VDO CANcockpit Series Product Manual

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New Generation 2009
Flexible instrumentation with CAN bus technology
www.vdo.com
CANcockpit
Product Manual
VDO - eine Marke des Continental-Konzerns / VDO - Atrademark of the Continental Corporation
Page 2
Topic Chapter
Description of Functions 2
Installation Instructions 3
Testing Instructions 4
Software-Description 5
System Components, Spare Parts and Accessories 6
Data Sheets 7
General Information 8
Sales and Service Informations 9
= will follow
The reproduction, distribution and utilization of this document as well as the communication of its contents to others without express authorization is prohibited. Offenders will be held liable for the payment of damages. All right reserved in the event of the grant of a patent, utility model or design.
Overview of Chapter
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1. Safety Instructions
Product Manual
Contents
Contents
1.1 Installation 2
Before installation 2 During installation 3 After installation 3
1.2 Electrical Connection 4
1.3 Sensors 5
1.3.1 Pressure Sensor for Oil 5
1.3.2 Temperature Sensor for Oil 6
1.3.3 Temperature Sensor for Engine Coolant 7
1.3.4 Fuel Level Sensor (Lever Type Sensor/Tubular Type Sensor) 8
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1.1 Installation
The product is only designed for use in land-bound vehicles (except motorcycles).
Make sure that the engine cannot be unintentionally started during installation.
Before installation
Withdraw ignition key from ignition lock.
Note down all data in temporary electronic memories.
Before installation refer to the vehicle documents for details of vehicle type and any special features.
Refer to the construction diagrams to find out the positions of the fuel/hydraulic/pneumatic and electrical lines.
Take account of any modifications to the vehicle which have to be considered during installation.
Failure to use the product correctly may cause harm to people, property and the environment. Therefore make sure you use our product correctly.
Basic knowledge of vehicle electrics and mechanics is necessary for installation to prevent harm to people, property and the environment.
The product has been developed, manufactured and tested in accordance with the basic safety requirements of EC di­rectives and the acknowledged state of the art.
Short circuits Short circuits in the vehicle's wiring can cause cable fires, battery explosions and damage to other electronic systems. Therefore disconnect the minus pole of the vehicle battery before starting work. If the vehicle has supplementary batteries, the minus poles of these batteries should also be disconnected.
Modifying or tampering with the product may affect safety. Therefore it must not be modified or tampered with.
When removing/installing seats, covers and the like, make sure that you do not damage lines or release plug connec­tions.
Possible data loss When the batteries' minus poles are disconnected, all the temporary electronic memories lose their entered data. Therefore, note down all the relevant data for re-programming before disconnection.
1. Safety Instructions
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No smoking! No naked flames or lights!
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1.1 Installation
During installation
During installation make sure that the product's components do not affect or restrict vehicle functions and are themsel­ves not damaged.
Only install undamaged parts in vehicles.
During installation make sure that the product does not impair the field of vision and that the product is not positioned within the impact range of the driver's or passenger's heads.
When selecting the installation location, make sure there is sufficient space behind the drilled holes and the installation opening.
Take account of the routing of lines and cable leads.
Do not select an installation location within the mechanical and electrical range of the airbag.
Do not drill holes or cut openings in load-bearing or stabilizing struts or members.
Err on the small side when predrilling installation apertures with cone-type cutters, compass or jig saws, or files, enlar­ge if necessary and complete. Deburr edges. Always follow the tool manufacturer's safety instructions.
When working beneath the vehicle, secure the vehicle in accordance with the vehicle manufacturer's instructions.
If any work is necessary while the engine is running, take special care. Only wear suitable working clothes because of the risk of injury due to pinching and burning. Long hair should be worn in a hair net.
Only use the envisaged multimeters or diode-test lamps to measure wattages and currents in motor vehicles. The use of conventional test lamps can cause damage to control units and other electronic systems.
After installation
Firmly connect the earth cable to the minus pole of the vehicle battery.
(Re-)program the data in the temporary electronic memories.
Test all(!) vehicle functions.
CANcockpit components to be cleaned with clear water only. Observe the IP-degrees of protection (DIN 40050).
1. Safety Instructions
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1.2 Electrical Connection
Take account of the cable cross section A reduction in the cable cross section results in a higher current density. This can cause the cable to heat up.
When laying electric cables, use existing cable ducts and routes but without laying cables parallel to ignition cables or cables leading to high current consumers. Fix the cables with cable tape or adhesive tape.
Do not route cables over mobile components. Do not fasten cables to the steering column.
Make sure that the cables are not exposed to tensile, compressive or shear forces.
If the cables are routed through drilled holes, protect them with rubber sleeves or the like.
Strip cables only with a cable stripper. Adjust the stripper so that no strands are damaged or severed.
Solder new cable connections only with the soft soldering process or use standard crimp connectors.
Crimp connections should only be made with a crimping tool. Follow the tool manufacturer's safety instructions.
Insulate exposed strands so that no short circuiting can occur.
Faulty wiring can cause short circuiting. Wire the cables only in accordance with the electrical connection diagram.
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Connect the cables in accordance with the electrical connection diagram.
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1.3 Sensors
1.3.1 Pressure Sensor for Oil
Sensor installation location: At the place provided by the engine manufacturer, equipment manufacturer or car manu-
facturer in the oil circulation system (most often in place of the oil pressure switch).
Sensor installation only when engine is cold. When removing the oil pressure switch or the screw from the drilled hole for the oil pressure measuring system, collect
the oil running out of the system in a proper container and dispose of it in accordance with legal regulations.
max.
The values mentioned in the following table for the maximum tightening
torque (Nm max.) refer exclusively to the load-bearing capacity of products. Prior to using the product, it is important to ask the manufacturer of the ve­hicle, equipment system or engine in each instance for the maximum tor­que (? Nm max.) value for the threaded hole into which the product is to be screwed. Non-observance of the maximum tightening torque specified for the threaded hole in each instance can result in damage to the vehicle, en­gine or equipment system.
If the connection thread is cylindrical, a sealing washer or a sealing ring made of copper must be fitted. Following sensor installation, fill up the system with the required quantity of specified oil.
1. Safety Instructions
Product Manual
M10 x 1 30 Nm 1/8 in. BSPF 30 Nm 1/8 - 27 NPTF 30 Nm R 1/8 DIN 2999 30 Nm M12 x 1,5 40 Nm M12 x 1 50 Nm M14 x 1,5 50 Nm 1/4 in. BSPF 60 Nm 1/4 - 18 NPTF 60 Nm 3/8 - 18 NPTF 60 Nm M16 x 1,5 80 Nm 3/8 - 18 Dryseal NPTF 80 Nm M18 x 1,5 100 Nm
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1.3 Sensors
1.3.2 Temperature Sensor for Oil
Sensor installation location: At the place provided by the engine manufacturer, equipment manufacturer or car manu-
facturer in the oil circulation system (e. g. oil drain plug).
Sensor installation only when engine is cold. When removing the oil drain plug, collect the oil running out of the system in a proper container and dispose of it in ac-
cordance with legal regulations.
max.
The values mentioned in the following table for the maximum tightening tor-
que (Nm max.) refer exclusively to the load-bearing capacity of products. Prior to using the product, it is important to ask the manufacturer of the ve­hicle, equipment system or engine in each instance for the maximum tor­que (? Nm max.) value for the threaded hole into which the product is to be screwed. Non-observance of the maximum tightening torque specified for the threaded hole in each instance can result in damage to the vehicle, en­gine or equipment system.
If the connection thread is cylindrical, a sealing washer or a sealing ring made of copper must be fitted. Following sensor installation, fill up the system with the required quantity of specified oil.
1. Safety Instructions
M10 x 1 10 Nm M10 x 1.5 10 Nm 1/8 - 27 NPTF 10 Nm
M12 x 1.5 15 Nm 1/2 - 20 Gang 15 Nm
M14 x 1.25 20 Nm M14 x 1.5 20 Nm 5/8 - 18 UNF - 3A 20 Nm 1/2 In. 20 Whit. S 20 Nm 1/4 - 18 NPTF 20 Nm
M16 x 1.5 30 Nm M18 x 1.5 30 Nm M20 x 1.5 30 Nm M22 x 1.5 30 Nm M24 x 1.5 30 Nm M26 x 1.5 30 Nm 1/2 - 14 NPTF 30 Nm 3/8 - 18 NPTF 30 Nm R 1/2 30 Nm R 3/8 30 Nm 3/8 - 18 Dryseal NPTF 30 Nm 3/4 - 16 UNF-3A 30 Nm
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1.3 Sensors
1.3.3 Temperature Sensor for Engine Coolant
Sensor installation location: At the place provided by the engine manufacturer, equipment manufacturer or car manu-
facturer in the coolant circulation system (e.g. in place of the temperature warning switch) or in the coolant hose.
Sensor installation only when engine is cold. Collect the coolant running out of the system in a proper container and dispose of it in accordance with legal regulations.
max.
The values mentioned in the following table for the maximum tightening tor-
que (Nm max.) refer exclusively to the load-bearing capacity of products. Prior to using the product, it is important to ask the manufacturer of the ve­hicle, equipment system or engine in each instance for the maximum tor­que (? Nm max.) value for the threaded hole into which the product is to be screwed. Non-observance of the maximum tightening torque specified for the threaded hole in each instance can result in damage to the vehicle, en­gine or equipment system.
If the connection thread is cylindrical, a sealing washer or a sealing ring made of copper must be fitted. Following sensor installation, fill up the system with the required quantity of the compositon specified coolant.
1. Safety Instructions
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M10 x 1 10 Nm M10 x 1.5 10 Nm 1/8 - 27 NPTF 10 Nm
M12 x 1.5 15 Nm 1/2 - 20 Gang 15 Nm
M14 x 1.25 20 Nm M14 x 1.5 20 Nm 5/8 - 18 UNF - 3A 20 Nm 1/2 In. 20 Whit. S 20 Nm 1/4 - 18 NPTF 20 Nm
M16 x 1.5 30 Nm M18 x 1.5 30 Nm M20 x 1.5 30 Nm M22 x 1.5 30 Nm M24 x 1.5 30 Nm M26 x 1.5 30 Nm 1/2 - 14 NPTF 30 Nm 3/8 - 18 NPTF 30 Nm R 1/2 30 Nm R 3/8 30 Nm 3/8 - 18 Dryseal NPTF 30 Nm 3/4 - 16 UNF-3A 30 Nm
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1.3 Sensors
1.3.4 Fuel Level Sensor (Lever Type Sensor/Tubular Type Sensor)
An installation opening remaining to be made in the tank at a suitable point for supply level measurement or at an in-
stallation flange or installation opening already provided by the tank manufacturer.
If an installation opening must be made, the tank must be completely drained first. Fill the fuel into an approved contai-
ner.
Risk of explosion exists due to presence of residual gases in the tank! Make sure that the tank is aired
sufficiently (approx. 10 minutes).
Make a preliminary hole in the installation opening using a drill and then finish the hole using a compass saw or piercing
saw. Comply with the safety instructions of the tool manufacturer. Clean the tank of residue from the drilling or sawing work.
