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 accordance 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 maintenance under the supervision of trained personnel.
2. This warranty expires 15 months after shipment by HOBART to the first user, or 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 (gasoline or diesel),storage
batteries, engine starters generators, alternators, regulators, governors, tires, axles,transmissions,and cable
retrieving devices. Many of the foregoingcomponents 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 manufacturerhas warranted its component to HOBART and will not deal 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. HOBART’S liability is limited to repair of any defects found by HOBART to exist, or at HOBART’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, orfor a period of ninety (90) days, whichever is greater.
7. UNDER NO CIRCUMSTANCES whatsoever shall HOBART and its authorized 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 in writing, this warranty does not cover any equipment that has been altered by any party
other than HOBART.
10. THERE ARE NO WARRANTIES WHICH EXTEND BEYOND THE DESCRIPTION ON THE FACE HERE OF.
HOBART MAKES NO WARRANTIES, EXPRESSED OR IMPLIED, OF ERCHANTABILITY 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.
AT ALL TIMES, SAFETY MUST BE CONSIDERED AN IMPORTANT FACTOR IN THE INSTALLATION,
WARNING
SERVICING AND OPERATION OF THE PRODUCT, AND SKILLED, TECHNICALLY QUALIFIED PERSONNEL
SHOULD ALWAYS BE EMPLOYED FOR SUCH TASKS.
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
Safety Warnings and Cautions
WARNING
WARNING
IMPORTANT
1.
General
Equipment that supplies electrical power can cause serious injury or death, or 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.
Shock Prevention
2.
Bare conductors, or 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 equipment, do not work in damp areas. Stand on a dry rubber
mat or dry wood, use insulating gloves when dampness or sweat cannot be avoided. Keep clothing dry,
and never work alone
CALIFORNIA PROPOSITION 65 - DIESEL ENGINES. Diesel engine exhaust
and some of its constituents are known to the State of California to cause
cancer, birth defects and other reproductive harm.
ELECTRIC SHOCK can KILL. Do not touch live electrical parts.
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 attached equipment.
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.
a. Installation and Grounding of Electrically Powered Equipment
Equipment driven by electric motors
and maintained in accordance with the National 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 3-phase line. DO NOTCONNECT 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.
November 27/1997Safety Warnings
(rather than by diesel or gasoline engines)
must be installed
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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
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. 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.
Service and Maintenance
3.
This equipment must be maintained in good electrical and mechanical 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 electrically-powered equipment, take the following precautions:
a. Shut OFF all power at the disconnecting switch or line breaker before inspecting or servicing
the equipment.
(amperage)
b. Lock switch OPEN
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
piping, misuse of batteries and fuel, or unsafe operating or fueling conditions.
a. Electrical Short Circuits and Overloads
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 removing fuel tank cap. DONOT 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.
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.
Bodily Injury Prevention
6.
Serious injury can result from contact with fans inside some equipment. Shut DOWN such equipment
for inspection and routine maintenance. When equipment is in operation, use extreme care in doing
necessary trouble-shooting and adjustment. Do not remove guards while equipment is operating.
(or remove line fuses)
so that power cannot be turned on accidentally.
Safety WarningsNovember 27/1997
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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 victims. Electric shock victims should be checked by a physician and taken to a
hospital immediately if any abnormal signs are observed.
EMERGENCY
FIRST AID
8.
Equipment Precautionary Labels
Inspect all precautionary labels on the equipment monthly. Order and inspect all labels that cannot be
easily read.
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.
November 27/1997Safety Warnings
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Safety WarningsNovember 27/1997
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Introduction
This manual contains operation and maintenance information for a Hobart generator set manufactured
by Hobart Brothers Company, Ground Power Division, Troy, Ohio 45373.
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 who have
never operated this equipment. It is the intent of this manual to guide and assist operators and
maintenance people in the proper use and care of the equipment.
Use of the manual should not be put off until a trouble or 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.
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, its location is identified by a
chapter, section, and paragraph or figure number.
For example: “
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: “
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.
Appendix A contains a list of options and corresponding TO documents. If the machine purchased
contains one of these options, the corresponding TO will be inserted in this section.
Content of the manual is 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 Literature
Appendix A. Options / Features
(see Section 2-3, Paragraph 1.a.)
” refers to information located in Chapter 2, Section 3,
(see Paragraph 1.a.).
