hours.
(1) Engine
a Check for leaks and correct. This involv es an overall inspection of the engine and may
require some maintenance if leaks are found. Refer to the engine manufacturer’s operations
manual for assistance. b Change all fuel filter elements. Metal shavings from the new fuel tank can clog the filter. c Change crankcase oil. New engines often release metal shavings more frequently.
Therefore, the crankcase oil must be changed as a precautionary measure. d Change oil filter element. The oil filter should be changed with the oil. e Check engine and generator mounts to ensure they are properly installed and they have not
worked loose. (Torque is set at 122 N-m, 90 ft-lb.). f Check coolant additive concentration. Refer t o the engine manufacturer’s operations manual
for assistance. g Steam clean the engine to free it of oil and dirt to prevent uneven engine cooling “hot spots”.
The oil and dirt can also fall into the engine and fuel system when covers are removed during
repair work. h Inspect the water pump weep hole for indicatio n of a steady leak. If a steady flow of coolant
or oil is observed, replace the water pump with a new or rebuilt unit. Refer to the engine
manufacturer’s operations manual for assistance.
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60CU20 / Series 500062 / 400 Hz. Generator Set
d) “A” Checks and Operations (10 Hours or Daily)
(1) Engine
a Check Crankcase Oil Level
CAUTION
CAUTION
WARNING
DO NOT overfill. DO NOT operate the engine with oil level below the lower bar or
above the upper bar on the dipstick.
(i) Check oil level daily with oil gauge dipstick.
(ii) Oil level should not be checked until 3 to 5 minut es after engine shutdown. Keep oil
level as near the upper bar as possible.
b Drain Fuel Lubricity Filter/Pre-Filter Element
The life of the fuel pump and injectors can be ext ended if the operator drains about a cup of
fuel from the fuel pre-filter element to remove wat er and sediment before starting the engine
each day.
BE SURE to prime and bleed the fuel system after draining the filters, replacing filter element, or if the fuel tank has run empty. F ai lure to do so can cause engine-starting problems.
(i) Provide a container for catching drained fuel.
(ii) Open the drain valve on the fuel/water filter by turning it counterclockwise.
(iii) Drain the filter until clear fuel is visible.
(iv) Tighten the drain valve.
(v) Safely dispose of drained fuel.
(vi) Purge air from fuel system if necessary. c Check Coolant Level
Check coolant level daily or at each fuel fill interv al . Investigate for cause of any coolant loss.
Cooling system is pressurized. To avoid personal injury, DO NOT remove radiator cap when engine is hot.
d Check for Leaks and Correct
At each daily start-up, check for coolant, fuel, and oi l l eaks. Coolant leaks may be more
noticeable when components are cold. Obse rv e pumps, hoses, fittings, gasket connections,
etc., for signs of leakage. Correct as require d.
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60CU20 / Series 500062 / 400 Hz. Generator Set
Water Drain
e Check Fault Code Meter
At each daily start-up, observe the fault code meter on the control panel. If the display shows
“air”, change the air filter. See Section 2-4 for oth er fault codes. f Check Exhaust System
Visually inspect muffler and exhaust pipes f or rust and signs of approaching failure. Listen f or
any gasket or joint leaks.
WARNING
A leaking and defective exhaust system could be a fire hazard.
Fuel Pre-Filter and Drain
Figure 2
(2) Electrical System (12 VDC)
a Check All Lights
Check all indicating lights to be sure they will operat e when they should. If any light fails to
operate, check both the lamp and its protective circuit breaker. Figure 5 lists all lamps with
their location and part number. Figure 6 list s all circuit breakers. b Check Engine Battery Voltage
Observe the 12 VDC engine voltmeter each time the engine is started to be sure the
alternator is functioning correctly and charging the batteries. If the batteries need t o be
replaced, be sure the replacements meet the specifications for Cold Cranking Amps (CCA)
and Reserve Capacity. c Check the operation of all the engine meters.
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60CU20 / Series 500062 / 400 Hz. Generator Set
(3) Electrical (400 Hz System)
b Check Output Cables and Connector
Check the output cable and plug connection for damaged i nsulation and contacts each time
the connector is detached from the aircraft. b Monitoring Instruments
Check operation of voltmeter, ammeter and frequency meter each time the unit is started.
e) “B” Check and Operations (250 Hours or 3 Months)
(1) Engine
a Prevent Diesel Engines Wet Stacking
All diesel engines operated for extended periods under light load may develop a condition
commonly referred to as wet-stacking. This condition results from the accumulation of
unburned fuel in the exhaust system. It is recognizable by fuel oil wetness around the
exhaust manifold, pipes, and muffler along wit h an excessive amount of soot.
Wet-stacking is common, and can be expected in diesel engines operated under light loads.
Light loads do not allow the engine to reach the most efficient operating temperature for
complete combustion of fuel and will also increase the fuel consumption rate. The unburned
fuel collects in the exhaust system to create the wet condition known as wet-stacking.
To alleviate wet-stacking in lightly loaded engines, it is recommended that the machine be
connected to a load bank after each 250 hours of use and operated under full rated l oad for
one hour. This will burn away and evaporate the accumulation of fuel and soot in the exhaust
system. This clean-out procedure should be considered as a regular maintenan ce operation
for machines operated under light loads. b Charge-Air-Cooler and Piping
Inspect the charge-air-cooler for dirt and debris blocking the fins. Check for cracks, holes, or
other damage.
Inspect the pipes and hoses for leaks, holes, cracks, or loose connections. Tighten the hose
clamps if necessary. c Check and record oil pressure
After each oil change, check and record oil pre ss ure at idle speed after oil has warmed to
approximately 140º F. Record oil pressure und er identical conditions at each oil change
interval. A comparison of pressure at idle spe ed with previous readings will give an indication
of progressive wear of oil pump, bearings, shafts, etc. Investigate any abnormal change in
pressure readings.
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d Check Radiator Core and Hoses
Inspect the radiator core for dirt and debris blocking the fins. Clean as necessary. Check for
cracks, holes, or other damage. e Check Fuel Pump
Inspect the fuel injection pump mounting nuts f or l oose are damaged hardware.
(2) Electrical (12 VDC system)
NOTE: The battery furnished with this g enerator set is MAINTENANCE FREE. Check battery terminals and clean if necess ary.
(3) Electrical (400 Hz System)
a Check the operation of the E-F bypass system.
f) “C” Checks and Operations (500 Hours or 6 Months)
(1) Engine
a Check Engine and Generator Mounts
CAUTION
An unstable or loosely mounted engine can create hazardous environment and may damage equipment.
(i) Engine mount bolts must be torqued to 122 N-m (90 ft-lb.).
(ii) Generator mount bolts must be torqued to 122 N-m (90 ft-lb.). b Change oil and oil filters c Change all fuel filters. d Check Coolant Additive Concentration
The cooling system protective liquid (nitri te-, amine- and phosphate free) provides effective
protection against corrosion, cavitation, and freezing. See engine manufacturer’s operation
manual for ordering and mixture details.
(2) Electrical (12 VDC system)
a Wiring
Inspect all cables and leads for worn or damag ed i nsulation. b Connections
Inspect connectors for damaged or corroded condition.