The safety instructions given by the welding equipment manufacturer and the working regulations applying to welding
work must be respected when welding the tank flange.
1. Safety Instructions
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Contents
Contents
1. System 3
1.1 Main Features 3
1.1.1 Block Diagram CANcockpit 3
1.2 Mechanical Concept 3
1.3 Safety Concept 4
1.3.1 Sensors 4
1.3.2 System Check 4
1.3.3 Satbus 4
1.3.4 WINgauge 4
2. Master Gauges 5
2.1 General Features 5
2.1.1 Main Functions 5
2.2 Mechanical Concept 6
2.2.1 Master dia. 80 mm 6
2.2.2 Master dia. 85 mm 6
2.2.3 Master dia. 100 mm 6
2.3 Input Signal Processing 7
2.3.1 Analog Inputs 7
2.3.1.1 Grounding Concept 7
2.3.1.2 Sensors 7
2.3.2 Input Signal Processing applied to the two frequency inputs 7
2.3.3 Input Signal Processing for CANbus messages 8
2.4 PIN Assignment Description 9
2.4.1 Technical Description 9
2.5 Display Functions 12
2.5.1 Navigation through Display 12
2.5.2 Display Layout 12
2.5.3 Display Functions 14
2.5.3.1 Main Display (Odometer, Hourmeter) 14
2.5.3.2 Alarm Display 14
2.5.3.3 CAN DTC Display 15
2.5.3.4 Warning Display 15
2.5.3.5 Service Message 16
2.5.3.6 Physical Value Display 16
2.5.4 Alarm- and Warning Functions 17
2.5.4.1 Description of the Outputs 17
2.5.4.2 Switch Output Acknowledgement Function 17
2.5.4.3 Alarm and Warning Trigger Conditions 18
2.5.4.4 Alarm and Warning Trigger enabling with Engine running 18
2.5.4.5 Alarm and Warning State Diagram (Maximum Value Algorithm) 19
2. Functional Specification
Product Manual
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2.5.5 Service 21
2.5.5.1 Reset of Service messages 21
2.5.6 CAN (SAE J1939) DTC (Diagnostic Trouble Codes) messages 22
2.5.6.1 CAN SAE J1939 Elements 22
2.5.6.2 CAN DTC Information Display Requirements 23
2.5.6.3 CAN DTC Display Functions 23
2.5.6.4 Speedometer Master Gauge 25
2.5.6.5 Tachometer Master Gauge 27
3. Satellite Gauges 28
3.1 Mechanical concept 28
3.2 Fault modes 28
3.3 Satellite gauge address 29
3.4 Warning Lamp inside the Satellite Gauge 29
3.5 Tolerance 29
A. Technical Data 30 B. Applied Standards 31
2. Functional Specification
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1. System
1.1 Main Features
Master-Slave relationship between Master gauge and other instruments
Up to 16 Slave functions on one Master instrument or 32 with the use of two Master instruments
CAN protocol flexibility ( processing two protocols simultaneously)
Modular "plug & play" as needed
Analogue sensor compatible
Frequency inputs
Dot-matrix information display
Switch outputs available
Flexible to customer needs
1.1.1 Block Diagram CANcockpit
1.2 Mechanical Concept
The Masters are 80, 85 and 100 mm in diameter, the Satellite gauges dia. 52, 80 and 100 mm. The dials are translucent backlighted. The illumination of the gauges is realised with white LED's. The backlighting of the LCD has a yellow LED. The warning lamp in the slave can have a red or yellow LED. The housing and bezel are made of non-flammable plastic, the design is like a triangle with the black color RAL 9005. The be-
zel is clipable. The lens is flat and frosted. The pointer has a PC hub in black and the pointer arm is OL5105 (white -coated on the underside). The pointer type is translucent illuminated.
The housings have an indent in the thread at 6 o'clock position, so that an optional key can be used according to SAE J1226 and SAE J 1399. The movements are front-mounted stepper motors MW2000, only clockwise indication.
2. Functional Specification
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1.3 Safety Concept
1.3.1 Sensors
Analog sensors can be checked for short and open circuit.
1.3.2 System Check
When the trip-reset button is pressed while ignition is being turned on, the system-check function is activated and clears the contents of the DTC List.
If there are any active service messages, they will be displayed on the Dot-Matrix Display starting with the first active service message. If the reset button is then pressed and held for 5 seconds or longer, this service message will be reset. The next active service message is displayed thereafter. To proceed to the next active service message without resetting the displayed code, the button needs to be pressed shortly (<5 sec). If all active service codes have been displayed, the system check function is started as described below:
1. All warning lamps and illumination of all gauges are activated for 3 seconds.
2. The Master gauge initializes all configured satellite gauges and waits until they are ready or a Satbus timeout occurs.
3. During time.this, all LCD-Dots are turned on for about 1.5 sec, all pointers are moved to their end value
4. Then all LCD-Dots are turned off and the pointers move back to zero, for about 1.5 sec too, and all warning lamps and illumination will be turned off
5. Firmware version and Check sum of the EEPROM in hexadecimal format are displayed for about 10 sec.
The display format is as follows: XX represents a hex-coded value
1.3.3 Satbus
After ignition for synchronisation the Master gets feedback from the satellites. A timeout function can be programmed too. If more satellites are configured, the Master will not get feedback from all gauges. After a timeout of about 14 seconds, the Master will act as described before, when the Master gets feedback from all satelli­tes.
During normal operation there is no feedback from the satellites.
1.3.4 WINgauge
A system diagnosis function for testing all in- and outputs is implemented in the WINgauge Software.
2. Functional Specification
Product Manual
Small
display
line
Format Description
2 hXX sXX.XX dd_mm_yyyy hXX specifies the Hardware version relevant to the Firmware
sXX.XX refers to the Firmware version, for example s12.A8 stands for V06 dd_mm-yyyy is the Firmware date in day, month and full-year format.
4 nXXXXwXXyXX cXXXXXX nXXXX is the WINgauge serial number of the device as programmed into the
EEPROM. wXXyXX displays the production week and year in short format. cXXXXXX shows the actual 3-byte Checksum of the EEPROM as calculated during the system check.
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2. Master Gauges
2.1 General Features
The design concept for this design includes:
2x High-speed Full-CANbus interface V2.0B compatible.
Half-duplex serial link to satellite gauges.
VMC SCAL CDVV Microcontroller with identical firmware.
Stepper motor MW2000 directly controlled by Microcontroller.
Satellite gauges use SM2 stepper motor driven by ISM IC.
LED illumination concept.
132 x 33 dots matrix LCD.
Wide input voltage range switch mode power supply.
Diagnostic Interface for configuration.
2.1.1 Main Functions
2. Functional Specification
Product Manual
Inputs
Outputs
CAN_1
CAN_2
Frequency_1
Frequency_2
Sensor Input_1
Sensor Input_2
Sensor Input_3
4 to 20 mA
Voltage Input
Illumination
term.15
term.30
Inp ut Sig nal Pr oc es sin g
Analogue Gauge Functions
W arning Fu nc ti ons
Odomete r,
Tripmeter
Hourmeter
,
Triphourmeter
Service Intervals
Illumination Control
Power Supply Control
Parameter Memory (EEPROM)
Diagnostics
Frequency-Divider
Ou tpu t Sig nal Pr oc es sin g
Flash-Boot-Loader
Intern al MW2000
SatBus
-Gauges
LCD
Sat-Gauge Warning Lamps
Switch Output_1
Switch Output_2
LCD
LCD
Master Gauge Illumination
SatBus
-Gauge Illumination
Master Gauge Supply
SatBus
Supply
Sensor Supply
K-Line Diagnostic s
Diagnostic Trouble Codes
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2.2 Mechanical Concept
As the same LCD is used for different Master gauge diameters the pointer position has different eccentricities and indication angles.
The connectors are 26-Pin MODU II-Connector and 4-Pin MATE-N-LOK from AMP.
2.2.1 Master dia. 80 mm
Two PCB's are necessary for this diameter. They are connected with a standard pin connector and two distance towers.
2.2.2 Master dia. 85 mm
The PCB assemblies and their corresponding parts of the Ø 80 mm and Ø 85 mm gauges are identical. The difference bet­ween the two gauges is the position of the stepper motor on the PCB so that the eccentricity of 7 mm in the Ø 80 mm gauge can be reduced to 4.5 mm in the Ø 85 mm gauge.
2.2.3 Master dia. 100 mm
For this size, only one PCB assembly is necessary. Input Signal Processing.
Gauge diameter [mm] Eccentricity [mm] Indication angle
80 7 210° 85 4.5 216°
100 0 206°
2. Functional Specification
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2.3 Input Signal Processing
2.3.1 Analog Inputs
All sensor characteristics can be defined with the WINgauge Software.
2.3.1.1 Grounding Concept
The Master gauge has two main ground lines. Ground term.31 is connected to the vehicle's body (negative battery terminal) and Sensor Ground is supplied from the instrument; insulated return sender are necessary. The Sensor Ground should not be connected to vehicle ground, which would result in a higher current flowing through this line and thus produce a signal noise and measurement error. Sensor Ground and Ground term.31 are joined together inside the Master Gauge. This grounding principle is necessary to accurately measure analog values. Ground shift on Sensor Ground is minimized by this concept.
2.3.1.2Sensors
The static and dynamic voltage drop of the sensors should not exceed 0.5 V.
Pressure: 10 - 184 Ohms Temperature: 10 - 700 Ohms Fuel lever type: 3 - 180 Ohms Fuel dip-pipe: 0.5 - 90 Ohms Other sensors: 4 - 20 mA Other sensors: 0 - 5 V
2.3.2 Input Signal Processing applied to the two frequency inputs
Frequency 1:
The standard modules can be changed to 500 < k < 400 000 pulses/km or miles for the Speedometer and 0.5 - 400 pulses/rev for the Tachometer.
Maximum frequency is 40 kHz (2 kHz via internal divider).
Frequency 2 as Hall Sensor / Terminal W:
500 < k < 65000 pulses/km or miles for Speedometer and 0.5 - 65 pulses/rev for Tachometer.
Maximum frequency is 2 kHz.
2. Functional Specification
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,
Fuel
Sender
Oil Pressure
Sensor
Engine-
Temperature
Vehicle
Sensor-Ground
Chassis GND
Gauge2000 System
Ground Term.31
CANcockpit System
Page 18
2.3.3 Input Signal Processing for CANbus messages
Example of SAE J1939 Messages received on one of the two CANbus Interfaces.
The Master Gauge CANbus interface conforms to CAN 2.0B specification and supports extended (29Bit) identifiers. The Gauge acts as a "Standard ECU, which is non-configurable as defined in SAE J1939. The application layer is based on SAE J1939/71 Rev 2008-01.
Additional communication protocol is CAN Open For this the different CANbus data bases will be provided by the WINgauge configuration.
2. Functional Specification
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2.4 PIN Assignment Description
Master:
2.4.1 Technical Description
PIN 1: Power Supply (terminal 30)
V
Batt
= + 10,5 V to + 32 V The instrument is supplied with permanent power through this terminal. Current consumption varies depending on the instru­ments operating mode (standby or active) and number of Slaves.
PIN 2: Ground (terminal 31)
Power ground of the instrument.