”
IntroductionNovember 27/1997
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November 27/1997Introduction
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Table of Contents
Chapter-SectionPage
Chapter 1. Description / Operation
Section 1. Description1-11
General1-11
Orientation1-11
Optional Equipment1-11
Special Features1-11
Protective Monitor1-11
Voltage Regulator1-11
Electric Governor1-11
Section 2. Preparation for Use, Storage or Shipping1-21
Preparation for Use1-21
Inspection/Check1-21
Installing Three-phase AC Output Cables1-22
Preparation for Storage1-23
General1-23
Temporary Storage1-23
Long Time Storage (Over 30 Days)1-23
Preparation for Shipment1-24
November 27/1997Table of Contents
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Section 3. Operation1-31
General1-31
Operating the Unit1-31
Pre-start inspection1-31
Normal Engine Starting Procedures1-31
Failed Starting Procedures1-34
Power Delivery1-34
Discontinue Power Delivery with Unit Shutdown1-35
Chapter 2.Servicing
Section 1. Maintenance Inspection/Check2-11
General2-11
Maintenance Schedule2-11
General2-11
Maintenance Schedule Check Sheet2-11
Time Intervals2-11
Identification of Interval Periods2-11
Inspection/Check2-14
General2-14
“AR” Checks and Operations (As Required)2-14
“BR” Checks and Operations (Break-In Period)2-14
“A” Checks and Operations (10 Hours or Daily)2-15
“B” Check and Operations (250 Hours or 3 Months)2-17
“C” Checks and Operations (500 Hours or 6 Months)2-17
“D” Checks and Operations (1000 Hours or 1 Year)2-18
“E” Checks and Operations (1500 Hours or 1 ½ Years)2-18
“F” Checks and Operations (2000 Hours or 2 Years)2-110
Seasonal Maintenance Checks (Engine)2-111
Lamps and Circuit Breakers2-112
Section 2. Maintenance Procedures2-21
General2-21
Lubrication2-21
General2-21
AC Generator2-21
Generator Controls2-21
Engine2-21
Engine Accessories Lubrication2-25
Servicing the Air Cleaner2-26
Inspecting the Air Cleaner2-26
Changing the Air Filter2-26
Disposal2-26
Table of ContentsNovember 27/1997
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Engine Fuel2-27
How to Select Fuel—Quality2-27
Cold Weather Operation2-27
Reassemble Engine and Generator3-210
Run-in and Periodic Check3-210
Section 3. Generator Assembly3-31
General3-31
Procedure for Generator Assembly Removal3-31
Procedure for Gaining Access to the Generator3-31
Removing the generator Assembly3-33
Installing a Generator Assembly3-34
Remounting the Generator Assembly3-34
Remounting the Previously Removed Assemblies3-34
November 27/1997Table of Contents
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Chapter 4.Illustrated Parts List4-11
Section 1. Introduction4-11
General4-11
Purpose4-11
Arrangement4-11
Explanation of Parts List4-11
Contents4-11
Parts List Form4-11
Section 2. Manufacturer’s Codes4-21
Explanation of Manufacturer’s (Vendor) Code List4-21
Section 3. Illustrated Parts List4-31
Explanation of Parts List Arrangement4-31
Symbols and Abbreviations4-31
Section 4. Numerical Index4-41
Explanation of Numerical Index4-41
Numerical Index4-41
Chapter 5.Manufacturer’s Literature5-11
Appendix A. Options/FeaturesAppendix A1
Unusual Service Conditions
Wet Stacking
Table of ContentsNovember 27/1997
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Chapter 1. Description / Operation
Section 1. Description
1. General
The basic generator set covered in this manual is manufactured by Hobart Brothers Company, Ground
Power Division, in Troy, Ohio. It is rated at 90 KVA and is designed to produce and deliver
115/200-volt, 400 Hz, 3-phase AC power to a parked aircraft or to Hobart approved test banks only.
Series 500392 consists of the following part numbers:
Part Number 500392-001 identifies a single output unit structured* for trailer mounting.
Part Number 500392-002 identifies a dual output unit structured* for trailer mounting.
Part Number 500392-003 identifies a single output unit structured* for fixed/truck mounting.
Part Number 500392-004 identifies a dual output unit structured* for fixed/truck mounting.
Part Number 500392-005 identifies a single output trailer mounted unit similar to 500392-001. A
list of other features that make the 500392-005 unique is located with the Appendix in the back
of this manual.
*In this manual, part numbers 500392-001 and 500392-003 are identical (single output) units.