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(3) Electrical (400 Hz System)
a Protective Monitoring Circuits
Check operation of all protective monitoring circuits to make certain they will function if a fault
should occurs in the output circuit. Procedures f or testing these circuits are contained in the
Adjustment/Test section of this manual. b Inspect Wiring and Connections
Check all cables, leads, and wiring for broken, worn and damaged insulation. Check all
connections for tightness. c Clean and inspect generally
g) “D” Checks and Operations (1000 Hours or 1 Ye ar)
(1) Engine
a Check Fan Hub and Drive Pulley
Inspect for loose bolts or worn features. Tight en bol ts and replace parts if necessary. Refer
to the engine manufacturer’s operations and m ai ntenance manual for assistance and the
most update to date information. b Check Hose Clamps on Air Intake Side
Be sure that all clamps are properly secured to prevent leaks and all hose are in good
condition. c Check Belt Condition and Tensioner
Refer to the engine manufacturer’s operat i ons and maintenance manual for assistance and
the most update to date information. d Check and/or Adjust Valve Clearance
Refer to the engine manufacturer’s operat i ons and maintenance manual for assistance and
the most update to date information. e Check Water Pump
Inspect the water pump weep hole for indication of a st eady leak. If a steady flow of coolant
or oil is observed, replace the water pump with a new or rebuilt unit . Refer to the engine
manufacturer’s operations manual for assistance.
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h) “E” Checks and Operations (1500 Hours or 1.5 Y ear )
(1) Engine
a Steam Clean Engine
There are several reasons why the engine ext erior should be kept clean. Dirt on the outside
will enter fuel and oil filter cases and rocker housings when covers are removed, unless dirt is
removed first. A clean engine will run cooler and develop fewer hot-spots. Steam cleaning is
one of the most satisfactory methods of cl eani ng and engine; however, there are some
CAUTIONS to be observed:
WARNING
Exercise care to avoid injury and damage to eyes and skin.
CAUTION
1. If a cleaning compound is used, select one that is free from acid and will not remove paint.
2. Protect (or remove) all electrical accessori es, such as voltage regulator, alternator, and electrical wiring.
3. Seal all openings. DO NOT use a flammable solvent.
4. DO NOT use mineral spirits or solvents on a hot engine.
5. Remove or protect bottom panel of unit (belly pan) to protect insulation.
b Clean Fuel System
See engine manufacturer’s operation manual for instructions.
c Check Alternator and Cranking Motor.
The alternator and cranking motor on this particular engine require no periodic lubrication.
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2
1
5
6
3 7 4
60CU20 / Series 500062 / 400 Hz. Generator Set
i) “F” Checks and Operations (2000 Hours or 2 Years)
(1) Engine
a Check Vibration Damper.
1. Fan Pulley
2. Vibration Damper
3. Engine Control Module (ECM)
4. Exhaust Outlet
Engine Accessories
Figure 3
Check vibration damper for looseness, wobble, chunking and streaking. Also verify the hub bolts are tightened to the engine manufacturer’s specifications.
Refer to the engine manufacturer’s operat i ons and maintenance manual for assistance and the most update to date information.
b Check Charge-Air-Cooler and Radiator Systems
(i) Check for damaged hoses and loose or damaged hose clamps.
c Flush cooling system and change coolant.
(ii) Check the radiator for leaks, damage, and build up of dirt in the fi ns. Clean or replace as
necessary.
5. Alternator
6. Belt Tensioner
7. Fuel Pump
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j) Seasonal Maintenance Checks Spring/Fall (Engine)
(1) Check Fan Mounting
a Check fan to be sure it is securely mounted. b Check for fan wobble and/or broken/cra ck ed bl ades.
c Check fan hub and crankshaft pulley for secure mounting. (2) Check cooling system each spring and fall. Clean if necessary. (3) Check All Hoses.
In addition to daily checks of hoses for leaks, ins pect hoses thoroughly each time the cooling
system is cleaned and serviced.
Inspect for signs of deterioration and collapse. Inspect for cracks and cuts. Inspect for cuttin g
and deformation caused by hose clamps. Repl ace hoses as required. (4) Check thermostat and seals each fall when cooling system is serviced.
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Schematic
Identifier
Engine Air Intake Heater
Engine
Electrical Panel
REG Load Contactor Circuit
REG Board
REG Diagnostics
REG Board
F3
1
MDL 1 A, 250 V
REG Field Voltage Circuit
REG Board
TRB Load Contactor Circuit
TR Board
ECM Protection
F101 1 5 A
ECM Protection
F102 1 30 A
2 A, 250 V (Fast
Blow)
60CU20 / Series 500062 / 400 Hz. Generator Set
k) Lamps Circuit breakers, and Fuses
(1) Check all lamps daily (2) Check circuit breakers and fuses as required. (3) The lamp chart lists all lamps with their location and identifying trade num ber in table below. (4) The circuit breaker chart lists all circuit breakers with their location, size, and type. (5) The fuse chart lists all fuses with their location, size, and type.
Item Protected Location
Quantity Type
F110 1 125 A, 300 VAC
F2 1 MDL 1 A, 250 V
F1 1 MDL 5 A, 250 V
F1 1 MDL 1 A, 250 V
Starter Solenoid
F112 1
Fuse Identification Chart
Figure 4
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Lamp (Bulb) as per Lamp
Description
60CU20 / Series 500062 / 400 Hz. Generator Set
Light Identification Location
Industry Trade Number or
Engine Start Indicator Switch Panel 1815 Engine Stop Indicator Switch Panel 1815 No. 1 Load Contactor Indicator Switch Panel 1815 No. 2 Load Contactor Indicator Switch Panel 1815 Test/Reset Indicator Switch Panel 1815 Pre-heater Indicator Switch Panel 1815 Clearance Lights (optional) Canopy Top 57 Engine Gauge Lights Inside Each Gauge Chapter 4, Section 3, Fig. 6 Generator Gauge Light Strip Around Meter Chapter 4, Section 3, Fig. 6
Lamp Identification Chart
Figure 5
Item Protected Location Quantity Size
Engine Circuit and Instrument Panel Inside Control Box 1 10 A Controls Inside Control Box 1 5 A Marker Lights (optional) I nside Contr ol Box 1 10 A
Circuit Breaker Identification Chart
Figure 6
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Section 2
Maintenance Procedures
Item
Maintenance Required
Check oil level daily or after every 10 hours of use. Change oil and the oil filter thereafter. Engine oil capacity is approximately 11.6 quarts (11 liters).
Check coolant level daily. Service and maintain coolant system according to (18.9 liters)
Coolant hoses and connections
panel shows the “Air” code.
Fan Belt
Check fan belt condition and tension every 1000 hours or 1 year of use.
Alternator
Alternator bearings are sealed and require no periodic lubrication.
Starter
Starter motor bearings are sealed and require no periodic lubrication.
Water Pump
The water pump is packed at assembly and requires no periodic lubrication.
Fan Hub
The fan hub is lubricated at assembly and requires no periodic lubrication.
AC Generator
Periodic cleaning – no lubrication or adjustment required
Generator Controls
No periodic maintenance is required. Adjustments are covered in Section 2-3.
1) General
A suggested maintenance schedule is provided in Section 1 of this Servicing Chapter. Each step of the schedule is also covered in general in Section 1. This Section covers maintenance in more detail, where necessary.