PIN 3, 4: CANbus Interface 1
High-Speed Full CANbus V2.0B compatible (10, 20, 50, 125, 250, 500 kbit/s, 1 Mbit/sec.). 12 V and 24 V system compatible. Cable: shielded, twisted pair with a drain. Cable Impedance: nom. 120 Ω. Topology: linear Bus Trunk Length: max. 40 meters Drop Length: max. 1 meter Termination: 2 resistors 120 at each end of the bus. Related documents: ISO 11898, SAE J1939/11
U
A combination of 29 bit ID and 11 bit ID can`t be processed!
PIN 5, 6: CANbus Interface 2
See on CANbus Interface 1.
PIN 7: Not connected
PIN 8: K-Line Diagnostic Interface
Programming of the EEPROM and the diagnostics carried out via serial diagnostic interface K-Line.
PIN 9, 25: Analog Input 1
Range: 0.5 - 200
Standard sensors: Tube-type Sensor: 0,5 to 90
Lever-type Sensor: 3 to 180 .
Sensor has to be connected between theese pins.
PIN 10, 25: Analog Input 2
2. Functional Specification
Product Manual
Pin Description Pin Description 1 Power Supply (terminal 30) 14 + 8 V DC for sensor supply 2 Ground (terminal 31) 15 0 - 5 V DC Input 3 CAN1 _High 16 Illumination (terminal 58 (d)) 4 CAN1 _Low 17 Ignition (terminal 15) 5 CAN2 _High 18 Frequency Input 2 (0-2 kHz) 6 CAN2 _Low 19 Frequency Input 1 (0-40 kHz) 7 NC 20 Switch-Output_1 8 k-Line 21 Switch-Output_2 9
Analog Input 1 (0,5 - 200 Ω)
22 NC
10
Analog Input 2 (0,5 - 300 Ω)
23 NC
11
Analog Input 3 (10 - 700 Ω)
24 External Switch 12 4 - 20 mAInput 25 Analog GND 13 4 - 20 mAGND 26 Frequency GND
Page 20
Range: 0.5 - 300 Standard sensors: Pressure sensor(10 - 184 ) Sensor has to be connected between theese pins.
PIN 11, 25: Analog Input 3
Range: 10 - 700
Standard sensors: Temperature sensor (38 - 700 Ω) Sensor has to be connected between theese pins.
PIN 12, 13: 4 to 20 mA Input
Range: 4 to 20 mA A resistor converts the 4 - 20 mA current into proportional voltage. Results are sampled every 31.25 msec by the Microprocessor.
PIN 14: +8 V sensor power supply:
Voltage: +8 V - 0 %, +10 % Max. current: 50 mA
U
This output can be used only at 24 V power supply.
PIN 15: 0 - 5 V Input :
Range: 0 - 5 V Results are sampled every 31.25 msec by the Microprocessor.
PIN 16: Illumination Input (terminal 58 (d):
Range: 0 to U
Bat.
(battery voltage) Dimming of Master gauge illumination and attached Satellite gauges is controlled by the voltage amplitude at the Illumination input.
PIN 17: Ignition (terminal 15)
Vign.= + 10,5 V to + 32 V The Microprocessor senses the voltage at the input and turns it into active mode, if the ignition is turned on.
PIN 18, 26: Frequency Input 2 Hall Sensor and terminal W:
Max. Frequency: 2 kHz U high min.: 5 - 7 V according to the configurated pulses Signal type: square, sinus Max. offset: 0.5 V Off current max.: 100 µA Duty cycle: 50 ± 15 % Pulse ratio: 500 - 65 000 pulses/km or miles Pulse/rev: 0.5 - 65 pulses/revolution The Instrument has a pull-up resistor at the ignition in the input circuit. Input can be either road speed or engine speed. Selection by configuration.
U
Only one frequency input (either Input 1 or 2) can be defined as road speed input.
PIN 19, 26: Frequency Input 1 Universal Frequency Input
Max. Frequency: 40 kHz (2 kHz via internal divider, 1:1; 1:2; ... 1:20) U
high
min: 1.5 - 10 V according to the configurated pulses Signal type: square, sinus Max. offset: 0.5 V Off current max.: 100 µA Duty cycle: 50 ± 15% Pulse ratio: 0.5 - 400 pulses/revolution
The instrument has a pull-up resistor at ignition in the input circuit. Input can be either road speed or engine speed. Selection
2. Functional Specification
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by configuration. An adjustable frequency divider reduces input frequency, so that it can be processed by the Microprocessor.
U
Only one frequency input (either Input 1 or 2) can be defined as road speed input.
PIN 20: Switch Output 1
Maximum voltage: 32 V Maximum current: 0.5 A Warning lamp to be connected between output and supply voltage (terminal 15 or terminal 30). Switch output controlled by the Microprocessor. The pin turns the output either on or off (static). The output is an open drain and acts like a low switch to ground.
U
Save against high current with a Fuse 0.5 A!
PIN 21: Switch Output 2
Identical with Switch output 1
PIN 22: Not connected
PIN 23: Not connected
PIN 24: External Switch
Switch has to be connected between this pin and GND
Satellite
PIN 1-3: Satellite Bus Interface (Satbus):
Bus signal levels: 5 V ± 10% Ground reference: ± 100 mV Max. Bus length: 10 m Cable impedance: Standard cable Connector: 4-Pin MATE-N-LOK AMP
Satbus is used in a Master-/ Slave-configuration and is bi-directional with half-duplex communication. When the system is ac­tive, a constant clock signal is produced on the bus by the Master gauge. Bit-rate on Satbus = 31.25 kHz.
2. Functional Specification
Product Manual
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Pin Description Pin Description 1 - 3 GND 2 Satellite - Bus 4 Power Supply
Page 22
2.5 Display Functions
Five main display functions have been specified for the Master gauge. (s. picture below) As the number of displays in each main function is configurable (except for odometer and hourmeter), the actual number of displays can be up to a maximum of
146.
A maximum of 30 Warnings and 30 Alarms can be set. The Physical Values of the defined Satellite gauges can be shown on the display (if configured). Atotal of 25 physical value Displays (PVD) are possible, including the physical values inidcated by the Satellite gauges. Thus with increasing numbers of Slaves defined by WINgauge, the number of freely selectable physical values to be displayed on the dot-matrix decreases.
2.5.1 Navigation through Display
The order of the display groups is: Odometer / Hourmeter, Alarms, CAN DTCs, Service Messages, Physical Values, Warnings and then back to Odometer / Hourmeter. The Alarms, CAN-DTCs, Service Messages and Warnings are being monitored and appear only if they are activated. If the button is pressed more than 2 sec., the LCD shows the main display which is Odometer / Hourmeter.
2.5.2 Display Layout
The Dot-matrix Display has 132 x 33 dots. The following picture shows the proposed display layout. The outer line represents the LCD glass and the inside marks the active display area. The structure inside has only been drawn for illustration; it is not visible on the display itself
2. Functional Specification
Product Manual
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1. Odometer Hourmeter
2. Physical V alues Display (max. 25)
3. Se rv ic e In te rv a l
Message (max. 15)
4. CAN Diagnostic
Trouble Codes (max. 5)
5. Warning and Alarm Messages (max. 30)
45)
60)
Page 23
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The display is structured into three main areas:
1. Symbol Area
This 30 x 32 pixel area is reserved for graphic symbols. The symbols are left aligned to optically enlarge the appearance of the symbol.
2. Central Area
The centre of the display is organised as one or two lines with 6 digits each. Here it is possible to show alphanumeric ASCII characters using the large font (12 x 16 pixel). If only one line is displayed, then this line will be centred in vertical direction. Short text (up to 6 letters) can be used to provide identification for the value displayed. This area is best suited to communi­cate important numeric values to the user. Values will be shown in the second line on the right, where units appear on the left. One or two centre lines are configured via WINgauge as well as the description of the short text.
3. Physical Unit Area
The physical unit area is located right of the alphanumeric Centre Lines. In general the unit belonging to the value displayed on the centre lines is shown here as text. This area is organised as four lines of 5 characters of the small font. If the Unit can be displayed with less than three ASCII characters, then the large font is applied, else the small font is used. Units will not be wrapped into the next line.
If there are two Centre Lines, then there will also be two-unit Lines (small Line 2 and Line 4). In case only one Centre Line is displayed, then only one corresponding Unit Line will be visible (small Line 3).
It is therefore possible to show the following parameters and units to give a clear indication of the valid physical unit which can be chosen via WINgauge:
2. Functional Specification
Product Manual
24 * 24
12 * 16
6 * 8
30 dots
72 dots
30 dots
32 dots
Dot Matrix Layout
One centre Line or optional two Alphanumeric Lines with 6digits (12*16dots) each
Four Alphanumeric Lines with 5 digits each
Graphic Symbol Area
Parameter Units
Revolution / rotation 1/min, rpm Speed km/h, mph, knots Distances km, m (Meter), mm, miles, mi, M, m (landmile = 1.609 km), nm (nautical mile = 1.852 km) Power supply Volt, V, A, mA Time h, hours, min, sec Temperatures °C, °F Pressures bar, psi, kPa, Mpa, Level of liquids %, l, gal (US-gallons) Fuel consumption l/h, gal/h, km/l, l/100, kg/h, km/kg Weight kg Power N, kN, Nm Diverse Ohm, Grad, deg, appl, Count, qm/h, Gear, Code, SPN, FMI
Page 24
2.5.3 Display Functions
2.5.3.1 Main Display (Odometer, Hourmeter)
The display shows total and trip in two lines. Total has 6 digits and trip has 4 plus 1 digit. The figures roll over to 0.0 after a distance of 999.999 /
9.999 or 100.000 / 1.000 hours. Pressing the button longer than 2 seconds will reset trip odometer or hourmeter. A part of the Display can be used to show the company logo as a start-up display configured by WINgauge
The centre of the display shows the value of the odometer in the first line and the tripmeter underneath. The physical unit is displayed right to it and can be either miles or km.
The main display of the tachometer is similar to the speedometer, except that it shows operating hours instead of odometer and trip meter. The physical unit is "h" for hours. The digit after the decimal point of the trip hourmeter shows 1/10h.
if no CAN signal is received, only dashes will be indicated.
2.5.3.2 Alarm Display
If an alarm is triggered the Alarm Display is shown. To alert the user, the General- Alarm-Symbol is flashing, alternating with the symbol that indica­tes the type of alarm. The Central area of the display shows the actual physical value (6digits). The physical unit appears to the right.
When the customer quits the alarm longer two seconds the Display will change to the last displayed value (if no other Alarm and Warning is exi­sting which weren't quitted). The General Alarm Symbol will remain in the graphic Symbol Area with a vertical line on the right side of the symbol to indicate that the Alarm doesn't correspond to the main display but to anot­her Physical Value.
When different Alarms are present the highest priority will be shown. The priority of the alarms is defined with the WINgauge Software. If the Alarm is confirmed and the Alarm condition does not exist anymore then the Alarm is cleared in the list of active Alarms. If the Alarm is not confirmed but the Alarm conditon does not exist anymore then the Alarm is still in the list of active Alarms.