Part numbers 500392-002 and 500392-004 are identical (dual output) units. The difference
between the units are the options available for them. For example, a fixed/truck mounting kit is
not available for part numbers 500392-001 or 500392-002. See Appendix A.
Orientation
2.
For purpose of orientation, the radiator is considered to be at the REAR of the unit. The generator and
controls are at the FRONT. RIGHT and LEFT are determined by standing at the REAR end facing the
machine. Thus, the control box is mounted on the LEFT side at the FRONT of the unit.
Optional Equipment
3.
Chapters 1 through 5 of this Operation and Maintenance Manual identifies only the “strip down” version
of the 90CU24 generator set. A list of optional equipment which make this manual unique to the
generator set that you have purchased, appears in Appendix A. A few items included in Appendix A
are cable trays, trailers, 28-volt DC power transformer-rectifiers, etc.
Special Features
4.
The generator set has special features in which are described more fully under assemblies in which
they appear. Three features, protective monitor, voltage regulator, and electric governor are mentioned
here and described briefly.
a. Protective Monitor
The protective monitoring system receives signals from the fault sensing units 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 regulator is also adjustable for a variety of output cable sizes and lengths.
November 27/1997Chapter 1-1
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90CU24 / Series 500392 Generator Sets
1. Control Panel
2. Output Cable Clamps
3. Frame
4. Emergency Stop Switch
5. Canopy
6. Radiator Access Door
Generator Set
Figure 1
Chapter 1-1November 27/1997
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90CU24 / Series 500392 Generator Sets
c. Electric Governor
The engine is equipped with an electric governor kit and other special equipment more fully
described under the engine description.
Canopy
5.
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.
PhysicalBasic Unit
Length100 in. (2540 mm)148 in. (3759 mm)
Width45 in. (1143 mm)77 in. (1956 mm)
Height47.5 in. (1203 mm)61 in. (1549mm)
Weight with T-R6700 lb. (3039 kg)
Weight of optional T-R300 lb. (136 kg)Not applicable
Generator
Output power rating (kVA)
Output Voltage115/200 Volts
Rated load capacity (Amps)260 Amps
Frequency (Hz)400 Hz
Output kilowatts72
Power factor0.8
Duty cycle100%
Operating speed (RPM)2400 RPM
Overload capacity, both outputs:
125% rated load (Amps)
Output cable size2/0
Over voltageTrips at 126 volts after a 1-second time delay
Under voltageTrips at any voltage below 100 volts after 7 seconds.
Over frequencyTrips at any value between 426-Hz and 480-Hz after a 5-second
Under frequencyTrips at 375-Hz or less after a 5-second time delay.
Overload time delayTrips in approximately 5 minutes at 125% load on either or both
90 kVA
325
Generator Protective System
Trips at 140 volts in 160 milliseconds.
Trips at 180 volts in 50 milliseconds.
time delay. Trips immediately at any frequency exceeding 480-Hz.
outputs.
With Trailer
Specifications and Capabilities
Figure 2
November 27/1997Chapter 1-1
(Sheet 1 of 2)
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ManufacturerCummins Engine Company, Inc.
Model No.6BT5.9C165
TypeIn-line 6 cylinder 4 Cycle Diesel
Bore and Stroke4.02 x 4.72 inches (10.2 x 11.9 cm)
Displacement359 c.i. (5.9 liters)
Compression Ratio17.5 : 1
Horsepower165
Idle speed850+/-50 RPM
High speed limitingApprox. 2750 +/-75 RPM
Normal governed speed2400 RPM
Electrical system12-V DC
GroundNegative
Firing order (RH rotation)1-5-3-6-2-4
Lubricating oil capacity (w/filter)16 quarts (15.1 liters)
Coolant capacity system38 quarts (36 liters)
Engine
Columbus, Ohio 47201
Specifications and Capabilities
Figure 2 (Sheet 2 of 2)
Engine and Generator
6.
The engine and generator comprise the principal components of the generator set. They are mounted
on the welded steel frame of the chassis. The engine coolant radiator is also mounted on the frame just
forward of the engine-generator combination. Figure 3 is an illustration showing the location of all major
components and sub-assemblies.
a. Basic Engine.
The basic engine is an in-line 6-cylinder diesel rated at 165 horsepower. See Fig. 2 for general
specifications.
b. Engine Manufacturer’s Equipment
As received from the engine manufacturer, the engine includes the following equipment which is
more fully described in the Cummins Operation and Maintenance Manual.
