VDO CANcockpit Series Product Manual

New generation 2009 flexible instrumentation with can bus technology

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www.vdo.com

CANcockpit

New Generation 2009

Flexible instrumentation with CAN bus technology

VDO - eine Marke des Continental-Konzerns / VDO - A trademark of the Continental Corporation

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Summary of Contents for VDO CANcockpit Series

Page 1 Product Manual www.vdo.com CANcockpit New Generation 2009 Flexible instrumentation with CAN bus technology VDO - eine Marke des Continental-Konzerns / VDO - A trademark of the Continental Corporation...
Page 2 Product Manual Overview of Chapter Topic Chapter Safety Instructions Description of Functions Installation Instructions Testing Instructions Software-Description System Components, Spare Parts and Accessories Data Sheets General Information Sales and Service Informations = 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.
Page 3 Product Manual 1. Safety Instructions Contents Contents 1.1 Installation Before installation During installation After installation 1.2 Electrical Connection 1.3 Sensors 1.3.1 Pressure Sensor for Oil 1.3.2 Temperature Sensor for Oil 1.3.3 Temperature Sensor for Engine Coolant 1.3.4 Fuel Level Sensor (Lever Type Sensor/Tubular Type Sensor) 0609 1 - 1 TU00-0736-0000002...
Page 4: Safety Instructions
Product Manual 1. Safety Instructions 1.1 Installation No smoking! No naked flames or lights! • 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 •...
Page 5 Product Manual 1. Safety Instructions 1.1 Installation During installation • During installation make sure that the product's components do not affect or restrict vehicle functions and are themsel- ves 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.
Page 6: Electrical Connection
Product Manual 1. Safety Instructions 1.2 Electrical Connection Connect the cables in accordance with the electrical connection diagram. • 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. •...
Page 7 Product Manual 1. Safety Instructions 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.
Page 8 Product Manual 1. Safety Instructions 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.
Page 9 Product Manual 1. Safety Instructions 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.
Page 10 Product Manual 1. Safety Instructions 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.
Page 11: Table Of Contents
Product Manual 2. Functional Specification Contents Contents 1. System 1.1 Main Features 1.1.1 Block Diagram CANcockpit 1.2 Mechanical Concept 1.3 Safety Concept 1.3.1 Sensors 1.3.2 System Check 1.3.3 Satbus 1.3.4 WINgauge 2. Master Gauges 2.1 General Features 2.1.1 Main Functions 2.2 Mechanical Concept 2.2.1 Master dia.
Page 12: Table Of Contents
Product Manual 2. Functional Specification 2.5.5 Service 2.5.5.1 Reset of Service messages 2.5.6 CAN (SAE J1939) DTC (Diagnostic Trouble Codes) messages 2.5.6.1 CAN SAE J1939 Elements 2.5.6.2 CAN DTC Information Display Requirements 2.5.6.3 CAN DTC Display Functions 2.5.6.4 Speedometer Master Gauge 2.5.6.5 Tachometer Master Gauge 3.
Page 13: System
Product Manual 2. Functional Specification 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) •...
Page 14: Safety Concept
Product Manual 2. Functional Specification 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.
Page 15: Master Gauges
Product Manual 2. Functional Specification 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.
Page 16: Mechanical Concept
Product Manual 2. Functional Specification 2.2 Mechanical Concept As the same LCD is used for different Master gauge diameters the pointer position has different eccentricities and indication angles. Gauge diameter [mm] Eccentricity [mm] Indication angle 210° 216° 206° The connectors are 26-Pin MODU II-Connector and 4-Pin MATE-N-LOK from AMP. 2.2.1 Master dia.
Page 17: Input Signal Processing
Product Manual 2. Functional Specification 2.3 Input Signal Processing 2.3.1 Analog Inputs All sensor characteristics can be defined with the WINgauge Software. 2.3.1.1Grounding 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;...
Page 18: Input Signal Processing For Canbus Messages
Product Manual 2. Functional Specification 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.
Page 19: Pin Assignment Description
Product Manual 2. Functional Specification 2.4 PIN Assignment Description Master: Description Description Power Supply (terminal 30) + 8 V DC for sensor supply Ground (terminal 31) 0 - 5 V DC Input CAN1 _High Illumination (terminal 58 (d)) CAN1 _Low Ignition (terminal 15) CAN2 _High Frequency Input 2 (0-2 kHz)
Page 20 Product Manual 2. Functional Specification Ω Range: 0.5 - 300 Ω Standard sensors: Pressure sensor(10 - 184 Sensor has to be connected between theese pins. PIN 11, 25: Analog Input 3 Ω Range: 10 - 700 Ω Standard sensors: Temperature sensor (38 - 700 Sensor has to be connected between theese pins.