T
o see the different Alarms in the Alarm display group the button has to be
pressed shortly (>50 msec).
2. Functional Specification
Product Manual
Main Display for Tachometer
Physikal
Unit
6 Digit Hourmeter
+ Triphourmeter
Main Display for Speedometer
Physikal
Unit
6 Digit Odometer
+ Tripmeter
Alarm Display
Alternating
ISO Symbol
6 Digit
Label
6 Digit Value
Configuration Option:
To provide additional information two Centre Lines can be programmed. The top line displays a label for identification.
If no physical value should appear on the display, then a configuration allows a di­splay, which only shows the alternating graphic symbol in the centre of the di­splay.
This option is useful, if a digital input triggers an alarm.
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Physikal
Unit
Page 25
2.5.3.3 CAN DTC Display
1 to 5 independent DTC channels can be configured. Every channel is able to receive the DTCs from one CAN device (Source Address). If DTCs are received from any of the configured CAN devices, they will be stored into a DTC receive buffer. The buffer will be able to hold a total of 40 DTCs and will be implemented as a ring buffer, so that old DTCs can be overwritten by newly received DTCs
2.5.3.4 Warning Display
In the Warning display the Specific Graphic Symbol (ISO) is flashing at 1 Hz. There is no alternating.
The operator can acknowledge the Warning by pressing the button longer than two seconds. The Display will change to the Display, which was acti­ve before, if no other Alarms and Warnings are existing, which have not been acknowledged yet.
When different Warnings are present the highest priority will be shown. The priority of the Warnings is defined with the WINgauge Software. Alarms have higher priorities than the Warnings. If the Warning condition vanishes also the Warning will vanish, if it has been acknowledged. To see the different Warnings in the Warning display group the button has to be pressed longer than 50 msec.
2. Functional Specification
Product Manual
CAN DTC Display
Symbol for
CAN DTC
Position in
Ring Buffer
6 Digit
Message Label
Warning Display
ISO Symbol
Physical
Unit
6 Digit Label
Configuration Option:
To provide additional information two Centre-Lines can be programmed. The top line displaying a label for identification.
If no phsyical value should appear on the display, then a configuration allows a display, which only shows the flashing graphic symbol in the centre of the display.
This option is usefull, if a digital input triggers a warning.
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Page 26
2.5.3.5 Service Message
The Service Message indication is based on operating hours and odome­ter.
The Graphic Symbol Area displays the "Service Symbol" in case a Service Message becomes due.
The corresponding service code is shown on the centre line of the display centre. As a "unit" the word "CODE" appears to indicate, that the value is a code number.
To see the different active Service Messages in the Service Message di­splay group the button has to be pressed longer than 50 msec.
2.5.3.6 Physical Value Display
The graphic display area shows a symbol relating to the physical value di­splayed. The symbol can be selected via configuration from the defined symbols in ROM or EEPROM. In the standard form the physical value is shown on a single Centre-Line, followed by the physical unit. This unit text can be selected from ROM du­ring configuration.
If the value is outside of the configurated range, then "------" is shown.
To see the different Physical Values in the Physical Value display group the button has to be pressed longer than 50 msec
2. Functional Specification
Product Manual
Service Message
Service
Symbol
Service Code
Configuration Option:
The Service Message indication can be con­figured as stand- alone or interval message.
Physical Value Display
ISO
Symbol
Physical value
6 Digit Value
Physical Value Display
ISO
Symbol
6 Digit
Label
6 Digit Value
Configuration Option:
As an option a text label can provide identifi­cation for the value displayed. For example Battery one of two batteries, or Motor-2 of two motors. The text label can be configured via WINgauge with maximum 6 letters.
The physical value is displayed in the lower centre line.
Physical
Unit
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2.5.4 Alarm- and Warning Functions
The Alarms and Warnings are triggered by the input values. Configuration parameters in EEPROM select the input values. These variables can have a size of 1, 8 and 16 bit. Possible inputs are engine speed, road speed, data in CAN messages and analogue sensor values. Input values are then monitored and if the configured thresholds are exceeded, then an Alarm or Warning action is triggered, resulting in switch outputs being activated.
2.5.4.1 Description of the Outputs
Definitions: Warning: Is a message to make the operator aware of a condition, which requires his attention. Alarm: Is a message to alert the operator about a condition, which requires his attention and immediate action. The Alarm is
more severe than a Warning.
The switch outputs are only controlled by the Alarm- and Warning Functions.
The following switch outputs are provided: a. Output 1 and Output 2
These are two outputs, which act like two switches to ground. The switch output can control i.e. a warning lamp, a buzzer or a relay. It turns off, when the Alarm condition is not existing anymore, or if the Alarm has been acknowledged and it was con­figured. It stays on, if another Alarm condition also configured to turn on this output is still active.
b. Display
Every Alarm or Warning activates a display on the dot matrix. When the Alarm is triggered, then the associated display appe­ars on the dot matrix, overwriting the previous display. The display combines a graphic symbol with a physical value (numeri­cal value plus physical unit), describing the input value, which has caused the Alarm or Warning.
c. Warning Lamps in the Satellite Gauges
The Satellite Gauges include a warning lamp. This warning lamp can be turned on and off via the Sat-Bus. An Alarm or Warning could be configured to activate a warning lamp in each of the Satellite Gauges. The selected warning lamp in the Satellite Gauge remains on as long as the trigger condition remains, and turns off as soon as the trigger condition is not exi­sting anymore. Flashing of the warning lamp can be configurated.
2.5.4.2 Switch Output Acknowledgement Function
The Acknowledgement Function provides a means to turn off some of the switch output action. This may be desired, if the Alarm activates a buzzer and the operator wants to turn the buzzer off.
To acknowledge a switch output, the operator must press the button for more than 2 sec, while the Alarm or Warning is acti­ve.
When a Warning or Alarm has been acknowledged, then the Switch Outputs (1, 2) will be deactivated, if they have been con­figured to turn off these outputs.
2. Functional Specification
Product Manual
Input Values
CAN Cockpit Plus
Switch Output Functions
Output 1
Output 2
Display
Lamp in SAT-Gauge 0.. 15
Configuration Data
From EEPROM
Page 28
2.5.4.3 Alarm and Warning Trigger Conditions
The diagram above illustrates the Alarm and Warning trigger conditions for the engine coolant temperature as an example. The Warning threshold is set at 105° C, where the Alarm threshold is reached at 110° C. To prevent repeated on/off cycles of the Warning or the Alarm an activation hysteresis is applied. Therefore in above example an Alarm is turned off, if the tempe­rature falls below 108° C and the warning is cancelled at 103° C. The hysteresis is 2° C in this case and is the same for both Alarm- and Warning condition. In addition a turn-on delay from 1 sec to 4 minutes can be configured. The delay time starts, when the threshold is reached. If the input value falls below the threshold value, then the delay time restarts from this point in time.
It can be configured, that the Warning is triggered, if a value rises above a threshold (as in the case of the engine coolant temp.), or if the input value falls below a threshold (e.g. fuel level).
2.5.4.4 Alarm and Warning Trigger enabling with Engine running
Triggering of some Alarms and Warnings only makes sense, when the engine is actually running. Examples are engine oil pressure or hydraulic pressure. For these situations triggering an Alarm and Warning can be disabled until the engine is run­ning. This conditional trigger enable is selectable for every Alarm and Warning (together) during configuration.
Engine running is detected, by exceeding a separately configurable threshold value: the Alarm and Warning enable engine speed threshold. The minimum threshold is 0 rpm and the maximum is 32.000 rpm.
An additional trigger-enable time delay starting from engine running condition can be configured. This is helpfull in cases, where it takes a while until a pressure is built up. This delay time is settable from 0 to 250 sec with a resolution of 1sec.
2. Functional Specification
Product Manual
T/°C
time/sec
105 103
110 108
Warning
on
Alarm on
Alarm off
Warning off
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Page 29
2.5.4.5 Alarm and Warning State Diagram (Maximum Value Algorithm)
2. Functional Specification
Product Manual
VALUE
Warning
Time delay
Time delay
Display Warning Indication *
Alarm
Value > WarnLev el
Value > Alar m Level
Display Alarm Indication *
Reminder: Alarm li s t and flas hing Ala r m symbol and WIN gauge "Alarm Action"
Re mi nder: Warning list an d WI Ngauge "Alarm Action"
?
Value > WarnLev el
Value < WarnLevel - Hysteresi s
Value < Alar m Lev el
?
Value > AlarmLevel + Hysteresis
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Page 30
Alarm and Warning State Diagram (Minimum Value Algorithm)
2. Functional Specification
Product Manual
VALUE
Warning
Time delay
Time delay
Display Warning Indication *
Alarm
Value <= WarnLevel
Value <= AlarmLevel
Display Alarm Indication *
Reminder: Alarm list and flashing Alarm symbol and WINgauge "Alarm Action"
Reminder: Warning list and WINgauge "Alarm Action"
Value <= WarnLevel
Value < WarnLevel - Hysteresis
Value <= AlarmLevel
Value > AlarmLevel + H yster es is
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Page 31
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2.5.5 Service
The Service message is based on the Hourmeter or Odometer.The service message indication can be configured via WINgauge. There are 15 independent service messages with customer specific settings, which can be configured via WINgauge. The service messages are implemented as periodic intervals. Amessage which should be indicated only once, the quantity of intervals would then be 0. Configuration data is stored in EEPROM.
For each of the 15 Service messages following can be specified in a table:
1. Service code number: Range: 1 to 255. 0 needs to be entered to disable this service function.
2. First message after x hours: ( 1h <= x <= 65.000 h )
3. Periodic service time: Range: 1h to 4.095h. If 0h is selected, it means only once (not periodic).
If a Service message has expired, this service code is displayed as a decimal number together with the common service symbol on the dot-matrix display. The Service message display remains active until this service code is reseted.
2.5.5.1 Reset of Service messages
The reset of the service message function is possible first if it occured and not before.
When a one-time service message will be reseted, then this Service message will be disabled by writing 0 into the service code field of the Service message table in EEPROM.
When a periodic interval will be reseted then the periodic service time will be added to the hours of the current hourmeter va­lue. This will ensure, that even if a Service message is reseted later than required, the time to the next service indication will be the periodic interval time as specified.
Example: Service message No.: 12
Service code: 153 First service after: 300 h Periodic service:100 h
The reset of the Service message is part of the system check function (part of safety check).
Procedure for resetting a Service message:
1. With ignition switched off, push the button and hold down while ignition is being turned on, then the system check function is activated and clears the contents of the DTC List.
2. If there are any service messages active, then they will be displayed on the Dot-Matrix Display starting with the first active service message. If the button is then pressed and held for 5 seconds or longer, then this Service message will be rese­ted. The next active Service message is displayed afterwards. To proceed to the next active service message without re­setting the displayed code the button needs to be pressed shortly (<5 sec). If all active service codes have been display­ed, then the system check function is started.
2. Functional Specification
Product Manual
Event Time (hourmeter) Display
First service code displayed after 300 h 153 Reset of this service at 340 h Next service display at 440 h 153
Page 32
2.5.6 CAN (SAE J1939) DTC (Diagnostic Trouble Codes) messages
It will be required to know the CAN source address (SA) of the controller (ECU), which has sent a DTC message, so that the problem can be located.