(1)
Electrical System
The 12-V DC electrical generating and starting system includes an alternator, voltage regulator,
and starter with solenoid switch.
(2)
Fuel Filter
The fuel filter is a spin-on disposable, vacuum type connected between the fuel lift pump and
injector pump
(3)
Oil Filter
The engine oil filter is a spin-on, full-flow type. It is mounted on the right side of the engine.
Chapter 1-1November 27/1997
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90CU24 / Series 500392 Generator Sets
5
7
9
1
86
4
2
1. Radiator
2. Engine
3. Generator
4. Air Cleaner
5. Control Box
Generator Set Components
Figure 3
November 27/1997Chapter 1-1
6. Output Module Panel
7. Engine-Generator Control Panel
8. Mounting Frame
9. Muffler
3
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90CU24 / Series 500392 Generator Sets
(4)
Engine over-speed protection
The engine is protected against over-speed by a speed-limiting mechanism in the mechanical
governor.
c. Engine-cooling fan
The engine fan is designed to blow air
inward as a conventional fan does.
Refer to the engine Operation and Maintenance Manual in Chapter 5 for more engine details.
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.
outward through the radiator, rather than pull the air
ENGINE FAULTS
Engine Fault ConditionWhat This Fault Condition Does
Over temperature or low
oil pressure
Low fuelTurns on the low fuel indicating
Clogged air cleaner or
other restriction in the
combustion air inlet.
Automatically removes power
from the electric governor
controller, shuts down the
engine, and turns on the
applicable indicating light.
light (27, Fig. 5). Depending on
the position of JP2 and JP3 on
the control PC board, a low fuel
fault may cause the engine to
idle, shut down, or continue to
run at rated speed.
Turns on the air cleaner
restriction indicating light
(6, Fig. 5)
To Put the Generator Set Back
into Service:
a) Press the engine stop button
(20, Fig. 5) to turn off the
indicating light and reset the
protective system.
b) Or use E-STOP (4, fig. 1)
button for immediate reset.
a) The low fuel fault indicating
function must be reset by
pressing the engine stop button
(20, Fig. 5). Fuel must be
added prior to attempting
another engine start.
b) Or use E-STOP (4, fig. 1)
button for immediate reset.
a) Press the engine stop button
(20, Fig. 5). The restriction
must be removed prior to
attempting another engine start.
b) Or use E-STOP (4, fig. 1) ]
button for immediate reset.
Chapter 1-1November 27/1997
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e. Hobart Installed Equipment
This generator set is modified at Hobart Brothers by the addition of the following equipment:
(1)
Shut Down/Reset device
In addition to the other devices provided by the engine manufacturer, an engine shutdown/reset
feature is added by Hobart Brothers.
a.
EMERGENCY SHUTDOWN/RESET SWITCH (mushroom button).
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 shut off of the generator
set by disconnecting power to the governor circuit through the control box. It is located on
the left side of the generator set on the door near 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
(2)
Engine Safety Devices
In addition to the safety devices provided by the engine manufacturer, other engine shutdown
features are added by Hobart Brothers
a.
Coolant high temperature shutdown system
The coolant temperature shutdown system consists of a Detroit Diesel supplied temperature
switch. This switch controls a relay in the control box, which is in series with the governor
system. This relay will stop the engine if the temperature reaches 220º F (96º C).
b.
Oil pressure shutdown system
The oil pressure shutdown system consists of a Hobart supplied oil pressure switch. This
switch is diaphragm operated and held is closed position by any normal oil pressure above
12 PSI (83 kPA). It is connected in series with the fuel shutoff valve and will open the holding
circuit if the oil pressure drops to 12 PSI (83 kPA) or below.
(3)
Electric governor system
An electric governor kit is installed on the engine to replace a conventional mechanical type.
The electric governor was selected for control of engine speed (and generator output
frequency) because it provides faster engine response to changes in load conditions. This
fast response results in very close frequency control. A brief description is given below:
The governor system consists of the following main components:
a.
Magnetic pickup
The magnetic pickup is a device for detecting the speed of the engine. It is mounted in the
flywheel housing directly over the ring gear. It produces an AC signal to the control unit when
the ferrous flywheel teeth pass through the magnetic field at the end of the pickup.
b.