Engine Oil
Fuel Water Separator
Coolant
Air Cleaner
after the first 50 to 150 hours of use, then at 500 hour or 6 month intervals
Drain filters daily. Change the filter elements every 500 hours or after 6 months of use, whichever comes first.
Section 2-2, paragraph 6. Engine coolant capacity is approximately 20 quarts
Check coolant hoses and connections daily for leaks.
Change air cleaner filter as required when the fault code display on engine control
Figure 1: Lubrication and Maintenance Chart
WARNING
STOP operations at once if a serious or possibly dangerous fault is discovered.
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Refer to the manufacturer’s operation manual.
Capacity
Approximately 11.6 quarts (11 liters)
Oil Filter Part Number
VISCOSITY
AMBIENT TEMPERATURE CONDITIONS
SAE 0W30
-20ºF and below to +50ºF (-29ºC and Below to +10ºC)
See the engine manufacturer’s operations manual for usable synthetic oils and instructions.
2) Engine Lubrication
a) General
Proper lubrication is one of the most important steps in good maintenance procedure. Proper lubrication means the use of correct lubricants and adherence to a proper time schedule. Lubrication points, frequency of lubrication, and recommended lubricants are indicated in Figures 1 and 2.
This section incorporates the engine manufacturer’s engine lubrication recommendations from their “Operation and Maintenance Manual.”
Lubrication schedule Time schedules indicated on the Lubrication Chart, Figure 1, are approximate and based on average
operating conditions. It may be necessary to lubricate more frequently under severe operating conditions such as: low engine temperatures, high oil temperatures, or intermittent operation. However, time intervals should not exceed those indicated in the chart without careful evaluation.
b) Oil specification
The engine lubricating oil that is recommended by the engine manufacturer is identified by an API (American Petroleum Institute) classification designation. The manufacturer does not recommend any specific brand of lubricating oil.
The use of quality lubricating oil, combined with appropriate lubricating oil drain and filter change intervals, are important factors in extending engine life.
Oil Type
Replacement
Lube Oil Viscosity Required as per Ambient Temperatures
Synthetic Oils
Use oil specification API CF-4, HT/HS Viscosity 3.7cP minimum. Oil recommended for the diesel engines in this application is API Class CCMC.
Hobart: 286897-029 Cummins: LF9370
SAE 15W40 (Preferred) SAE 10W30 SAE 5W30
0ºF (-18ºC) and above for most climates
-10ºF to +50ºF (-23ºC to +1 0ºC) Winter conditions
-20ºF to +50ºF (-29ºC to +10ºC) Arctic Conditions
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Always use clean containers, funnels, etc.
Dip Stick
Oil Fill
c) Changing engine oil
Change the oil once after the first 50 - 150 hours of use and then every 500 hours of engine operation thereafter. The generator set is equipped with an hour meter to record actual engine operating time.
The ideal time to change engine oil is soon after a power delivery run, when the engine is at operating temperature. If lubricating oil is drained immediately after the unit has been run for some time, most of the sediment will be in suspension and will drain readily.
Change the oil filter element each time the oil is changed.
CAUTION
High ash oils may produce harmful deposits on valves that can cause valve burning.
Do not use solvents as flushing oils in running engines.
Figure 2: Oil Fill and Check Locatio n s
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Change oil as follows: (1) Provide an open container for catching the old oil below the oil drain plug. Container capacity
must be greater than 30 quarts (28.4 liters).
(2) The oil drain tube can be attained though a hole in the access panel underneath the generator
set. (3) Open drain pl ug located in oil pan. (4) While oil is draining, change the oil filter element. See instructions below. (5) Provide a container for catching spilled oil from the filter. (6) Remove the oil filter by twisting counter-cloc kwise and inspect it. (7) NOTE: The gasket can stick to the filter head. Make sure it is removed before installing a new
filter. (8) Fill the new filter with clean lubricating oil before installation. (9) Apply a light coating of lubricating oil to the gasket-sealing surface and install the filter. DO NOT
over tighten the filter. (10) Clean the drain plug and install when engine oil has completely drained. Torque the drain plug to
50 foot-pounds (68 Nm). (11) Refill the engine with new, clean oil that meets engine manufacturer’s recommendations.
CAUTION
CAUTION
CAUTION
Remember to close the drain plug valve and install the new oil before starting the engine.
(12) Start engine and check oil pressure at once. Allow engine to idle for 5 minutes, check for leaks,
than stop the engine. (13) After the engine has been stopped for about 5 minutes, recheck the oil level. Add oil, if required,
to bring the level up to the high bar on the oil dipstick.
If bearing metal particles are found on the element or in the shell, the source should be determined before a failure.
Determine source of moisture, internal leaks, defective seals, gaskets, etc.
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1
Grease, General Purpose
MIL-G-3545
Excludes those of sodium or soda soap thickness.
Symbol Name Specification Notes
Lubricants Chart
e) Engine Accessories Lubrication
(1) Alternator
Most alternators contain sealed bearings and require no periodic lubrication, however, check to
make certain there are no lubrication points on your particular alternator. (2) Starter
Most starting motors are lubricated at assembly and should be re-lubricated on l y when the starter
is removed and disassembled, however, inspect the starter to make certain it has no lubrication
points. (3) Water Pump
The water pump is packed at assembly and requires no periodic lubrication. Replace pump if
signs of lubricant leakage are found. (4) Fan Pulley
The fan hub is also lubricated at assembly and requires no periodic lubrication. Replace hub if
lubricant is leaking.
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Replacement air filter part
3) Servicing the Air Cleaner
A definite time schedule for cleaning or changing the air cleaner cannot be determined because of varying operating conditions. Unfasten the three metal latches on the end of the air cleaner housing to access the air cleaner filter. It may be inspected either at prescribed service intervals or at any time deemed necessary.
number: Hobart: 290941
Inspect regularly. Replace when the fault
code meter indicates an “Air” code.
a) Inspecting the Air Cleaner
(1) Make periodic checks of air cleaner inlet screen for obstructions. If any obstructions are present,
(2) Check outlet connection for proper seal.
b) Changing the Air Filter
(1) Lift the latch and rotate the back cover to the unlocked position (counterclockwise as viewed from
(2) Remove the end cover of housing. (3) Pull out air filter elements and replace. (4) Replace end cover on housing, making certain that the filter is centered in the housing. (5) Replace the end cover and rotate it to the locked position.
Figure 3: Air Cleaner Assembly
remove them.
the rear). The cover has padlock symbols to show the locked and unlocked positions.
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c) Disposal
Normal trash pick-up is should be acceptable. NEVER burn the air filter for disposal.
4) Engine Fuel
a) How to select Fuel—Quality
The quality of fuel oil used in the diesel engine is a major factor in engine performance and life. Fuel oil must be clean, completely distilled, stable and non-corrosive.
CAUTION
Due to the precise tolerances of diesel injection systems, it is extremely important that the fuel be kept clean and free of dirt or water. Dirt or water in the system can cause severe damage to both the injection pump and the injection nozzles.
CAUTION
Use commercially available diesel fuel with less than 0.5% sulfur content. If the sulfur content is higher than 0.5%, oil change intervals should be reduced (See engine manufacturer’s operation manual).