Page 21 Product Manual 2. Functional Specification by configuration. An adjustable frequency divider reduces input frequency, so that it can be processed by the Microprocessor. 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...
Page 22: Display Functions
Product Manual 2. Functional Specification 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.
Page 23 Product Manual 2. Functional Specification Dot Matrix Layout One centre Line or optional two Alphanumeric Lines Graphic Four Alphanumeric with 6digits (12*16dots) each Symbol Area Lines with 5 digits each 6 * 8 12 * 16 72 dots 30 dots 30 dots 24 * 24 The display is structured into three main areas:...
Page 24 Product Manual 2. Functional Specification 2.5.3 Display Functions 2.5.3.1Main 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.
Page 25: Can Dtc Display
Product Manual 2. Functional Specification CAN DTC Display 2.5.3.3CAN 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 6 Digit stored into a DTC receive buffer.
Page 26: Service Message
Product Manual 2. Functional Specification Service Message 2.5.3.5Service Message The Service Message indication is based on operating hours and odome- ter. Service Service Code The Graphic Symbol Area displays the "Service Symbol" in case a Service Symbol Message becomes due. The corresponding service code is shown on the centre line of the display centre.
Page 27: Alarm- And Warning Functions
Product Manual 2. Functional Specification 2.5.4 Alarm- and Warning Functions Configu ration Data From EEPR OM Inp ut Values O utputs Output 1 Engine Speed 16bit C AN C ockp it Plus Output 2 Road Speed Switch Output Fu nctions 16bit Display CAN Values...
Page 28: Alarm And Warning Trigger Conditions
Product Manual 2. Functional Specification 2.5.4.3Alarm and Warning Trigger Conditions T/°C Alarm on Alarm off Warning Warning off time/sec 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.
Page 29: Alarm And Warning State Diagram (Maximum Value Algorithm)
Product Manual 2. Functional Specification 2.5.4.5Alarm and Warning State Diagram (Maximum Value Algorithm) VALUE Value > WarnLevel Time delay Display Warning Warning Indication * Reminder: Warning list and WINgauge "Alarm Action" Value < WarnLevel - Hysteresis Value > WarnLevel Value > AlarmLevel Time delay Display Alarm...
Page 30 Product Manual 2. Functional Specification Alarm and Warning State Diagram (Minimum Value Algorithm) VALUE Value <= WarnLevel Time delay Display Warning Warning Indication * Reminder: Warning list and WINgauge "Alarm Action" Value < WarnLevel - Hysteresis Value <= WarnLevel Value <= AlarmLevel Time delay Display Alarm...
Page 31: Service
Product Manual 2. Functional Specification 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.
Page 32: Can (Sae J1939) Dtc (Diagnostic Trouble Codes) Messages
Product Manual 2. Functional Specification 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).
Page 33: Can Dtc Information Display Requirements
Product Manual 2. Functional Specification 2.5.6.2CAN 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.
Page 34 Product Manual 2. Functional Specification 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.
Page 35: Speedometer Master Gauge
Product Manual 2. Functional Specification 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 va- riable (Byte1 and Byte2).
Page 36 Product Manual 2. Functional Specification 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 micro- controller calculates the deflection angle of the speedometer based on this physical speed value and gauge output characteri- stic.
Page 37: Tachometer Master Gauge
Product Manual 2. Functional Specification 2.5.6.5Tachometer 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 confi- guration the source of the engine speed information has to be defined.
Page 38: Satellite Gauges
Product Manual 2. Functional Specification 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.
Page 39: Satellite Gauge Address
Product Manual 2. Functional Specification 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: Address Numbers of the Satellite gauges Speedo / Tacho 1 Pressure Engine Oil Pressure Brake 1 / Rudder / Primary air...
Page 40: A. Technical Data
Product Manual 2. Functional Specification 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 90% r.F.
Page 41: B. Applied Standards
Technical test specification for mechanical and electronic information systems in motor ve- VDON 2.1954.001 1997-12 hicles Specification: customer specific integrated circuit in cmos technology for control of vdo- VDON 2.1955.070 1997-12 stepper motors (SM2/ MW2000) VDON 2.1958.001 Company sign VDO...