Control unit
The control unit is a box containing a compact assembly of solid state components. It
receives an AC signal from the magnetic pickup and senses speed changes in the engine. It
provides a voltage signal to the actuator which causes the actuator to move the fuel control
lever as required to maintain a predetermined engine speed. Its power is received from the
12-V DC battery system.
c.
Actuator
The actuator supplies the force needed to move and position the fuel lever as required to
maintain a constant engine speed. The actuator is operated by a DC signal from the control
unit.
November 27/1997Chapter 1-1
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90CU24 / Series 500392 Generator Sets
(4)
Radiator
The radiator is a one-piece type designed for long periods of operation without servicing.
Refer to Section 2-1 for servicing procedure.
(5)
Air cleaner
The diesel-engine air cleaner (fig. 4) is so constructed that air enters through its cylindrical body,
and then is filtered in the process before being passed onto the engine turbo-charge assembly.
An air cleaner service indicator device is mounted on the air cleaner assembly to monitor air flow
in the air cleaner. As the air cleaner becomes filled with dust, dirt, and carbon, the intake system
air flow 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 light (6, Fig. 5) on the engine-generator control
panel is illuminated to warn the operator that the air cleaner must be changed. The electrical
indicator automatically resets after a new air cleaner is installed.
Service Indicator
Air Cleaner
Air Cleaner and
Service Indicator
Figure 4
f. Generator
The 400 Hz generator is a brushless, revolving field, three-phase, alternating current type. The
generator set covered by this manual is a dual-bearing type. The front end of the rotor shaft
extends forward beyond the front bearing and is attached 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 with three diodes is
mounted on the exciter rotor and converts 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 amount of DC voltage supplied to exciter fields by the voltage
regulator. A centrifugal, radial-blade fan which is part of the flexible coupling assembly, draws
cooling air over all internal windings. Air enters at the exciter end and is discharged at the drive
end. The complete generator is bolted to the engine flywheel housing.
Chapter 1-1November 27/1997
Page 8
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
7. Control Box Assembly
The control box is a sheet metal enclosure which houses and provides mounting facilities for engine
and generator controls and monitoring equipment.
a. Control Panel (Fig. 5)
On the door of this control box is the control panel. The control panel is divided into three sections.
On the left side of the control panel, as one faces it, are engine meters and indicating lights. On the
right side of the control panel are generator meters and indicating lights. At the bottom of the control
panel are push-button switches for operating the engine and generator.
(1)
Panel lights and panel light push-button switch
Meters are lighted from inside the control panel. They are controlled by a push-button switch (28)
at the bottom left on the control panel.
(2)
Engine hour meter
The hour meter (5) is electrically driven from the 12-V DC battery system. The hour meter
measures and records engine running time and will record up to 9999.9 hours on five revolving
drums. It is only functional when when the engine is running and the oil pressure safety
shutdown switch, mounted on the engine block, is closed.
(3)
Engine oil pressure gage
The oil pressure gage (7) is an electrical type which 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).
(4)
Engine ON indicating light
When the engine control push-button switch (26) is pressed to start the engine, a green
indicating light within the push-button switch glows.
(5)
Engine coolant temperature gage
The temperature gage (3) is an electrical type which 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 to 240 º F (38 to 116º C).
(6)
Engine start push-button switch
,
This push-button switch (26)
which actuates the solenoid switch to connect power to the engine starting motor. 12-V DC
power is supplied directly to the governor controller and the oil pressure safety 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 pressed a second time, this push-button switch provides a 12-V DC signal to the speed
adjust PC board on the governor controller, which causes the governor actuator to adjust the
engine speed to 2400 RPM. At the same time, a ground signal is provided to the regulator,
enabling the generator to build up voltage for 400-Hz generator output.
Pressing the push-button switch once more removes these signals and the engine reverts to idle
speed.
(7)
Engine stop push-button switch
When the engine stop push-button switch (20) is pressed once, the indicator within the switch
will glow (red). Then a 3 - 5 minute delay will occur to permit the turbo and other engine
components to cool evenly. After the delay, power is disconnected from the governor controller.