In general, fuels meeting the properties of ASTM designation D 975 (grades 1-D and 2-D) have provided satisfactory performance. For more information regarding the selection of fuel to use, refer to publication “Engine Requirements—Lubricating Oil, Fuel, and Filters” available from authorized engine manufacturer’s service outlets.
b) Cold Weather Operation
In cold weather, diesel fuel will form wax crystals, which can restrict flow and clog filters. Fuel oil suppliers approach this problem several ways. Some provide a specially refined product, while others may use flow-improving additives or winter blends. Winter blended fuel will likely contain kerosene or 1-D fuel, which provide good cloud point temperatures, but result in a lighter fuel with a lower heat content. These fuels may be used, but they may result in reduced engine power and/or fuel consumption.
In most cases, adequate resistance to cold can be obtained by adding an additive. For further assistance contact the nearest engine manufacturer’s service representative.
The use of low lubricity fuels can shorten life and/or damage the engine’s fuel pump. The engine manufacturer recommends only diesel fuel.
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Water Drain
5) Engine Fuel System
The fuel system consists of five primary components: fuel tank , lubricity filter, primary fuel filter, fuel lift pump, and the fuel return line. The following are maintenance procedures for each of these item s.
a) Fuel Tank
Be sure that no foreign objects are permitted in the fuel tank. The fuel tank must be removed and flushed out if objects are found in the Fuel Water Separator or Lubricity Additive Filter.
b) Fuel Water Separator or Lubricity Additive Filter
A lubricity fuel filter, which is also a fuel/water separator, is mounted in the generator compartment above the fuel tank outlet. The filter’s function is to add a lubricant to the fuel to help prolong the engine seals and fuel pump life when fuels other than diesel are used (i.e. jet fuel). The filter also removes foreign material and removes both free and emulsified water from the fuel before it enters the fuel lift pump. Daily draining of the filter is required.
Replacement Filter Element:
Hobart: 286897-031
Cummins. FS20022
Drain the water daily. Replace the filter after every
500 hours of operation.
To drain the water:
(1) Open drain valve (2) Drain accumulated water and contaminants.
Figure 4: Lubricity Filter
(3) Close drain valve. The lubricity filter must be changed after every 500 hours of operation in order for the fuel filter to
continue adding the proper amounts of the lubricity additive into the fuel system.
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Replacement fuel filter part number:
Figure 5: Primary Fuel Filter
To change the lubricity filter :
CAUTION
(1) Place a pan underneath the fuel filter to catch spilled fuel. (2) Shut off fuel valve. (3) Drain of f som e fuel by opening the drain val ve . (4) Undo fuel filter with commercial tool and spin off. (5) Clean any dirt from the filter carrier rim (6) Apply a light film of oil or diesel on the rubber seal on the new filter. (7) Fill new filter with diesel fuel. (8) Screw in the new fuel filter “snug”. (9) Check that the cartridge is seated correctly against the gasket and tighten with a final half turn. (10) Make sure that all rags, or absorbent sheets, are clear of moving engine parts and cannot be
drawn in to the radiator fan. (11) Open fuel valve. (12) Start the engine and check for leaks. Correct as necessary with the engine off.
c) Primary Fuel Filter
A primary fuel filter is mounted above the engine starter in the engine compartment. The filter’s function is to remove foreign material from the fuel before it enters the fuel lift pump.
Change the fuel filter after every 500 hours of operation.
When installing new elem ent, do not over tighten it; mechanical tools may distort or crack filter head.
Hobart: 286897-036
Cummins: FF5612
Change the fuel filter after every 500 hours of operation.
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DO NOT attempt to crack fuel lines. This engine is equipped with a common rail fuel injury or death.
The fuel filter must be change after every 500 hours of operation.
To change the fuel filter:
(1) Shut off fuel valve. (2) Place a pan underneath the fuel filter to catch spilled fuel. (3) Undo fuel filter with commercial tool and spin off. (4) Catch any fuel. (5) Clean any dirt from the filter carrier rim (6) Apply a light film of oil or diesel on the rubber seal on the new filter.
CAUTION
CAUTION
(7) Fill new filter with diesel fuel. Screw in the new fuel filter “snug”. Check that the cartridge is
(8) Open fuel valve.
d) Fuel Pump
The fuel pump supplies high pressure to the fuel system so the diesel fuel can circulate freely. This engine is equipped with a common rail fuel system that is under very high pressure. DO NOT attempt to crack fuel lines.
WARNING
e) Fuel Return
The fuel return is a fuel line (tube) that takes unused fuel from the engine, and delivers it to the fuel tank. No maintenance is required.
When installing new element, do not over tighten it; mechanical tools may distort or crack filter head.
Make sure that all rags, or absorbent sheets, are clear of moving engine parts and cannot be drawn in to the radiator fan.
seated correctly against the gasket and tighten with a final half turn.
system that is under very high pressure. Failure to follow this guideline could result in
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6) Engine Cooling System
a) General
Cooling system service requires more than maintaining the proper coolant level in the radiator and protecting the system against freezing. Water should by clean and free of any corrosive chemicals such as chloride, sulfate, and acids. It should be kept slightly alkaline with a pH value in the range of
8.0 to 9.5. Any water, which is suitable for drinking, can be used in the engine when properly treated as described in engine manufacturer’s operation manual. The engine manufacturer’s representative should be consulted regarding the selection of satisfactory brand, permanent-type antifreeze for use in the cooling system.
b) Radiator Cap
(1) General
A pressure relief valve is built into the radiator cap. It is designed to open at a pressure of
approximately 15 psi (103.4 Kpa).
WARNING
(2) Removal
To remove, turn the cap to the left (counterclockwise) to the safety stop. When all pressure is
released, press down on the cap and continue to turn until the cap is free to be removed.
When removing cap from a very hot radiator, do not turn cap past safety stop until the pressure or steam has escaped.
CAUTION
CAUTION
c) Coolant
Allow engine to cool before adding coolant.
Do not attempt to repair the valve in a radiator cap in case of failure. Replace with a new cap.
(3) Installation
When installing the cap, be sure it is turned clockwise as far as it will go so that the pressure
retaining valve will be functional.
The preparation and maintenance of the coolant solution is important to engine life and is completely covered in the engine manufacturer’s operation manual. For information regarding coolant specifications, testing equipment, antifreeze, etc., refer to engine manufacturer’s operation manual that accompanies the equipment manufacturer’s manual or consult the local engine manufacturer’s representative.
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CAUTION
Never use soluble oil in the cooling system.
(1) General
A permanent type antifreeze is recommended for use in the cooling system.
CAUTION
1. DO NOT use methanol or alcohol as antifreeze.
2. DO NOT mix brands or type of antifreeze. A solution containing two or more types of antifreeze is impossible to test accurately.
(2) Selecting antifreeze
a Select a permanent type antifreeze known to be satisfactory for use with chromate corrosion
resistor.
b When it is not known if the antifreeze is satisfactory for use with chromate resistor, check with
local engine manufacturer’s representative for a list of compatible antifreezes.
(3) Checking antifreeze solution
Check the solution with a reliable tester when in doubt about antifreeze protection.
d) Draining the Cooling System
To completely empty the cooling system requires draining the engine block (if furnished) and the radiator assembly. Both drain valves (radiator and block drain), can be opened/closed at the same time but they do not need to be. Follow these steps to drain the cooling system:
(1) Remove radiator cap. (2) Place a drain pan with at least a 40 quarts (28.4 liters) capacity under radiator to catch coolant. (3) Place the radiator drain hose that comes off the two radiator dra in valv es, into the drain pa n. (4) Open the radiator drain valves. (5) Allow the system to drain completely. NOTE: Be sure the drain valves do not clog during draining. (6) When the system is completely drained, close the drain valves and replace engine drain plug.
e) Flushing the Cooling System
Flushing the cooling system should be a yearly maintenance procedure. By flushing the system, clean water is forced through the engine block to remove expired coolant and other contaminants.