Page 42: Tu00-0736-0000002
Product Manual 3. Installation Instructions Enclosures Installation instructions TU00-0736-5107120 0609 (Page 1-8) 0609 3 - 1 TU00-0736-0000002 Technische Änderungen vorbehalten Technical details subject to change...
Page 43 Montageanleitung I Installation Instructions www.vdo.com CANcockpit Neue Generation I New Generation 2009 VDO - eine Marke des Continental-Konzerns / VDO - A trademark of the Continental Corporation...
Page 44 Montageanleitung Installation Instructions Systemkomponenten Gerät Dichtring Schraubring System components Gauge Seal ring Clamp ring 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...
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: Anwendung / Application: für Kabelbaum Master (26polig) / for wiring harness master (26-pole) für Kabelbaum Master - Slave / for wiring harness master - satelitte für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte Pos.
Page 46 Montageanleitung Installation Instructions 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.
Page 47 Montageanleitung Installation Instructions für Kabelbaum Master (26polig) / for wiring harness master (26-pole) Ausstoßwerkzeug / Push out tool (Pos. 7) Beispiel / Example für Kabelbaum Master - Slave / for wiring harness master - satelitte für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte Mit den Kontakten (Pos.
Page 48 Montageanleitung Installation Instructions für Kabelbaum Master - Slave / for wiring harness master - satelitte für Kabelbaum Slave - Slave / for wiring harness satelitte - satelitte Die Kabel (Pos. 15, 16, 17) je nach Belegung in den 4poligen schwarz gelb (Pos.
Page 49 Montageanleitung Installation Instructions Slave-Gerät Satellite gauge Ø 52 mm 54 mm 0,5 mm bis/to 8 mm Master-Gerät Master gauge Ø 80 mm 70,2 mm 0,5 mm bis/to 8 mm Kabelbaum Slave - Slave Wiring harness satelitte - satelitte rot schwarz gelb red black yellow Kabelbaum Master - Slave Wiring harness master - satelitte...
Page 50 Montageanleitung Installation Instructions Beispiel / Example TU00-0736-5107120 0609 (1-8) - 7 Technische Änderungen vorbehalten Technical details subject to change...
Page 51 Montageanleitung Installation Instructions Beispiel / Example Kabelbaum Master Wiring harness master Kabel-Belegung Geräteanschluss cable allocation Gauge connection Beschreibung / Description Beschreibung / Description Kl. 30 / Power Supply (terminal 30) + 8 V DC für Geber / for Sensor supply Kl.
Page 52 Product Manual 5. Software Description Enclosures W inGauge Software 0303 (Page 1-53) 0609 1 - 1 TU00-0736-0000002 Technische Änderungen vorbehalten Technical details subject to change...
Page 53 page 1 June 2009 Training WinGauge Software...
Page 54 Components and Concept page 2 June 2009 Training WinGauge Software...
Page 55 Example of a fully configured Instrumentation page 3 June 2009 Training WinGauge Software...
Page 56 Example of a fully configured Instrumentation cont. page 4 June 2009 Training WinGauge Software...
Page 57 Basic Steps to build a new Configuration: Definition of Project Properties Adding a Master Instrument Adding the required Slaves or Displays Configuration of Master, Slave- and Display Instruments. Save Configuration Test / Diagnose the new Configuration. page 5 June 2009 Training WinGauge Software...
Page 58 Definition of Project Properties 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.
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. After confirmation with „OK“ a picture of the selected Master is shown in the overview dialog "Configuration-Window"...
Page 60 TACHO and SPEEDO Instruments can be chosen from a broad variety of instruments. page 8 June 2009 Training WinGauge Software...
Page 61 The left screen part, The right part of the overview screen, the "Configuration-Window " is used "Navigation-Window" to show a picture of the selected Master, Slave or Display devices in addition shows the Configuration. with the characteristic parameter values e.g. Part No., Type, Primary- and Subcategories show up Secondary Range, potential Sensor type and Address, after a mouse-click to...
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. After confirmation with "OK" a picture image of the selected Satellite is shown in the overview dialog "Configuration-Window"...
Page 63 This shows the Selection of possible Satellites for the System like: Pressure, Temperature, Level, Voltage, Current, Speedometer, Tachometer and Various. page 11 June 2009 Training WinGauge Software...