This governor actuator will then close and shut off fuel to the engine so the engine can shut
down.
when pressed, connects 12-V DC power to the starter solenoid coil
November 27/1997Chapter 1-1
Page 9
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
1. Fuel Gage
2. Front Panel
3. Engine Coolant Temperature Meter
4. Over Temperature Indicator Light (Red)
5. Engine Hour Meter
6. Indicating Light, Air Cleaner Restriction (Red)
7. Oil Pressure Gage
8. Engine Ammeter
9. Frequency Meter
10. Control Box Label
11. Strip Lights (3)
12. Generator Ammeter
13. Voltmeter
14. Overload Indicator Light
Engine Generator Control Panel
(Dual Output Shown)
Figure 5
Chapter 1-1November 27/1997
Page 10
15. Over Voltage Indicator Light
16. Adjustable Grip Latch
17. Under Voltage Indicator Light (Red)
18. Meter Selector Switch
19. Test-Reset Push-Button Switch (Red)
20. Engine Stop Push-Button Switch
21. Under Frequency Indicator Light (Red)
22. No. 2 Contactor Push-Button Switch (Orange)
23. Over Frequency Indicator Light (Red)
24. No. 1 Contactor Push-Button Switch (Yellow)
25. Low Oil Pressure Indicator Light (Red)
26. Engine Start Push-Button Switch (Green)
27. Low Fuel Indicator Light (Red)
28. Panel Light Push-Button Switch (Yellow)
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
(8)
Engine ammeter
The ammeter (8) indicates the direction and value of current flow from or to the 12-V DC battery.
Its graduated range is from -60 A through O A to + 60 A.
(9)
Engine fuel gage
An electric fuel gauge (1) receives its controlling signal from a sending unit in the fuel tank.
Twelve volt DC operating power is supplied to the fuel gauge when the green engine start
push-button switch (26) is pressed. The fuel level can be checked when the unit isn’t running by
pressing the yellow lamps push-button switch (28)
(10)
Protective system Indicating lights, test and reset push-button switches
The function of this set of five lights (14, 15, 17, 21 and 23)
abnormal condition of over voltage, under frequency, etc., which caused the protective monitor
system to function. Each of the five lights is connected to an actuating circuit within the memory
and time delay module. When one of the circuits is activated, it turns on the applicable indicating
light. The light will remain on until the test/reset push-button switch (19) is pushed. All lamps in
indicating lights may be tested by pressing the test/reset push-button switch. A lamps test should
be performed only when disconnected from a load, as the contactor(s) will open during the test
cycle.
(11)
Engine systems warning lights (red)
Four red indicator lights are illuminated to warn the operator of abnormal engine operations
which must be corrected. These indicators are: The over temperature indicator light (4), air
cleaner restriction indicator
(27). The function of the air cleaner indicator circuit is explained in detail in Para. 6, E, (4).
Generator output monitors
The generator output is monitored by three instruments; a frequency meter (9),a voltmeter (13)
and an ammeter (12). 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
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 selector swit ch (18)
has a 3-1/2-inch face and the scale is graduated 0 to 300 V. The ammeter is also 3-1/2-inch size
and is graduated 0 to 500 A. The amperage value in each of the three phases may be read on
the ammeter by selecting the desired phase with meter selector switch (18)
current transformers, located on the output module (Fig. 9), lower the output load current to a
lesser value, of definite ratio, which will operate the ammeter movement without damage. The
ammeter dial scale is graduated and numbered so that the pointer will indicate the true load
current value rather than the meter movement current.
(13)
Voltmeter-ammeter selector switch
This switch provides a means of selecting and determining which phase of voltage and current is
indicated on the voltmeter and ammeter and whether the voltage is line-to-neutral or line-to-line.
The meter switch (18) is a six-position, rotary type. A nameplate, located under the switch knob,
is marked and lettered to indicate the six functional positions of the meter switch.
(14)
Load contactor indicating lights
Indicating lights within the respective contactor control push-button switches (22 orange and 24
yellow) 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.
(meters)
(cycles per second)
.
The voltmeter
.
Three ammeter
,
. The
November 27/1997Chapter 1-1
Page 11
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
1. Control Box Wrapper
2. Control Box Top
3. Receptacles (4)
4. Memory and Time Delay PC Board
5. Over-Under Frequency PC Board
6. Over-Under Voltage PC Board
7. Voltage Regulator PC Board
8. Terminal Blocks (2)
9. Switch Mounting Bracket
11. Panel Lights (2)
12. Engine Circuit Breaker (10A)
13. Controls Circuit Breaker (5A)
14. Marker Light Circuit Breaker (10A)
15. Contactors Circuit Breaker (5A)
16. Test Bank / Aircraft Switch, No. 2 Output
17. Test Bank / Aircraft Switch, No. 1 Output
18. Regulated / Diagnostic Switch
19. Generator Set Control PC Board
10. Label, Switch Mounting Bracket
Control Box
Interior Components
(Dual Output Shown)
Figure 6
Chapter 1-1November 27/1997
Page 12
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
b. Control Box Interior Components (Fig. 6)
(1)
Test bank aircraft switches
For each load contactor circuit, a single-pole, single-throw toggle switch (16 or 17) provides a
means of bypassing the interlock circuit for that contactor when supplying power to a load bank
or to an aircraft not equipped with a plug interlock system.