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f) Cleaning the Radiator Core
Blow out accumulated dirt from the radiator core air passages, using water. Bent or clogged radiator fins often cause engine overheating. When straightening bent fins, be careful not to damage the tubes or to break the bond between fins and tubes.
NOTE: Direct the water in a reverse direction to normal air flow. Normal flow on this installation is from the engine compartment out ward.
g) Filling the Cooling System
The preparation and monitoring of coolant in liquid-cooled engines is especially important because corrosion, cavitation, and freezing can lead to engine damage. For coolant system protection details see the engine manufacturer’s operations manual.
(1) Install coolant
a Remove radiator cap. Be sure that both radiator drain valves are closed.
b Pour coolant into radiator very slowly until it reaches the bottom of fill neck. Allow time for
trapped air to escape from the system then continue filling until the coolant level remains at the bottom of the fill neck.
c Start the engine and bring up to rated speed and allow the thermostat to open. Add coolant
as trapped air escapes from the system and the coolant level falls.
(2) Inspection/Check
NOTE: It is good practice to attach a card, indicating the cooling system contents and date serviced, to the radiator filler neck.
h) Thermostat
The thermostat should be checked each fall, or as required. Refer to engine manufacturer’s operations manual for recommended instructions.
d Continue to check coolant level until all trapped air escapes. Add coolant if needed to fill to
the bottom of fill neck. Install radiator cap.
a Check system for evidence of leaks.
b Inspect all hoses. Install new hoses as necessary. Tighten hose clamps as required. c Check the condition of fan and water pump belts. Replace belts if necessary.
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7) Engine Drive Belt
a) General
The engine cooling fan, alternator, and water pumps are driven by one serpentine belt, which must be replaced if worn or damaged.
b) Preparation for Belt Check and Adjustment
All driven assemblies must be securely mounted in operating position before checking belt tension.
c) Checking Belt Tension
CAUTION
Check belt tension every 1000 hours, or once year, whichever comes first. A belt that is too tight is destructive to bearings of the driven part. A loose belt will slip and cause inefficient operation of the part being driven as well as wear to the belt.
CAUTION
Belt tension may be checked by hand. To do so, manually depress the belt with an index finger to determine the amount of belt deflection obtained. When a force is applied at a point halfway between pulleys on the longest span of a belt, there should be no more than 1/2 inch of deflection attained.
Refer to the engine manufacturer’s operation manual for checking belt tension and changing worn belts.
Checking the tension and changing the serpentine belt should only be performed with the engine off.
Inspect and replace the belt if it has unacceptable cracks, is frayed, or has pieces of material missing.
8) Generator Maintenance
The 400 Hz generator requires no maintenance or service other than periodic cleaning. The unit is brushless and has bearings that are permanently lubricated and sealed.
a) Cleaning
The generator may be cleaned by careful use of compressed air and/or a good, SAFE commercial cleaner. Steam cleaning of the generator is not recommended because the use of steam and harsh chemical compounds may result in damage to insulation and other generator components.
CAUTION
b) Adjustment
The generator itself requires no adjustment. Adjustment procedures for generator controls are covered in Section 2-3.
Do not use a flammable solvent. Be sure the unit is completely dry before operating.
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Section 3
Adjustment/Test
1) General
These adjustments and test procedures are applicable to testing and adjusting the generator set after major repair, major parts replacements, or overhaul.
IMPORTANT
In order to perform most of the following test, a load bank with an EF interlock circuit is required. However, if no EF interlock is available on a load bank, see special procedure in the EF Bypass section for testi ng the EF c irc uit.
2) Testing the 400 Hz. Generator Set
a) Pre-operational Test Procedures
(1) Connect cables from the generator output terminals to a load bank. Use cables of the same size
and length as those to be used in service. Be sure the generator output N cable is grounded. (2) Check engine oil level. Oil should be at the high bar on the dipstick. (3) Check radiator coolant level. (4) Check tension of drive belt. (5) Inspect for oil, fuel and coolant leaks. (6) If the setting of the output voltage coarse adjustment potentiometer on the voltage regulator has
been disturbed, set it at center position (halfway between full clockwise position and full
counterclockwise position). (7) Check control panel lights circuit breakers by pressing panel “LAMPS” push button switch. If
panel lights operate, the circuit breaker, switch, and lamps are good.
(8) Check fault indication lights by pressing “TEST/RESET” push button switch. If fault code display
lights up, the control circuit breaker is good.
(9) Make a general inspection of all wiring, and terminals. Inspect the equipment to be certain no
damage will result from starting the engine.
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1. Engine Coolant Temperature Gauge (M24)
2. Running Time Meter (M4)
3. Battery Voltmeter (M5)
4. Fuel Gauge (M13)
5. Oil Pressure Gauge (M25)
6. Frequency Meter (M3)
13. Panel Light Switch (S74)
14. Air Intake Heater Switch (S79)
15. Engine Start Switch (S24)
16. AC Output No. 1 Switch (S75)
17. AC Output No. 2 Switch (S275)
7. AC Generator Voltmeter (M2)
8. AC Generator Ammeter (M1)
9. Fault Code Meter (M6)
10. DC Voltmeter [Optional with TR]
11. DC Ammeter [Optional with TR]
12. Front LED Display (A5)
18. DC Output Switch (S430) [Optional with TR]
19. DC Starting Current Switch (S431) [Optional with TR]
20. Engine Stop Switch (S76)
21. Test/Reset Switch (S77)
22. Meter Selector Switch (S3)
Figure 1: Operator Controls
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b) Operational Test Procedures
(1) Start the engine in accordance with instructions in Section 1-3. (2) Check operation of engine instruments; ammeter, coolant temperature indicator, oil pressure
gage and hour meter. (3) Check engine idle speed. Should be 1000 +/- 25 RPM. NOTE: A stroboscope may be required for this check. (4) Again check for oil, fuel, and coolant leaks and correct any leaking condition
. (5) Position switches and controls for automatic voltage regulation and power delivery as follows:
a Place regulated-diagnostic switch in “REGULATED” position.
b Place EF Bypass switches in “BYPASS / OFF” position.
c If the output voltage coarse adjustment potentiometer on the voltage regulator has been
disturbed, place the knob at mid-range position.
(6) Bring the engine up to rated speed, which also energize the generator, by pressing the “ENGINE
START” push button switch a second time. If the engine comes up to rated speed and a 115 V voltage value appears on the voltmeter, the engine ECM and excitation circuits are functioning.
(7) After generator overhaul or repair, the Regulated/Diagnostic switch must be placed in the
DIAGNOSTIC” position for 3 to 5 seconds to re-magnetize the exciter. Then return the switch to
the “REGULATED” position after voltage has built-up. (8) Observe frequency meter. If engine speed is properly set, frequency should read 400 Hz. (9) Obs erve vo ltmeter. Use output fine voltage coarse adjustment potentiometer to adjust voltage to
115 V AC. (10) Check adjustable voltage range.
a Observe voltmeter and turn output voltage coarse adjustment potentiometer to full clockwise
position. Maximum voltage should be 134 volts or higher.