The SAE J1939 specifies 13 different diagnostic modes (DM1 to DM13). But for CANcockpit only DM1 is relevant. In DM1 active DTCs are broadcast on the CAN-Bus. Active means, that these faults are existing at the moment, compared to faults, which existed sometime in the past.
2.5.6.1 CAN SAE J1939 Elements
DTCs consist of 4 elements defined in SAE J1939:
1. Suspect Parameter Number (SPN) 19 bits
In the DTC, the SPN identifies the faulty element, component, sensor or parameter of a device (ECU).
2. Failure Mode Indicator (FMI) 5bits
The FMI defines the type of failure detected. It provides additional information about the nature of the fault. There are 32 pre­defined FMIs. Examples are: "Out of calibration", "Data Valid but above normal operational range", "Mechanical System not responding or out of adjust­ment"….
3. Occurrence Count (OC) 7bits
Shows the number of times a fault was active
4. SPN Conversion Method (CM) 1bit
The February 1996 version of SAE J1939-73 contained inadequate definitions to assure consistent implementations. Consequently the specification of the DTC format was changed. To indicate the new consistent format this bit must be set to 0. Also the old versions will be supported by CANcockpit.
The number of possible DTCs is very large, therefore efficient filtering is important for this function.
There are two main applications for DTCs (Diagnostic Trouble Codes):
To inform the operator, that something is not as expected. Depending on the DTC it can have the nature of an Alarm (most severe), Warning or only Information
To provide diagnostic information for the workshop, so that system faults can be analyzed and repaired.
2. Functional Specification
Product Manual
DTC
Data Byte 3 8 least significant bits of SPN
Data Byte 4 8 medium significant bits of SPN
Data Byte 5 3 most significant bits of SPN plus 5 bit FMI
Data Byte 6 Conversion Method bit plus 7 bit Occurrence Count.
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Page 33
2.5.6.2 CAN DTC Information Display Requirements
1. Information for the operator needs to be brief and clear, so that action can be taken quickly, if required.
Activate Warning Lamp
Activate Switch-Output
Display Short Text
2. For the workshop it is more important to get detailed information, so the cause can be found and fixed.
DTC List with SPN, FMI and Occurrence Count
The DTC List can also be viewed by the operator, but requires detailed knowledge of the CAN devices reporting the DTCs. Also it can be expected, that the workshop will have other diagnostic tools, which can access even more Information than J1939 DM1.
2.5.6.3 CAN DTC Display Functions
2.5.6.3.1 DTC Reception
0ne to five independent DTC channels can be configured. Every channel is able to receive the DTCs from one CAN device (Source Address). If DTCs are received from any of the configured CAN devices, they will be stored into a DTC receive buffer. The buffer will be able to hold a total of 40 DTCs and will be implemented as a ring buffer, so that old DTCs can be overwritten by newly recei­ved DTCs. Every newly received DTC will be compared with latest DTC`s in the ring buffer. If they are different it will be stored in the ring buffer. Thus avoid overflowing of the ring buffer by toggling transmitted DTC`s.
2.5.6.3.2 DTC List
If the service personnel or the operator wants to check for received DTCs, he can step through the display list until coming to the DTC-Displays. There will be no automatic display, which comes up and must then be acknowledged. Therefore it is possi­ble to prevent annoying displays coming up, if DTCs are received, which have no actual relevance.
The DTC List function will provide access to the DTCs inside the DTC receive buffer. One DTC Display will exist in the di­splay list for every configured DTC channel (channel 1 to 5).
To see the received DTCs of one channel the operator presses and holds the button for longer than 2sec. At this time the pro­cessor will transfer the received DTCs from the DTC Receive Ring Buffer to the DTC List. Only the DTCs of the selected channel will appear in the DTC List. The most recent DTC will be shown first. Every short press will lead to earlier received DTCs, until all DTCs have been shown or the button is pressed and held for more than 2sec.
The DTC List will be cleared at ignition off/ on (configurable).
2. Functional Specification
Product Manual
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Page 34
2.5.6.3.3 DTC List Display Format
One Graphic Symbol per DTC Channel (Source Address) can be configured and will be shown together with the DTC in the upper and lower level. It indicates, where the DTC message comes from. Also the number of received DTC`s on this channel (0-40) which are currently inside the DTC Ring Buffer will be displayed.
Examples:
Electronic Engine Controller (EEC) reports Pre-Filter Oil Pressure (SPN=1208) was 102 times (occurrence count) above normal operating range - most severe level (FMI=0). Index 10 provides information about the position inside the Ring Buffer.
Electronic Engine Controller (EEC) reports System Diagnostic Code #1 (SPN=611), occurrence count information not available (OC=127) and Special Instructions (FMI=14). Index 15 provides information about the position inside the Ring Buffer.
Electronic Transmission Controller (ETC) reports Clutch Actuator (SPN=788) was 2 times Out of Adjustment ((FMI=7) Index 18 provides information about the position inside the Ring Buffer.
Hydraulic Controller reports Hydraulic Reservoir Temperature (SPN=1508) one time Above Normal (FMI=3) Index 40 provides information about the position inside the Ring Buffer.
2. Functional Specification
Product Manual
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Page 35
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2.5.6.3.4 Diagnostic Lamp Status
The following diagnostic lamps are defined in SAE J1939:
1. Red Stop Lamp —> Stop Engine
2. Amber Warning Lamp
3. Protect Lamp
4. Malfunction Indicator Lamp
The status information of all configured DTC received channels are collected and the result will be stored in a 16bit status va­riable (Byte1 and Byte2). It is then possible to configure alarm or warning functions to react on the diagnostic lamp status. This also has the advantage that normal Alarm- or Warning-Functions are integrated with Alarms or Warnings (DTC Lamp Status) from the CAN Bus.
2.5.6.3.5 DTC Scan
When DTC`s are received via interrupt, they are immediately stored into the DTC-receive ring buffer. This ring buffer will then be scanned for 8 specific DTC`s. These DTC`s can be configured via WINgauge with unique icons and labels. Alarm and/ or Warning Functions can then be configured to trigger on the status of certain bits inside the DTC scan result register.
2.5.6.4 Speedometer Master Gauge
2.5.6.4.1 Tolerance
The overall speedometer accuracy is within 0% to +4% of full scale reading for each indicated value over the operating range of the instrument. This fulfills SAE J1226 for the American market and for the European market DIN 75521-2.
2. Functional Specification
Product Manual
SAE J1226 DIN 75 521 - 2
-4% 4% 0 <= v1-v2 <= v2/25 + 5km/h
Actual speed u. Tol. o. Tol. u. Tol. o. Tol.
0 0 0 10 9 ,6 10,4 20 19,2 20,8 30 28,8 31,2 40 38,4 41,6 40 46,6 50 48 52 50 57 60 57,6 62,4 60 67,4 70 67,2 72,8 70 77,8 80 76,8 83,2 80 88,2 90 86,4 93,6 90 98,6
100 96 104 100 109 110 105,6 114,4 110 119,4 120 115.2 124.8 120 129,8
Page 36
2.5.6.4.2 Speedometer Gauge Operation
The Master gauge receives speed information either via CAN or via one of the frequency inputs. During configuration the source of the speed information has to be defined. The input signal is first converted into a physical speed value. The micro­controller calculates the deflection angle of the speedometer based on this physical speed value and gauge output characteri­stic.
Specification of odometer storage
The standard Speedometer version of the Master gauge contains an Odometer. It can be configured that also the Tachometer can have an Odometer instead of an Hourmeter. The Odometer consists of a total Odometer and a Tripodometer. Both can be displayed on the dot matrix LCD as two lines. Format is 6 digits for total km, landmiles, nautical miles or meter and 4 di­gits, decimal point and 1 digit for 1/10 kilometer, land mile or nautical mile. The resolution of meter is 1m.
a. Information comes from CAN-Bus Interfaces (one of two):
For the Odometer indication it must be ensured that a ECU is broadcasting this information on the CAN-Bus. If no signal is received only dashes will be indicated.
b. Total odometer information generated by master gauge:
The Odometer information will be written to EEPROM every 1km. Aring counter algorithm is applied to save and recover the information from EEPROM. The rest-distance is written to EEPROM 10 sec after ignition has been turned off.
A special 16-word-ring-counter algorithm is applied to recover the odometer in case the battery was disconnected. With nominal input frequency applied, the odometer shall indicate calculated mileage within ± 0.3% [SAE J1226].
2. Functional Specification
Product Manual
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Page 37
2.5.6.5 Tachometer Master Gauge
2.5.6.5.1 Tolerance
The Tachometer indication must be within ± 2% of full scale with nominal voltage applied at temperature of 24 ± 3° C. [SAE J1399].
2.5.6.5.2 Tachometer Gauge Operation
The Master gauge receives the engine speed information either via CAN-Bus or via one of two frequency inputs. During confi­guration the source of the engine speed information has to be defined. The input signal is first converted into a physical engi­ne speed value. The micro-controller calculates the deflection angle of the Tachometer.
2.5.6.5.3 Specification of the hourmeter
The standard Tachometer version of the Master gauge contains an Hourmeter. It can be also configured with the WINgauge that also the Speedometer can contain an Hourmeter.
U
Legal demands are to fulfil!
a. Information comes from CAN-Bus Interfaces (one of two):
For the Hourmeter indication it must be ensured that a ECU is broadcasting this information on the CAN-Bus. If no signal is received only dashes will be indicated.
b. Total hours information generated by master gauge:
The Hourmeter counts the number of engine hours, when the engine speed exceeds a threshold value configurable via WINgauge (default value 300 rpm). If the engine speed is below the threshold value the hour counting stops (total and trip). The last value willI be stored within 10 sec in EEPROM after the ignition is turned off, then counting stops, no matter if the en­gine is running or not.
The time indication is within + 5 sec with nominal voltage supplied at 25 degrees C and within + 10 sec with nominal voltage supplied over the full operating temperature range. The total hour information is backed-up in EEPROM every 7.5 minutes. Aspecial 16-word-ring-counter algorithm is applied to recover total hours in case battery had been disconnected.
2. Functional Specification
Product Manual
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Page 38
3. Satellite Gauges
3.1 Mechanical concept
The movements are front mounted stepper motors SM2, only clockwise indication.
Connectors: AMP 6 Pin MATE-N-LOK
The dials have a 240° scale and a black panel effect for the warning lamps, so without activating of the warning lamp no sign is visible.
3.2 Fault modes
When ignition is off, the pointers are positioned 6° below the left side of the scales. With ignition on the pointers are moving to the scale start value. When the gauges receive wrong informations or the analog signals are out of range (configured by WINgauge), the pointers are moving 6° below the scale start value
2. Functional Specification
Product Manual
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Page 39
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3.3 Satellite gauge address
Each Satellite has his fixed address. The address is defined with the Assy PCB.
The matrix of the combination of the gauge type and address:
U
Maximum 16 Satellite gauges can be connected per Master. To avoid grave system conflicts, on each address is only one gauge allowed.