(2)
Regulated-diagnostic switch
When the regulated-diagnostic switch
output voltage is regulated by the solid state voltage regulator (7,Fig. 6, and Fig. 8) for 115/200
V-AC output to an aircraft. When this switch is placed in the DIAGNOSTIC (up) position, battery
voltage (12-V DC) is applied to the generator exciter with the engine running at rated RPM, in
order to check the operation of the generator. By applying this 12 V-DC battery voltage to the
exciter and observing generator output voltage, it can be determined 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.
However, a low-level, unregulated voltage of approximately 30-V AC will be produced at the
generator output terminals due to the residual magnetism of the exciter.
(3)
Circuit breakers
A 10-ampere circuit breaker (12), protects the 12-V DC engine governor and fault circuits, and
another 10-ampere circuit breaker (14)
breaker (13) protects the 12-V DC control system, and another 5-ampere circuit breaker (15)
protects the circuits of the load contactors.
(18)
is in the REGULATED (down) position, generator
,
protects the 12-V DC lighting system. A 5-ampere circuit
(4)
Memory-time delay module
The memory and time delay module (4) is sometimes called the protective monitor module. It is
a solid-state device with a hermetically-sealed, reed-type circuit. The printed circuit board
includes five memory circuits and a time delay circuit. Each circuit is connected to a
corresponding sensing circuit in the sensing modules. All memory circuits are connected to the
module circuit relay coil, and any one of the circuits can energize the coil to open the circuit relay
contacts. Thus, when a sensing device energizes any one of the module circuits, the module
circuit is also energized to break the load contactor holding circuit and allow the load contactor to
open. A time delay system is designed into the under voltage circuit to prevent nuisance opening
of the contactor under conditions of momentary under voltage in the generator output. An under
voltage condition which continues uninterrupted for a period of 4 to 12 seconds (adjustable) will
cause the time delay circuit to open the load contactor. Each of the five circuits is connected to
a corresponding indicating light (Fig. 5; 14, 15, 17, 21 or 23)
occurs. The module circuit will remain energized (OPEN) and the light will remain ON until the
reset push-button switch (19, Fig. 5) is pushed to break the module 12-V circuit, and allow the
circuit to return to normal, CLOSED position.
(5)
Sensing modules
The voltage sensing module (6) and frequency sensing module (5) are connected to generator
output leads between the generator and load contactor. These solid-state modules sense any
abnormal condition of voltage or frequency and signal the solid-state circuitry of the memory and
time delay module (4) to open the load contactor and disconnect output to the aircraft. Trip
values are adjustable; however, adjustments should be made ONLY under laboratory conditions.
On the 400-Hz output module, one solid-state overload signaling device (1, Fig. 9), is also
connected to the protective monitor module. Its function is similar to the voltage and frequency
sensing modules.
,
which is turned on when a fault
November 27/1997Chapter 1-1
Page 13
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
Trip values for protective circuits are as follows:
Over voltage relayTrips at 126 volts after 1-second time delay.
Under voltage relayTrips at 100 volts after 7 seconds.
Over frequency relayTrips at any value between 420-Hz and 480-Hz
Under frequencyTrips at 380-Hz or less after a 7-second time
Overload time delayTrips in approximately 5 minutes at 125% load
(6)
Generator Set Control PC Board
The generator set control PC board (19, Fig. 6 and Figure 7) is a central location for the various
plug-in relays used for generator operation. Troubleshooting is thus easier for technicians
working on the generator set. This PC board contains the following relays and associated
circuitry.
Trips at 140 volts in 160 milliseconds.
Trips at 180 volts in 50 milliseconds.
after a 5-second time delay. Trips immediately
at any frequency exceeding 480-Hz.
delay.
on either output or both outputs.
• Master relay, K69, routes 12-V DC power to all circuits, except panel and clearance lights.