NOTE: If voltage should decrease when regulator potentiometer is turned clockwise, it indicates that internal wiring in the voltage regulator is incorrect. Replace complete voltage regulator assembly.
b Observe voltmeter and turn regulator potentiometer knob to full counterclockwise position.
The minimum voltage should be 95 volts or lower.
(11) Position load bank switches, etc., to apply a light load to the generator.
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Figure 2: Control Box Interior Components
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c) Testing the No. 1 Output Circuit
(1) Place EF Bypass switch in “BYPASS / OFF” position turn the EF signal “ON” on the load bank.
Then press the yellow No. 1 load contactor push button switch to close contactor, which is indicated when its internal indicating light glows.
(2) Place EF switch on the load bank in the off position. The No. 1 load contactor should open
immediately, and the indicating light within the push button switch should go off. The fault code display should also read “EF 1”, indicating an EF warning. This is because the interlock circuit of the control PC board is not receiving 28.5 VDC signal from an outside source. It indicates that the No. 1 interlock circuit is OPEN, as it should be when the interlock circuit is not receiving a 28 VDC signal. Reset the fault by pressing the “TEST/RESET” push button.
(3) Verify that when the EF Bypass switch is in the “BYPASS / ON” position or the “BYPASS / OFF
position that the appropriate LED indication on the control panel display is correct.
(4) Place EF bypass switch in “BYPASS / ON” position. Press the No. 1 load contactor push button
switch. The No. 1 contactor power indicating light within the push button switch should glow and remain on when the push button switch is released. This indicates that EF bypass switch is functioning correctly. The corresponding LED should also indicate the bypass mode.
Figure 3: Digital Control PC Board
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EF Bypass Indication
(5) Place the No. 1 EF bypass switch to “BYPASS / OFF” position. The No. 1 load contactor should
open at once and the yellow indicating light within the No. 1 load contactor push button switch should go off and the fault code display should also read “EF 1”, indicating a EF warning. The corresponding LED should also indicate the EF present mode. Reset the fault by pressing the “TEST/RESET” push button.
(6) Proceed to step 12.
(Steps 8 - 11 are only required if EF interlock system is not available on a load bank.)
(7) Connect a source of 24 V-DC power (two twelve-volt batteries connected in series) to terminals
N, F (or E) at the output terminal panel. Connection polarity is important. Connect plus (+) to terminals E or F, and minus (-) to terminal N.
(8) Verify that when the EF Bypass switch is in the “BYPASS / ON” position or the “BYPASS / OFF
position that the appropriate LED indication on the control panel display is correct during the following steps 9 and 10.
(9) Place the No. 1 EF bypass switch to “BYPASS / OFF” position. Press the No. 1 contactor
operating push button switch. The No. 1 contactor power on indicating light, within the push button switch, should glow and remain on when the push button switch is released. This indicates that the load contactor is closed and the plug interlock circuit is functioning properly.
(10) Disconnect the 24 V-DC power source and the No. 1 load contactor should open immediately,
and the indicating light within the push button switch should go OFF. The fault code display should also read “EF 1”, indicating an EF warning. This is because the interlock circuit of the control PC board is not receiving 28.5 VDC signal from an outside source. It indicates that the No. 1 interlock circuit is OPEN, as it should be when the interlock circuit is not receiving a 28 VDC signal. Reset the fault by pressing the “TEST/RESET” push button.
Figure 4: EF Bypass Indication
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(11) In EF bypass mode, apply 1/3 to 1/2 load at the load bank and allow the unit to run for 15 to 30
minutes. Observe operation of all monitoring instruments. (12) Increase load at the load bank to full load. (13) Check operation of the engine ECM by observing the frequency meter when generator is
switched from no load to full load, and vice versa. Use the No. 1 contactor control push button
switch to apply and remove load several times. Steady-state frequency droop should be no more
than 1 Hz. (14) Follow instructions in Paragraph 3 to set voltage regulator line-drop compensation for the length
and size of cable being used. (15) Check voltage regulator, at intervals, from no load to full load. Observe and note voltage at
various loads. Steady-state voltages should vary no more than +/- 1% from normal output
voltage. (16) Operate the No. 1 output circuit of the unit no less than 10 minutes under full load. The overload
protection MUST NOT trip. (17) Operate the No. 1 output circuit of the unit at 125% load (325 amperes) for 5 minutes immediately
following the full load run. The overload device MUST trip within 5 minutes, and the fault code
display should read “70.18” indicating an overload condition in “OUTPUT NO 1” (Reference fault
chart in Section 2-4). (18) Reset the fault by pressin g “ TEST/RESET” push button.
d) Testing the No. 2 output circuit
(1) Repeat steps (1) through (18) in the previous section “Testing the No. 1 Output Circuit” for
testing the No. 2 output circuit.
e) Testing and checking meters, switches, protective monitoring circuits, and fault code display
(1) Check accuracy of AC voltmeter
a Open door of control box and connect a master voltmeter of known accuracy to terminals of
the AC voltmeter.
b Compare the unit’s voltmeter reading with master meter. Error must not exceed 2% of full
scale.
(2) Check accuracy of AC ammeter
a Connect a master ammeter of known accuracy to the AC ammeter. b Compare the unit’s ammeter reading with master meter under various loads. Error must not
exceed 4% of full scale.
(3) Check operation of the “METER SELECT” switch.
a In any LINE-TO-NEUTRAL position, the voltmeter reading should be 115 volts when the LED
under the voltmeter indicates one of the 3-phase being checked.
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b In any LINE-TO-LINE position, voltmeter reading should be 200 volts when the LED under
the voltmeter indicates two of the phases being checked.
(4) Check accuracy of frequency meter
a Connect a master frequency meter of known accuracy to the terminals of the frequency
meter.
b Compare meter readings. Error must not exceed 1% of full scale. NOTE: Make all protective system tests with the unit operating under a load for the following steps.
(Reference Chapter 2, Section 4, for all fault codes)
(5) Check operation of over-voltage circuit and fault code display.
a With the unit running at a normal load, adjust the coarse adjustment potentiometer on the
voltage regulator clockwise to increase voltage until the over-voltage sensing circuit actuates the protective monitor. After the protective monitor is activated, the load contactor will open and the fault code di splay will display fault “70.16”. At 125 volts, the circuit will trip after a 1- second time delay. At higher values of voltage, time delays for over voltage trips are as follow:
At 140 volts, the circuit will trip within 160 millisec on ds.
At 180 volts, the circ u it wi ll tr ip w ith in 50 milliseconds .
b If the load contactor does not open under the conditions described in step (a), refer to the
Troubleshooting Chart in Section 2-4.
c Return unit to normal operating conditions by adjusting coarse adjustment potentiometer
(turning it counterclockwise) and pressing “TEST/RESET” button switch to clear the fault code.
(6) Check operation of under-voltage circuit and fault code display.