3.4 Warning Lamp inside the Satellite Gauge
All warning lamps are red except the amber level warning lamps. The WINgauge allows configuration of these warning lamps.
3.5 Tolerance
The Satellites have the pointer accuracy of ± 2.5%.
2. Functional Specification
Product Manual
Address Numbers of the Satellite gauges
00 Speedo / Tacho 1 01 Pressure Engine Oil 02 Pressure Brake 1 / Rudder / Primary air 03 Pressure Transmission Oil 04 Pressure Turbocharger / Tacho 2 05 Temperature Engine Oil 06 Temperature Transmission Oil 07 Coolant Water Temperature 08 Temperature Hydraulics Oil 09 Temperature without Symbol / Gear Oil 10 Pyrometer / Pressure Brake 2 / Turbo / Exhaust 11 Level, Fuel level 1 12 Level, Fresh Water / Cylinder Head / Position Rear Wheel 13 Level, Waste Water / Fuel Level 2 / Pressure Brake 2 (250 bar) / AddBlue / Winch 14 Voltmeter 15 Hydraulic Pressure / Ammeter / Pressure Brake 1(250 bar)
Page 40
A. Technical Data
Operating Temperature
Operating Temperature: -40°C to + 85°C (at nominal voltage) Visible restrictions: for LCD outside -20°C and +70°C
Storage Temperature
Storage temperature: -40°C to +85°C LCD Humidity resistance: +65°C ± 2°C
+2
90% r.F. -3%
Supply Voltage
Nominal Voltage: + 12 V and + 24 V Operating Voltage: + 10,5 V to + 32 V as standard Test voltage: + 14 V and + 28 V Total Supply Current: 200 mA ± 20% for Master and 110 mAper Satellite
Satellite supply: + 10,5V to + 32V, current consumption max. 2 A Sensor supply: + 8 V ± 10% (8 V - 0%, +10% at 24 V), Imax: 50 mA
Ground is connected to the negative battery terminal.
Idle Current
The Ignition off current (stand by mode) is 4 mA for the System (Master and Satellites).
Ground shift
Ground shift on non-analogue inputs are assumed to be < ± 0.5 V. i.e. all digital input have to work with an additional signal offset of ± 0.5 V
EMC Requirements
See enclosures
Overvoltage Protection
The Master can withstand a voltage of 56 V for 5 minutes without damage (SAE J1810).
I/O circuit protection
The gauges are protected against reversed battery polarity.
Cable requirement To the Master:
Type cross section: 0,5 mm²
From Master To Satellite
Type cross section: 0,75 mm² Max quantity of gauges: 16 Satellites
U
Max. cable length: 10 m from Master to the last daisy chained Satellite
2. Functional Specification
Product Manual
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Page 41
B. Applied Standards
2. Functional Specification
Product Manual
Technische Änderungen vorbehalten Technical details subject to change
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Accompanying Documents. For reference only
Document Description Version
SAE J1226 Electric speedometer specification 1983-02 SAE J1399 Electric tachometer specification 1984-06 SAE J1810 Electrical indicating system specification 1993-01
SAE J1939 Recommended practice for truck and bus control 2000-04 SAE J1939 / 11 Physical layer 1999-10 SAE J1939 / 21 Data link layer 2001-04 SAE J1939 / 31 Network layer 1997-12 SAE J1939 / 71 Vehicle application layer 2008-01 SAE J1939 / 81 Network management 2003-05
89/336/EWG
Applied Standards, Breakdown sending to the DIN/EN standards 50 081-1, 50 082-1, 50 082-2 (applied standards, disturbance acc to DIN/EN standards 50 081-1, 50 082-1, 50 082-2)
95/54 EWG Motor vehicle guideline EMV (vehicle guidance emc) 1995-10 DIN 40 839
Electromagnetic compatibility (emc) in road vehicles; disturbances conducted along supply lines in 12V and 24V onboard systems
1992-10
DIN 70 005 Teil 2 Graphische symbole, Grundlagen und Übersicht (graphic symbols, basis and overview) 1993-12 DIN 75 521 Teil 2 Speedometer instrument panel mounting for motor vehicles 1992-02
DIN-EN 50081-1 Electromagnetic compatibility - generic emission 1993-03
DIN-EN 50 081-2 Electromagnetic compatibility - industrial environment 1994-03
DIN-EN 50082-1 Electromagnetic compatibility - generic immunity emission 1997-11 DIN-EN 50082-2 Electromagnetic compatibility - generic immunity industrial environment 1996-02
IEC 60068-2-11 Corrosion resistance 1995-10
EN IEC 60 529 Schutzarten durch Gehäuse 1991-10
ISO 2575 Road vehicles - symbols for controls, indicators and telltales 2000-03
ISO 3767-1
Tractors, machinery for agricultural and forestry powered lawn and garden equipment ­symbols for operator controls and other displays.
1998-12
ISO 6405-1 Earth-moving machinery - symbols for operator controls and other displays 1991-12
ISO 7000 Graphic symbols for use on equipment - index and synopsis 1989-11
ISO 7637-1-2 Road vehicles - electrical disturbance by conduction and coupling: 1990-06
UL 94
Part 1: passenger cars and light commercial vehicles with nominal 12V supply voltage ­electrical transient conduction along supply lines only
1998-10
TPV
Part 2: commercial cars with nominal 24V supply voltage - electrical transient conduction along supply lines only
1998-10
ISM-Z Test for flammability of plastic materials for parts in devices and appliances 2000-07
VDON 2.1954.001
Technical test specification for mechanical and electronic information systems in motor ve­hicles
1997-12
VDON 2.1955.070
Specification: customer specific integrated circuit in cmos technology for control of vdo­stepper motors (SM2/ MW2000)
1997-12
VDON 2.1958.001 Company sign VDO 2000-12
Page 42
Enclosures
Installation instructions TU00-0736-5107120 0609 (Page 1-8)
3. Installation Instructions
Product Manual
Technische Änderungen vorbehalten Technical details subject to change
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Page 43
www.vdo.com
CANcockpit
Neue Generation I New Generation 2009
Montageanleitung I Installation Instructions
VDO - eine Marke des Continental-Konzerns / VDO - Atrademark of the Continental Corporation
Page 44
Systemkomponenten System components
Gerät Gauge
Master-Gerät (Gehäuse Ø 80mm) Master gauge (housing dia. 80mm)
Slave-Gerät (Gehäuse Ø 52mm) Satelitte gauge (housing dia. 52mm)
Kabelbaum Master (26polig), Wiring harness master (26-pole) Bestell-Nr. / Order No.: A2C53041729
3000 mm
200 mm
200 mm
Kabelbaum Master - Slave Wiring harness master - satelitte Bestell-Nr. / Order No.: A2C53344035
Kabelbaum Slave - Slave Wiring harness satelitte - satelitte Bestell-Nr. / Order No.: A2C53344036
Dichtring Seal ring
Schraubring Clamp ring
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 1
TU00-0736-5107120 0609
Montageanleitung Installation Instructions
Page 45
Montageanleitung Installation Instructions
Oder eigener Zusammenbau der Kabelbäume. Nur mit folgenden Teilen: Or own installation of the wiring harnesses. With following parts only:
8
1
4
5
6
9
7
10
11
12
13
15
14
16
17
3
2
Anwendung / Application: A: für Kabelbaum Master (26polig) / for wiring harness master (26-pole) B: für Kabelbaum Master - Slave / for wiring harness master - satelitte C: für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 2TU00-0736-5107120 0609
Pos. Pos.
Bezeichnung Designation
Anwendung
Application
Verp.-Einheit Items / Package
Bestell-Nr. Order No.
1 Handzange / Hand tool AMPMODU A (AMP-Nr./ No. 0-0169481-1) 2 Gehäuse /Housing AMPMODU A 700 3 Abzugsbügel / Draw-off bracket AMPMODU A 600 4 Kontaktsicherung / Contact seal AMPMODU A 2000 5 Kontaktgehäuse / Contact housing AMPMODU A 500 6 Kontakt (Master) / Contact (master) AMPMODU A 10000 7 Ausstoßwerkzeug / Push out tool AMPMODU A 2 8
Kabel 0,5mm2 / Wire 0.5mm
2
A
9 Kabelbinder / Cable strap A, B, C — 10 Handzange / Hand tool MATE-N-LOK B, C (AMP-Nr./ No. 0-0734202-1) 11 Stecker, 4polig / Connector, 4-pole MATE-N-LOK B 500 12 Stecker, 6polig / Connector, 6-pole MATE-N-LOK B, C 1000 13 Kontakt / Pin MATE-N-LOK B, C 10000 14 Ausstoßwerkzeug / Push out tool MATE-N-LOK B, C 2 15
Kabel, gelb 0,75mm2 / Wire, yellow 0.75mm
2
B, C
16
Kabel, rot 0,75mm2 / Wire, red 0.75mm
2
B, C
17
Kabel, schwarz 0,75mm2 / Wire, black 0.75mm
2
B, C
Page 46
Montageanleitung Installation Instructions
14
1
26 13
A: für Kabelbaum Master (26polig) / for wiring harness master (26-pole)
Mit den Kontakten (Pos. 6) und den entsprechenden Kabeln (Pos. 8) eine Crimpverbindung nach EN 60352-2/A1 Teil 2 herstellen. Make a crimp connection per EN 60352-2/A1 Part 2 with the contacts (Pos. 6) and the corresponding cables (Pos. 8).
Dabei besonders darauf achten, dass alle Einzeldrähte des
Kabels von der Crimphülse erfasst werden, denn sonst besteht Kurzschlussgefahr! Take special care to contain all individual wires of the
cable in the crimp socket to avoid the risk of a short-circuit!
Die Kabel je nach Belegung in das 26polige Kontaktgehäuse (Pos. 5) einstecken. Die Kontakte müssen hörbar einrasten. Insert the cabels into the 26-pole contact housing (Pos. 5) according to connector pin allocation. The contacts must engage with an audible click.
Pin-Belegung Pin allocation
A1
A2
A3
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 3TU00-0736-5107120 0609
Pin Beschreibung / Description Pin Beschreibung / Description
1 Kl. 30 / Power Supply (terminal 30) 14 + 8 V DC für Geber / for Sensor supply
2 Kl. 31 / GND (terminal 31) 15 0 - 5 V DC Eingang / Input
3 CAN1 _High 16 Kl. 58 d / Illumination (terminal 58 d)
4 CAN1 _Low 17 Kl. 15 / Ignition (terminal 15)
5 CAN2 _High 18 Frequenzeingang 2 / Frequency Input 2 (0-2 kHz)
6 CAN2 _Low 19 Frequenzeingang 1 / Frequency Input 1 (0-40 kHz)
7 nicht belegt / not connected 20 Schaltausgang 1 / Switch-Output 1
8 k - Line 21 Schaltausgang 2 / Switch-Output 2
9 Analog Eingang 1 / Input 1 (0,5-200 Ohm) 22 nicht belegt / not connected 10 Analog Eingang 2 / Input 2 (0,5-300 Ohm) 23 nicht belegt / not connected 11 Analog Eingang 3 / Input 3 (10 -700 Ohm) 24 Externer Schalter / External Switch 12 4 - 20 mA Eingang / Input 25 Masse Analog / Analog GND 13 4 - 20 mA Masse / GND 26 Masse Frequenz / Frequency GND
Page 47
Montageanleitung Installation Instructions
B: für Kabelbaum Master - Slave / for wiring harness master - satelitte C: für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte
A: für Kabelbaum Master (26polig) / for wiring harness master (26-pole)
Beispiel / Example
Ausstoßwerkzeug / Push out tool (Pos. 7)
Mit den Kontakten (Pos. 13) und den entsprechenden Kabeln (Pos. 15, 16, 17) eine Crimpverbindung nach EN 60352-2/A1 Teil 2 herstellen. Make a crimp connection per EN 60352-2/A1 Part 2 with the contacts (Pos. 13) and the corresponding cables (Pos. 15, 16, 17).