This relay is operated upon pressing the START push-button switch
remains in the OPERATE condition until it is RESET by the STOP push-button switch
(26, Fig. 5)
, and
(20,
Fig. 5).
• Bypass relay, K73, is also activated by pressing the START push-button switch. Relay
K73 enables the start signal to the starter solenoid for 5 seconds after it is initially
activated. K73 also disables the low oil pressure fault circuit during this 5 second period.
• Idle-excitation relay, K68, controls engine speed and generator excitation. K68 activates
to idle the engine and remove excitation from the generator. In the RESET state, K68
provides a 12-V DC signal to the governor controller, causing the engine to attain rated
speed (2400 RPM). At the same time, K68 provides a ground signal to voltage regulator,
which enables excitation current to the generator. When the engine is running, K68
changes from OPERATE to RESET, or vice-versa, with each closure of the START
push-button switch. Auxiliary circuit also controls the idle-excitation relay. This auxiliary
circuit causes the relay to operate when: (1) Engine is at rest and the start push-button
switch (26, Fig. 5) is pressed, (2) Any engine fault, except the air filter restriction, occurs.
• The circuit which controls K68 also drives a flasher circuit that controls the lamp within the
START push-button switch (26, Fig. 5).
• Relay K72 controls the No. 1 contactor. When the engine is at rated speed, and voltage
has built up, K72 changes from OPERATE to RESET, or vice-versa, with each closure of
the No. 1 contactor push-button switch. An auxiliary circuit will reset K72 when the No. 1
plug is removed from the aircraft. The No. 2 contactor control relay, K272 operates in the
same manner.
• Relay K70 controls panel and clearance lights. This relay changes from OPERATE to
RESET, or vice-versa, with each closure of the LAMPS push-button switch (28, Fig. 5)
The fuel gage is also powered by K70 when the engine is at rest. K70 is reset, turning off
all lights, when the engine STOP push-button switch is pressed.
.
Chapter 1-1November 27/1997
Page 14
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
1. Master Relay (K69)
2. Idle-Excitation Relay (K68)
3. Over Temperature Fault Relay (K67)
4. Low Oil Pressure Fault Relay (K71)
5. No. 2 Contactor Control Relay (K272)
6. Panel and Clearance Lights Relay (K70)
Generator Set Control PC Board
November 27/1997Chapter 1-1
7. No. 2 Plug-Interlock Relay (K202)
8. No. 1 Plug-Interlock Relay (K2)
9. Bypass Relay (K73))
10. Low Fuel Fault Relay (K65)
11. Air Filter Fault Relay (K66)
12. No. 1 Contactor Control Relay (K72)
Figure 7
Page 15
OM-2084 / Operation and Maintenance Manual
90CU24 / Series 500392 Generator Sets
• Relays K65, K66, K67 and K71 are fault relays. Each receives a signal from engine
sensors, and illuminate panel lights to indicate the presence of a fault. Activation of the
over temperature relay, K67, or low oil pressure relay, K71, result in interruption of 12-V
DC power to the governor controller, causing the engine to shut down. Activation of low
fuel relay K65 may result in the engine reverting to idle speed or shut-down, depending on
the condition set by jumpers JP2 and JP3. The only result of an air filter fault, is that relay
K66 causes illumination of the panel light. All engine fault relays remain activated until
power is removed by pressing the STOP push-button switch (20, Fig. 5) or the emergency
stop switch.
• The plug-interlock relays (K2 and K202) on the control PC board cause the respective
output load contactors to open in the event the cable plug connector becomes accidentally
disconnected from the aircraft during power delivery, or if an attempt is made to deliver
power when the output cable is not connected to the aircraft. Twenty-eight volt direct
current for operation of the circuit is supplied from the aircraft either through an on-board
transformer- rectifier, or from a twenty-eight volt electrical system. Connection from aircraft
to the interlock circuit is made through terminals E and F on the output cable plug
(7)
Voltage regulator PC board
This voltage regulator (7, Fig. 6 and Fig. 8) is designed to provide 1% voltage regulation for all
loads up to 100% of rated load on a three-phase, four-wire, 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.
• 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: (1) A current
transformer on each phase of the load circuit, and (2) A fixed resistance in parallel with
each current transformer. The current transformers detect the magnitude of current flowing
through the power cables from the alternator to its load and feed 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.
• A receptacle connector at the bottom of the voltage regulator PC board provides a quick
connect-disconnect facility for interconnecting wire leads.
Chapter 1-1November 27/1997
Page 16
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