With the unit running at a normal load, adjust the coarse adjustment potentiometer on the voltage
regulator counterclockwise to decrease voltage until the under-voltage sensing circuit actuates
the protective monitor. After the protective monitor is activated, the load contactor will open and the fault code display will display fault “70.17”. Follow the following steps below to activate the under-voltage protective monitor. A stopwatch is required for this check.
a With the unit running at normal load, use the output voltage coarse adjustment potentiometer
on the voltage regulator to reduce the voltage to 104 volts. The load contactor should NOT open.
b Reduce voltage in increments of 1 volt, with a time delay of 7 seconds between steps. At a
setting of 100 volts, the load contactor will open and the under voltage light will glow after a 7­second time delay.
c If the load contactor does not open under the conditions described, refer to the
Troubleshooting Chart in Section 2-4.
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d If the under voltage circuit performs satisfactorily, return unit to normal operation by adjusting
output voltage coarse adjustment potentiometer for normal output voltage, pressing the “TEST/REST” push button switch to clear the fault code.
(7) Check under-frequency circuit and fault code display.
At some frequency value 380 Hz or less, after 7 seconds, the frequency condition should signal
the under-frequency circuit protective monitor to OPEN the load contactor and display “70.23” on
fault code display. To check the under-frequency protective components, proceed as follows:
a While the unit is operating normally under load, set the frequency adjust switch to “TEST”.
Rotate the frequency adjust potentiometer to adjust frequency to 400 HZ. b Reduce frequency in steps of 1 Hz, with a time delay of 7 seconds between steps. c If the protective circuit opens the load contactor and displays fault “70.23” on the fault code
display after 7 seconds, at 380 Hz or less, all components of the system are functioning
properly. d If the load contactor is not opened at 380 Hz or less after 7 seconds, refer to Troubleshooting
Chart in Chapter 2, Section 4. e Return unit to normal operating condition by setting the frequency adjust switch to
NORMAL” and pressing “TEST/RESET” button switch to clear fault code.
Figure 5: Engine Specific PC Board
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(8) Check over-frequency circuit and fault code display.
At some frequency value 420 Hz to 440 Hz, after 5 seconds, the over frequency sensing circuit should signal the over-frequency circuit protective monitor to OPEN the load contactor and display “70.22” on fault code display.
At any frequency value exceeding 440 Hz, the over-frequency circuit should immediately signal the protective monitor to OPEN the load contactor and display “70.22” on fault code display...
To check the under frequency protective components, proceed as follows: a While the unit is operating normally under load, set the frequency adjust switch to “TEST”.
Rotate the frequency adjust potentiometer to adjust frequency to 400 HZ. b Increase frequency in steps of 1 Hz, with a time delay of 5-7 seconds between steps. c If the protective circuit opens the load contactor and displays fault “70.22” on the fault code
after 5 seconds at 426 Hz, all components of the system are functioning properly. d If the load contactor is not opened at 426 Hz after 5 seconds, refer to Troubleshooting Chart
in Chapter 2, Section 4. e Return unit to normal operating condition by setting the frequency adjust switch to
NORMAL” and pressing “TEST/RESET” button switch to clear fault code.
NOTE: If the generator is operating under load at this point, open the contactors. There will be no further need for the load bank in the following checks.
f) Testing for engine ECM faults
(1) Set the starter enable/disable switch to “DISABLE”. “DISABLE” will prevent the engine from
starting, but will still supplying 12 VDC to the control system, while checking the ECM faults.
(2) Press the green “ENGINE START” push button switch. Although the en gin e is not runni ng, the
green light in the “ENGINE START” switch will flash to indicate that power is available to the engine ECM.
(3) If no active codes are recorded, both the “Engine Stop” and “Check Engine” lamps will come on
and stay on. If active codes are recorded, both lamps will come on momentarily and then begin to flash one
code of the recorded faults.
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Figure 6: Engine Interface PC Board
(4) The fault code will flash in the following sequence:
First, a “Check Engine” (yellow) lamp will flash. There will be a short 1- or 2-second pause after which the number of the recorded fault code will flash in the “Engine Stop” (red) lamp. There will be a 1- or 2-second pause between each number. When the number has finished flashing in the red lamp, the yellow lamp will appear again. The fault code will repeat in the same sequence.
The lamps flash each fault code 3 times before advancing to the next code. To skip to the next fault code, move the Engine Codes Switch momentarily to the UP position. You can go back to the previous fault code by momentarily moving the Engine Codes Switch to the DOWN position. If only one fault is recorded, the QSB control system will continuously display the same fault code when the Engine Codes Switch is moved to either the UP or DOWN position.
(5) See engine manufacture’s manual for code meanings.
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g) Re-checking the entire unit after testing
(1) With the engine running at normal rated speed, check the entire unit for vibration and for any
parts that may have become loosened during the above checks. Tighten any loose hardware as required.
(2) Check engine oil pressure at rated speed (2000 RPM). The oil pressure gage should indicate at
least 44.9 psi (3.1 bar) when engine is hot. Also at rated speed, check the engine coolant temperature. The temperature gage should indicate in the range of 180° to 190° F (82º to 88º C), depending upon operating c onditions.
WARNING
(3) Check 400 Hz generator bearings. Use a stethoscope or metal sounding rod to listen for unusual
noises. If using a metal rod, place on end on the generator housing and hold the other end near the ear. Hold the rod with three fingers and use the index finger and thumb to form a sounding chamber between the rod and the ear. Do NOT allow the rod to touch the ear. Listen for grinding or pounding sounds, which would indicate a defective bearing. An engine noise may be telegraphed to the generator and misinterpreted as a generator noise. Contact the equipment manufacturer if in doubt of bearing serviceability.
If a metal sounding rod is used to detect bearing noises, exercise extreme care to avoid injury from moving components.
3) Generator Set Adj ustmen t
a) Generator Adjustment
The 400 Hz generator is a brushless type requiring no adjustments of any kind.
b) Adjust 400 Hz voltage regulator.
When a voltage regulator is first put into service, or when output (generator-to-aircraft) cables are changed, the regulator may require adjustments of output voltage value and line-drop compensation. For making these adjustments, the voltage regulator has three potentiometers:
A coarse output voltage potentiometer
A fine output voltage potentiometer
A line-drop compensation potentiometer
For the following adjustment, the generator set must be running at rated speed (2000 RPM), under no-load conditions. Adjust the regulator as follows:
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Figure 7: Voltage Regulator PC Board
(1) Output Vo lta ge Adjus tment
a Adjust Voltage Control
The output voltage, at which the generator is regulated, is adjustable by the fine voltage
adjustment potentiometer. Turn the potentiometer adjustment clockwise to increase
generator output voltage, and counterclockwise to decrease voltage.
Observe the output voltage as indicated by the voltmeter, located on the control panel of the
generator set. Set output voltage at 115-V AC line-to-neutral (200-V AC line-to-line).
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b Adjust Line-Drop Compensation
Adjustment of line-drop compensation is made with the line-drop compensation
potentiometer. Turning the potentiometer knob clockwise increases the magnitude of the
compensation, and turning the pote nti ometer knob counterclockwise dec reas es th e
magnitude (A graduated nameplate for specified cable lengths is included for quick
reference.). To adjust the line-drop compensation, proceed as follows:
(i) Connect the generator set output cables to a load. Load the generator set with the
largest available three-phase load of rated power factor not exceeding the maximum rating of the generator set.
(ii) Measure output voltage at the load end of the cables. If the load voltage rises or drops
more than 1% at the load end of the cables, decrease or increase the line-drop compensation until the regulation is flat (115-V AC line-to-neutral and 200-V AC line-to­line).