Dabei besonders darauf achten, dass alle Einzeldrähte des Kabels von der Crimphülse erfasst werden, denn
sonst besteht Kurzschlussgefahr! Take special care to contain all individual wires of the cable in the crimp socket to avoid the risk of a short-circuit!
B1
C1
A5A4
A6
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 4TU00-0736-5107120 0609
Page 48
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 5TU00-0736-5107120 0609
Montageanleitung Installation Instructions
B: für Kabelbaum Master - Slave / for wiring harness master - satelitte C: für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte
Ausstoßwerkzeug (Pos. 14) Push out tool
Die Kabel (Pos. 15, 16, 17) je nach Belegung in den 4poligen (Pos. 11) / 6poligen Stecker (Pos. 12) einstecken. Die Kontakte müssen hörbar einrasten. Insert the cabels (Pos. 15, 16, 17) into the 4-pole (Pos. 11) / 6-pole connector (Pos. 12) according to connector pin alloca­tion. The pins must engage with an audible click.
B2
B3
C2
rot red
schwarz black
gelb yellow
rot red
schwarz black
gelb yellow
rot red
schwarz black
gelb yellow
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Montageanleitung Installation Instructions
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(1-8) - 6TU00-0736-5107120 0609
0,5 mm bis/to 8 mm
54 mm
Slave-Gerät Satellite gauge
Master-Gerät Master gauge
Kabelbaum Slave - Slave Wiring harness satelitte - satelitte
Kabelbaum Master - Slave Wiring harness master - satelitte
70,2 mm
Ø 52 mm
Ø 53 mm
Ø 81 mm
0,5 mm bis/to 8 mm
rot schwarz gelb red black yellow
Ø 80 mm
Page 50
Montageanleitung Installation Instructions
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 7TU00-0736-5107120 0609
Beispiel / Example
Page 51
Montageanleitung Installation Instructions
Technische Änderungen vorbehalten Technical details subject to change
(1-8) - 8TU00-0736-5107120 0609
Beispiel / Example
Kabel-Belegung cable allocation
Geräteanschluss Gauge connection
Kabelbaum Master Wiring harness master
Pin Beschreibung / Description Pin Beschreibung / Description
1 Kl. 30 / Power Supply (terminal 30) 14 + 8 V DC für Geber / for Sensor supply 2 Kl. 31 / GND (terminal 31) 15 0 - 5 V DC Eingang / Input 3 CAN1 _High 16 Kl. 58 d / Illumination (terminal 58 d) 4 CAN1 _Low 17 Kl. 15 / Ignition (terminal 15) 5 CAN2 _High 18 Frequenzeingang 2 / Frequency Input 2 (0-2 kHz) 6 CAN2 _Low 19 Frequenzeingang 1 / Frequency Input 1 (0-40 kHz) 7 nicht belegt / not connected 20 Schaltausgang 1 / Switch-Output 1 8 k - Line 21 Schaltausgang 2 / Switch-Output 2
9 Analog Eingang 1 / Input 1 (0,5-200 Ohm) 22 nicht belegt / not connected 10 Analog Eingang 2 / Input 2 (0,5-300 Ohm) 23 nicht belegt / not connected 11 Analog Eingang 3 / Input 3 (10 -700 Ohm) 24 Externer Schalter / External Switch 12 4 - 20 mA Eingang / Input 25 Masse Analog / Analog GND 13 4 - 20 mA Masse / GND 26 Masse Frequenz / Frequency GND
Page 52
5. Software Description
Product Manual
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Enclosures
WinGauge Software 0303 (Page 1-53)
Page 53
June 2009
Training WinGauge Software
page 1
Page 54
Components and Concept
June 2009
Training WinGauge Software
page 2
Page 55
Example of a fully configured Instrumentation
June 2009
Training WinGauge Software
page 3
Page 56
Example of a fully configured Instrumentation cont.
June 2009
Training WinGauge Software
page 4
Page 57
Basic Steps to build a new Configuration:
1. Definition of Project Properties
2. Adding a Master Instrument
3. Adding the required Slaves or Displays
4. Configuration of Master, Slave- and Display Instruments.
5. Save Configuration
6. Test / Diagnose the new Configuration.
June 2009
Training WinGauge Software
page 5
Page 58
Definition of Project Properties
June 2009
Date and Time will be added to the „Created / Last modification“ fields, after the configuration has been saved the first time. The „Last modification“ field receives an update every time changes are made to the project.
Training WinGauge Software
page 6
Page 59
2.) Adding a Master Instrument
By execution of the commands "Edit – Add Master" alternative "right mouse button – Add Master" shows the following dialog by which the required Master can be chosen from the Data Base.
June 2009
After confirmation with „OK“ a picture of the selected Master is shown in the overview dialog "Configuration-Window"
Training WinGauge Software
page 7
Page 60
TACHO and SPEEDO Instruments can be chosen from a broad variety of instruments.
June 2009
Training WinGauge Software
page 8
Page 61
The left screen part, "Navigation-Window" shows the Configuration. Subcategories show up after a mouse-click to "+" on the left side near the configured device (Master/Slave/Display).
The right part of the overview screen, the "Configuration-Window " is used to show a picture of the selected Master, Slave or Display devices in addition with the characteristic parameter values e.g. Part No., Type, Primary- and Secondary Range, potential Sensor type and Address, During the configuring process of the different devices, this window shall be used to set all required parameters.
With a click to " Subcategories view is
closed again.
June 2009
-" the
Training WinGauge Software
page 9
Page 62
3.) Adding the required Satellites
By execution of the commands "Edit – Add Slave" alternative "right mouse button – Add Slave" shows the following dialog by which the required Satellite can be chosen from the Data Base.
June 2009
After confirmation with "OK" a picture image of the selected Satellite is shown in the overview dialog "Configuration-Window"
Training WinGauge Software
page 10
Page 63
This shows the Selection of possible Satellites for the System like: Pressure, Temperature, Level, Voltage,
Current, Speedometer, Tachometer and Various.
June 2009
Training WinGauge Software
page 11
Page 64
3.) Adding the required Satellites
This shows the Selection of possible Sensors for the various Satellite types like: Pressure,
Temperature, Level, Voltage, Current, Speedometer, Various and Tachometer.
June 2009
Training WinGauge Software
page 12
Page 65
The first two Instruments for the requested configuration are added now. Parallel to the last steps the system can be expanded with additional Satellite instruments
June 2009
Training WinGauge Software
page 13
Page 66
June 2009
Training WinGauge Software
page 14
Page 67
June 2009
Training WinGauge Software
page 15
Page 68
3.) Adding the required Displays
By execution of the commands "Edit – Add Display" alternative "right mouse button – Add Display" shows the following dialog by which the required Display can be chosen from the Data Base.
June 2009
After confirmation with "OK" a symbol representing the selected Display is shown in the overview dialog "Configuration-Window"
Training WinGauge Software
page 16
Page 69
This shows the Selection of possible Displays for the System like: Pressure, Temperature, Level, Voltage,
Current, Speedometer, Tachometer and Various.
June 2009
Training WinGauge Software
page 17
Page 70
This shows now the Basic System - Configuration including the essential blocks like: Master, three Satellites and one Display. However, the parameter Settings are only standard and don‘t match the required functions. This must be adopted later. Before the configuration of the details for this system can be started, it‘s required to add the other missing components.
June 2009
Training WinGauge Software
page 18
Page 71
In the "Navigation- Window" it can be followed, how the whole System builds up to completion. Certainly this shows also which parts of the detailed configuration need to be performed next. Remarkable are the missing symbols and the commonly used name – General -
Due to the size of this very complex Configuration it‘s necessary to understand that part of the configuration continues in the invisible part of the "Configuration-Window" . Using the roll-bar on the right side of the window may help to pull the non visible part up.
June 2009
Training WinGauge Software
page 19
Page 72
Rolling the screen up, the other configured Displays inclusive their characteristic values defined up to this point are visible. With the next step the basic Configuration shall be completed in a way that it matches the requested layout.
June 2009
Training WinGauge Software
page 20
Page 73
Exemplary for the other Displays the necessary modifications shall be implemented for one unit. The two arrows show the pair of views belonging to one Display unit. By clicking to the chosen Display in the "Navigation-Window" a new dialog window opens up in the "Configuration-Window".
June 2009
Training WinGauge Software
page 21
Page 74
If a Symbol cannot be found amongst the predefined list of Symbols, this particular one can be created new through the use of the "ICON Editor". The ICON Editor is started up by "Edit – ICON Editor".
This information is already known from the „Add Display“ configuration.
1. Step: Overwrite the name from „General“ to „Fuel Temperature“
2. Step: Select the requested Trailing digits for the particular device. Will be visible on the Master Display.
3. Step: Choose the Unit (km/h, °C, h,…) for the Display
5. Step: Enter any descriptive text which shows up later in the Master Display.
6. Step: By selection of a Hysteresis-value an interval which helps to stabilize the display of the physical value in the Master Display is defined.
4. Step: Select the appropriate Symbol for „Fuel Temperature“ from a list of predefined, standardized Symbols by clicking to the Symbol select button and role up or down in the pull-down-list.
This dialog is closed by selection of another device Master, Satellite or Display in the "Navigation-Window"
June 2009
Training WinGauge Software
page 22
Page 75
The performed modifications can be recognized after returning back to the specification view for the just configured Display.
Contrary to a Satellite device, a Display has no other option than to view the measured values via the Display in the Master unit of the System. In accordance to this a switch to show the physical Value in Display is not available here.
June 2009
Training WinGauge Software
page 23
Page 76
The modifications made are as well visible in the overview screen.
Applying the recent described steps to the remaining Displays generates a complete basic Confi guration which includes:
a) All essential Components for the configuration and b) All the Symbols, Units, descriptive Texts, trailing Digits and Hysteresis values belonging to them.
June 2009
Training WinGauge Software
page 24
Page 77
At this point it’s easy to realize which Satellites still have not the right Symbols assigned. By use of the ICON Editor these Symbols are now created and can be assigned to the appropriate device.
Up to now basic configuration values like Name, Symbol, Unit, trailing Digits and Hysteresis values have been defined. This parameter setting is dedicated to present the individual device values in the Master Display. After creation of the missing Symbols plus the assignment to the correct device the next step is to define the In/Out characteristics for each device. Doing this implies that for each device, Master, Satellite or Display, the right Sensor is assigned and configured.