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. page 12 June 2009 Training WinGauge Software...
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 page 13 June 2009 Training WinGauge Software...
Page 66 page 14 June 2009 Training WinGauge Software...
Page 67 page 15 June 2009 Training WinGauge Software...
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. After confirmation with "OK" a symbol representing the selected Display is shown in the overview dialog "Configuration-Window"...
Page 69 This shows the Selection of possible Displays for the System like: Pressure, Temperature, Level, Voltage, Current, Speedometer, Tachometer and Various. page 17 June 2009 Training WinGauge Software...
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.
Page 71 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 In the "Navigation- pull the non visible part up.
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. page 20 June 2009 Training WinGauge Software...
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". page 21 June 2009 Training WinGauge Software...
Page 74 This dialog is closed by This information is already selection of another device known from the „Add Display“ Master, Satellite or Display in configuration. the "Navigation-Window" 1. Step: Overwrite the name from „General“ to „Fuel Temperature“ 2. Step: Select the requested Trailing digits for the particular device.
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.
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 Configuration 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.
Page 77 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.
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.
Page 79 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 The new created logo plus all the new defined Symbols are added define the position for the Symbols in the sequentially to the Symbol table.
Page 80 Examples of new defined Symbols. page 28 June 2009 Training WinGauge Software...
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.
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.
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 •...
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. All Satellites, Master or Display being upsetted in the previous configuration process have in their configuration "CAN1"...
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.
Page 86 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.
Page 87 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. page 35 June 2009 Training WinGauge Software...
Page 88 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.
Page 89 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.
Page 90 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...
Page 91 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.
Page 92 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".
Page 93 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.
Page 94 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.
Page 95 Activation of configured Activation of Master switch Satellites warning lamps check output check at "Ignition at "Ignition on". No function on". No function indicates indicates a possible external a possible external wiring wiring fault! fault! page 43 June 2009 Training WinGauge Software...
Page 96 "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.
Page 97 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.
Page 98 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).
Page 99 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.
Page 100 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.
Page 101 Configuration of DTC Messages Five independent DTC Channels can be configured. Every Channel can receive DTCs from one CAN Device (Source Address). E.g. ECU = 0; TCU = 3 etc. If DTCs are received from any of the configured CAN Channels, they will be stored into a DTC Ring Buffer.
Page 102 After Saving, the Configuration may now be transferred to the connected physical units and executed there by The Configuration now can use of the function: be Saved by the use of : "Project - Write Master settings" "File – Save as" or "File –...
Page 103 The next two functions serve the EEPROM side of the Master device. They can be used to read out the EEPROM and save it to disc, or to load a new/modified EEPROM configuration into the Master device: "Project - Hardcopy - Read Master settings" "Project - Hardcopy - Write Master settings"...
Page 104 Two more Functions: • Diagnostics and • Recorder can be found below the function "Edit". A description is available in the following pages. page 52 June 2009 Training WinGauge Software...
Page 105 CAN shows the data content of 15 x The Diagnostics function covers Inputs means to show all physical 8 Bytes on the CAN-BUS. Those four important areas: values generated by the connected represent the information coming - Inputs Instruments configuration analogous from the different CAN Objects.
Page 106 The dialog "Warn Lamps/Illumination" allows to Pointer position can be used to check out the diagnose the Warn Lamps and the Illumination of a functioning of the individual Pointer Instruments. connected Set of Instruments. After selection of the Instrument to be tested in the •...
Page 107 The function "Recorder" allows to log and track all status- and changing Signals of all the connected Sensors. Adjustable is the range of the Y-Axis by just overwrite the min./max. values. Master-/Slave- and the different display curves are color coded for better recognition. On the right side, next to the legend, the measured values are shown together with the units they are measured in.
Page 108 Product Information www.vdo.com CANcockpit CANopen-Specification for VDO – A trademark of the Continental Corporation...
Page 109 CANopen-Specification for CANcockpit Product Manual CANcockpit Contents 5.2.1 Summary of Features 5.2.2 Expressions 5.2.3 Hardware Requirements CANopen Baud Rates and Sample Points for CANcockpit Galvanic isolation 11bit Identifiers 5.2.4 Firmware Requirements CAN Interfaces Master or Slave? Operational States Initialisation Boot-Up Message Pre-Operational Heartbeat Lifeguarding...