(iii) If the line-drop compensation adjustments have affected the no-load voltage output,
adjust the fine output voltage control potentiometer to the desired value.
(2) Test the Voltage Regulator
After necessary adjustments have been completed, re-test the voltage regulator as follows: a Connect a voltmeter at the load end of the generator output cables. b Operate the generator set at no-load and observe voltage reading. c Operate the generator set under load and observe voltage reading. d Voltage under load and no load should vary no more than 1% at the load end of the cables.
c) Basic Engine Adjustments
Adjustment procedures applicable to the diesel engine are included in the engine manufacturer’s operation manual, which is referenced in Chapter 5. Refer to the engine operation manual for detailed information on the follow ing engin e adj us tments.
NOTE: A stroboscope is required for engine idle speed checks. Engine idle speed is programmed at the factory. If adjustment is required, contact the local engine
distributor. The recommended idle speed is 1000 RPM, +/- 25 RPM. The speed limiting adjustment is also set and sealed at the factory. Speed should be limited to
approximately 2350 RPM. If adjustment is required, contact your local engine distributor.
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Generator Stator Phase A to N (G1)*
0.0026
Generator Stator Phase B to N (G1)*
0.0026
Generator Stator Phase C to N (G1)*
0.0026
Exciter Stator Field (L2)
29
A - B, B - C, C - A Exciter Armature (G2)
0.041
Generator Revolving Field (L1)
2.1
*NOTE: The two leads of a phase must be connected when test is made. Take readings when unit is cold and in an ambient temperature of 70 ºF (21ºC.).
d) Engine Accessories Adjustment
Alternator and fan belt adjustment: Refer to Section 2-1 and engine manufacturer manual.
4) Generator and Exciter Test
The generator fields and exciter stator may be tested with a Kelvin bridge. This is a double-bridge type instrument required for the very low resistance’s encountered in this test. It is understood that zero (0) resistance indicates a SHORT CIRCUITED condition. An infinite resistance reading indicates an OPEN CIRCUITED condition.
a) Disconnect generator stator leads at the output module panel. b) Disconnect the two black exciter field leads from terminal block mounted on output module panel. c) Check resistance and compare to values.
Test Connection Resistance (Ohms)
Figure 8: Generator and Exciter Test Readings
Figure 9: Generator Connections
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5) Diode Test
Test values for diodes are not given here because they could be misleading. Test values may vary even between diodes of the same part number, rating, and manufacturer. General instructions for testing diodes are as follows:
a) Disconnect exciter windings from diode lead(s). b) Use a good quality ohmmeter. An instrument, which indicates 50 ohms at the center of the scale, is
preferable.
NOTE: Make certain the battery is in good condition and the pointer is adjusted to zero when the test lead points are shorted together.
c) Hold one ohmmeter lead point on the threaded end of the diode. Hold the other lead point on the
wire terminal end. Observe and note the indicated resistance. Now reverse the lead connection on the diode. Again observe and note the ohmmeter indicated resistance. Generally speaking, if an infinite or very high resistance was indicated with the leads connected one way and a low, readable resistance was indicated with the leads connected the opposite way, the diode may be considered good.
6) Testing the Transformer-Rectifier (for units with the DC option)
The 28.5-VDC transformer-rectifier is an optional add-on to the GPU. The following test procedures may be used for testing the T-R following repair, or for just checking performance.
a) Preparation for Testing
(1) Connect the T-R to a load bank. (2) Start the GPU per the operating procedures in Chapter 1, Section 3.
b) Operational Test Procedure
(1) Power Del i ver y
a Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp will glow indicating that DC power is being delivered to the load bank. b Observe the DC voltmeter on the control panel, under no load for accuracy. It should indicate
approximately 28.5 VDC. c With the GPU connected to a load bank, place a 600 A load on the GPU. Observe the DC
voltmeter and ammeter for accuracy.
(2) Discontinue Power Delivery
Press “DC OUTPUT” push button to open the DC output contactor. The blue “DC OUTPUT” lamp
will not glow indicating that DC power has been removed from the load bank.
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(3) Current Limiting / Soft Starting Control
a Press the “STARTNG CURRENT” push button to activate the current limiting and set the limit
to 1500 A. b Press the “DC OUTPUT” push button to close the contactors to apply the load to the load
bank. Observe the ammeter, the current should stay below 1500 A. c Discontinue the power delivery.
(4) Over-Voltage Protection
a Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp will glow indicating that DC power is being delivered to the load bank. b Adjust the voltage adjustment potentiometer on the TRB PC Board to range of 32-34 VDC. c With 7 to 9 seconds after the trip voltage is reached, the contactor will open and an over-
voltage fault will be indicated on the fault code meter, which will read “70.28” d Reset the voltage back to 28.5 VDC.
(5) Under-Voltage Protection
a Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp will glow indicating that DC power is being delivered to the load bank. b Adjust the voltage adjustment potentiometer on the TRB PC Board to less than 20 VDC. c With 7 to 9 seconds after the trip voltage is reached, the contactor will open and an under-
voltage fault will be indicated on the fault code meter, which will read “70.29” d Reset the voltage back to 28.5 VDC.
(6) Overlo ad Prot ec tio n
a Press the “STARTNG CURRENT” push button to activate the current limiting and set the limit
to 1500 A. b Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp will glow indicating that DC power is being delivered to the load bank. c The contactor should open in 30 seconds. The fault code meter will read “70.30” d Discontinue power delivery and let the cables cool for 2-3 minutes. e Press the “STARTNG CURRENT” push button to activate the current limiting and set the limit
to 2000 A. f Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC O UT PUT
lamp will glow indicating that DC power is being delivered to the load bank.
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g The contactor should open in 10 seconds. The fault code meter will read “70.30” h Discontinue power delivery and let the cables cool for 2-3 minutes.
(7) Temperature Overload Protection
a Press “DC OUTPUT” push button to close the DC output contactor. The blue “DC OUTPUT
lamp will glow indicating that DC power is being delivered to the load bank. b Remove one wire from the thermostat switch located on the right side of the T-R heat sink.
This will open the switch, thus simulating an over temperature fault. The fault code meter will
read “70.44
(8) Silicon Diodes
a Shut the GPU completely down removing all power from the system. b Disconnect diode leads. c Use a good quality ohmmeter, place one ohmmeter lead on the threaded end of the diode
and the other lead on the diode lead and the record value. d Reverse the ohmmeter leads and record the value. e The diode may generally be considered good if one reading is infinite or very high and the
other reading is extremely low.
(9) Control Interlock Kit (Optional)
a With the output cable sitting in the cable tray, start the GPU and bring the engine to rated
speed. b Close the output contactor by pressing the “DC OUTPUT” push button. The output contactor
should open immediatel y with an “EF3” warning displayed on the fault code meter. c Using a 28 VDC power source, apply a 28 VDC signal to the control socket of the output
cable (small socket). d Close the output contactor by pressing the “DC OUTPUT” push button. The output contactor
should stay closed. e Remove the 28 VDC power source and the contactor should open with an “EF3” warning.
7) Adjusting the Transformer-Rectifier (fo r units with DC option)
The T-R is design to be adjustment free. No adjustments required, other than periodically checking the output voltage and adjusting the TRB PC board potentiometer as necessary.
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