Searching for Satellites or Displays which haven’t received the full configuration is made easier when pointing with the mouse pointer to the “CAN 1” sign on the upper right corner of each device in the "Configuration-Window" . This opens up a window with all the CAN Parameter settings. A device is not configured when essential parameters are preset by "0".
June 2009
Training WinGauge Software
page 25
Page 78
ICON Editor
The ICON Editor is accessible via the function
"Edit – ICON Editor".
This routine is used to define nonexistent new Symbols or any kind of Logo. While the Symbols are represented in a square of 24 x 24 pixel, the Logo is defined in a rectangle of 24 x 87 pixel. Any new defined Symbol / Logo will be automatically added to the existent Symbol-list and is saved together with the project information. New defined Logos and Symbols can be saved to disc too.
June 2009
Training WinGauge Software
page 26
Page 79
The new created logo plus all the new defined Symbols are added sequentially to the Symbol table. The Logo however must be defined as Icon selection number 1. It requires the equivalent space of 3 Symbols. Logo and Symbols are immediately visible after creation and confirmation with "OK" in the Symbol list and can be selected for the appropriate device.
To help design a new Symbol / Logo the ICON Editor provides small utility tools on the top part of the window. The small white square shows the designed Symbols in the later size. Icon selection is used to define the position for the Symbols in the memory of the Icon Editor as well as for later reference. The checkbox for the Logo opens up a larger, rectangular pixel window.
June 2009
Training WinGauge Software
page 27
Page 80
Examples of new defined Symbols.
June 2009
Training WinGauge Software
page 28
Page 81
New created Symbols may be saved in a file for later use by the function:
"File – Save Icon".
In the same way the function
"File – Load Icon"
may be used to load a Symbol which has been defined at an earlier state. It is important to watch if the checkbox for Logo is checked or not. If it’s checked, a Logo is expected to be loaded. This differentiation is necessary because a Logo occupies the space for 3 Symbols and requires different treatment.
June 2009
Training WinGauge Software
page 29
Page 82
Now Master, Satellites and Displays are completed with the correct and required Symbols.
The assignment of the new defined Symbols works as described in the previous steps.
1.) Select the Device without Symbol or with Symbol to be exchanged.
2.) Pick the new created Symbol from the Symbol list.
3.) Close this step by selecting another Device of choice.
June 2009
Training WinGauge Software
page 30
Page 83
The next task to perform is:
Definition of the In/Out Characteristics
By a click to the "+" sign on the left of the Satellite in the "Navigation- Window" two more sub categories pop up:
In / Out characteristics and
Warnings & Alarms
As a mater of fact, these two new categories are available for all Satellites, Master and Displays.
June 2009
Training WinGauge Software
page 31
Page 84
Master, Satellite and Display may receive the required information, from the Sensors directly connected to the Master Instrument. The differentiation is amongst Resistor-, Current-, Voltage and Frequency Inputs. CAN1 and CAN2 may deliver information from other Sensors however.
June 2009
All Satellites, Master or Display being upsetted in the previous configuration process have in their configuration "CAN1" defined as the preferred Signal Source. The next steps will show how to connect the right Sensors to the correct Satellite.
Training WinGauge Software
page 32
Page 85
The dialog "Add Display" has preconfigured the "Speed" device. E.g. the Signal Source is been presetted with "CAN1" and the Curve is defined as linear with standard Values. For the definition of the Prime Range those two values have to be corrected. However it’s more important for Satellite than for Display devices, as Displays don’t really have a upper limit, but are showing their Values in the LCD Display of the Master Device. The first step here is to select as Signal Source the Frequency input 1 (0 – 40 kHz).
Typically the required Parameters for this part of the Configuration are predefined as they depend very much on the physical Instruments like Signal Source, Switches, Sensors… which are connected in the System. Those Parameters may be taken from the Hardware Configuration. It is recommended to have these Characteristic Values of the Sensors available before the Software Configuration via WinGauge is started.
June 2009
Training WinGauge Software
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Further Specification of the Frequency Input happens by using the function "Configure". Required Parameters for this Configuration are, the k-value (characteristic Value for the Frequency Input) and the max. velocity value. The starting point will be assumed as “0” for Velocity and Frequency. From those factors the max. Frequency value will be calculated as well as the 8 value pairs (Hz and km/h) which are filled in the table and are displayed as a curve.
June 2009
The k-value is a very sensor specific defined value. It can however be determined by the "Calculate" - function. To execute this function is only meaningful if it can be done in a vehicle.
Training WinGauge Software
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On exit of the Configuration for the "Speed – Display" the last configured values will be activated and displayed. For the other Displays with Frequency Input the same steps have to be performed again.
June 2009
Training WinGauge Software
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The green lines are shown when the "Show pointer position" box is checked. They shows the values in degree for the angle Phi [°] from the table below. This can be used as test if the values in the table seem to be correct.
For Signal Sources delivering their information via the CAN­BUS System, it’s enough to build the pair relationship for unit in (%, km/h, bar, °C) to the angle Phi [°] for the Pointer position.
June 2009
Satellite instruments do require as an additional specification the pair relationship between the physical measured values (mA, Ohm, V, Hz, ) and the unit ( %, km/h, °C..).
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Based on the Satellite function, in this case "Cooling Water Temperature", the right CAN Sensor needs to be chosen. By the SAE J1939 PGN Number the Sensors are described in detail. In this example it is “65262”. This shall make it easier to select the correct CAN Sensor.
June 2009
Training WinGauge Software
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CAN settings, Load CAN Message and define new CAN Sensor.
The function "CAN Settings" shows up in various dialogs. This other dialogs can be opened to get into a more detailed specification mode for the CAN Sensors. To configure those Sensors however, very detailed and specific knowledge about the Sensors, the environment where they are used as well as the specific parameters are required.
Note: Changes to the predefined Parameters shall only be made, if the adequate level of knowledge is avail.
June 2009
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A "Level-lever-type-sensor" with a resistor range of 3-180 Ohm has been selected for the Fuel Display. When choosing a predefined Sensor, all table values "Input" and "Display" are automatically presetted, as soon as the selection is confirmed with "OK". At the same time the adequate curve is displayed beside.
June 2009
Adjustments to the table values can be made as easy as just override the presented value in the table above. Be aware of later impact of this change.
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Add Sensor Data / Define Sensor Characteristics
The function "Load sensor data" shows up in various dialogs. This allows to select the preferred Sensor from a list of predefined Sensors. If required, a "New" Sensor can be defined too. Those self defined Sensors will be found later under the type "User defined". Configuration of a new Sensor requires good knowledge of the Sensors, the environment, the physical characteristics and the exact parameters. Note: Changing the initial values may only be performed with the appropriate knowledge and care.
June 2009
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The function "Check analog input signals" is activated by a click on the checkbox and verifies continuously if the Signal source operates correct. The test operates within a given min/max. range of values. A Sensor defect Signal will be triggered in case the Signal values are outside the defined min/max. range for more that a time specified in the delay field. This Sensor defect Signal is visualized in the Satellite through moving the pointer to the left down (0) position. For Displays, the Sensor Symbol is shown together with a row of “--------“in the Master Display.
The checking function should be activated for every Sensor!
The left and right side of the white field marks the min. / max. values of the range to check the analog input signals.
June 2009
Equivalent to the previous steps the Configuration for the remaining Master, Satellite and Display devices has to be performed. After that the specification process for the input side of the Configuration is essentially completed.
Training WinGauge Software
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The specifications of the output side for all components of the Configuration: Master, Satellites and Displays is equivalent, excepting only few differences. In the In/Out characteristics dialog it is possible to define individual Warnings and Alarms for each Sensor. After assigning a Priority, the selection of the preferred Symbol, the Warning and Alarm Threshold shall be defined. When these min/max values are passed, Warning / Alert shall be triggered.
Delay specifies the time to wait after the event occurred until the Warning / Alarm is made visible.
By use of the Algorithm the Threshold value is defined as upper/lower limit. The value in the Hysteresis field specifies the difference value after which the Warning / Alarm can be vanished.
June 2009
This overview field is only available for the Master Instrument. Here are the Warning / Alarm conditions for all instruments listed which have such conditions set.
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Activation of configured Satellites warning lamps check at "Ignition on". No function indicates a possible external wiring fault!
Activation of Master switch output check at "Ignition on". No function indicates a possible external wiring fault!
June 2009
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"Minimum engine start time" and "rpm threshold" defines the operating conditions needed to be achieved before any Warning / Alarm for this Instrument is meaningful to be triggered.. The "Flash interval" defines the flashing-frequency for all Warning LED’s in the Satellites used to signalize Warnings and Alarms. All the three Parameters are valid for all Devices in the same way.
Selection for the "Maximum / Minimum" limit means that the value shall not grow larger or fall lower than the threshold. The selection for "with / without RPM" means that the values shall not be valid for Warning / Alarm signaling before the RPM threshold, defined for the whole configuration, is reached.
June 2009
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Example: It‘s defined with a priority 5, that Alarm shall be initiated as soon as the Cooling Water Temperature has been reached above 103°C for longer than the delay time of 3 sec. Switching on Output1 and the Warning Lamp in the Cooling Water Satellite the Alarm is visualized. At the same time the Symbol for Cooling Water Temp. together with the actual physical value will be shown in the Master Display. Cooling down by more than 3°C to below 100°C the Warning Lamp in the Satellite together with the Output1 Signal is switched off again. The Warning message in the Master Display disappears after manual confirmation by pushing the button on the Master Instrument. These actions, to take back the Warning / Alarm are implicitly defined by setting the value for the Hysteresis.
June 2009
Training WinGauge Software
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A picture image of the selected instrument is only available for Master and Slave Devices, not for Displays.
Only a few special specifications which are only valid for the Master Instrument are left to be set before the Configuration will be completed. These specifications are: Default settings, Service Messages and CAN messages (DTC). Those three will be shown on the following pages.
To bring up a Logo in the Master Display with "Ignition on", this check box has to be activated.
June 2009
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The listed Parameters in the description frame are already known from the "Add-Master dialog". This information will be enhanced with information about the selected Sensor / Signal source for the Hourmeter respective the ODO-Meter. In essence the selection process is the same as for the In/Out Characteristics. But here no curve will be shown.
June 2009
It’s required to define for either the ODO-Meter or Hourmeter which the Signal Sources are. Is it a CAN device or a Sensor connected directly to the Master device. Further the parameters for Unit, RPM threshold, Total Distance/Hours or Trip Distance /Hours need to be defined / selected. The selected Symbol will be the Symbol for the Master device showing the values of the respective Sensor, Hours or ODO.
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This dialog is used to configure the Display of Service-Message numbers after a predefined interval (h / km depending if the Master is defined as Hourmeter or ODOmeter), to allow maintenance tasks to be performed in time. Depending on the Service Codes there may be different intervals set for the first notification and the following intervals. In this example Service­Message no. 1 is shown after 150 h and then with a frequency of 150 h again. Service-Message no. 5 shall be repeated after all 500 operating hours. The meaning of the Service-Message numbers needs to be predefined by the manufacturer and should be described in the documentation joining the vehicle.
June 2009
Training WinGauge Software
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