Page 110 CANopen-Specification for CANcockpit Product Manual CANcockpit 5.2.1 Summary of Features NMT: Slave Error Control: Heartbeat Node ID: Configurable in EEPROM with WINgauge No. of PDOs: 7 x RPDOs and 3 x TPDOs PDO modes: Manufacturer specific time-triggered with one configurable interval for each TPDO with WINgauge.
Page 111: Hardware Requirements
CANopen-Specification for CANcockpit Product Manual CANcockpit 5.2.3 Hardware Requirements CANopen Baud Rates and Sample Points for CANcockpit Standard CAN Bus Baud Rates on the CDVV controller at 10MHz crystal frequency Standard Baudrate Time Nominal Bit Sample Comment Baud Rate Prescaler Quantum Time Time...
Page 112 CANopen-Specification for CANcockpit Product Manual CANcockpit Operational States Initialisation The initialisation starts after ignition (Kl15) is turned on for the CANcockpit Gauge. Here the gauge application-programme and CAN hardware is initialised and then it transits to the Pre-Operational state automatically. Boot-Up Message The Boot-Up Message is transmitted, when CANcockpit performs the transition from "Initialising"...
Page 113: Error Handling
CANopen-Specification for CANcockpit Product Manual CANcockpit Error handling Emergency messages shall be triggered by internal errors in the device and they are assigned the highest possible priority to ensure that they get access to the bus without latency. The Emergency messages shall contain the error field with pre-defined error numbers and additional information.
Page 114 CANopen-Specification for CANcockpit Product Manual CANcockpit Minimum Capabilities To enable devices, which do not support the complete DBT- (Distributor) and NMT (Network Management) Slave functionality, to co-operate with full capability devices, the following minimal capabilities are required:  M odule-ID, ...
Page 115 CANopen-Specification for CANcockpit Product Manual CANcockpit Device Profile Standard "Human Machine Interface" or Custom device profile? Based on Device Profile for Generic I/O Modules DS 401 V2.1. Reason: The Human Machine Interface profile DSP-403 has been withdrawn by CiA. Another alternative would have been to use DSP-407 "Application profile for Passenger Information", but this Draft Proposal is marked "not recommended for implementation"...
Page 116 CANopen-Specification for CANcockpit Product Manual CANcockpit Pre-Defined Connection Set In order to reduce configuration effort for simple networks a mandatory default identifier allocation scheme is defined. These identifiers are available in the PRE-OPERATIONAL state directly after initialization (if no modifications have been stored). The default profile ID-allocation scheme consists of a functional part, which determines the object priority and a Node-ID-part, which allows distinguishing between devices of the same functionality.
Page 117 CANopen-Specification for CANcockpit Product Manual CANcockpit Object Dictionary Administrative Messages (Layer Management, Network Management and Identifier Distribution Messages) By means of Administrative Messages the setting up of layer specific parameters (Layer Management services), the initialisation, configuration and supervision of the network is performed. Services and protocols of these functions are according to the LMT (Layer Management), NMT (Network Management) and DBT (Distributor) service entities of the CAL specification.
Page 118 CANopen-Specification for CANcockpit Product Manual CANcockpit Triggering Modes The CANopen Communication Profile distinguishes two message-triggering modes: Event Driven Message transmission is triggered by the occurrence of an object specific event. In case of the CANcockpit the event triggering is time-based. Remotely requested The transmission of asynchronous PDOs may be initiated on receipt of a remote request initiated by another device.
Page 119 CANopen-Specification for CANcockpit Product Manual CANcockpit Manufacturer Firmware Version (100Ah) Contains the manufacturer firmware version description. For CANcockpit this is the firmware date, because this is relevant for the configuration with WINgauge and is required to be checked before a new EEPROM configuration may be written into the EEPROM via CANopen.
Page 120 The minor revision number identifies different versions with the same CANopen behavior. The administration of the minor revision number is the responsibility of the party, who administers the configuration data for a given application (VDO or OEM).
Page 121 CANopen-Specification for CANcockpit Product Manual CANcockpit ENTRY DESCRIPTION Sub-Index Description Number of entries Entry Category Mandatory Access PDO Mapping Value Default Value Sub-Index Description Vendor ID Entry Category Mandatory Access PDO Mapping Value Range UNSIGNED32 (Actual value 0x09000053) Default Value Sub-Index Description Product code...
Page 122 CANopen-Specification for CANcockpit Product Manual CANcockpit ENTRY DESCRIPTION Sub-Index Description Largest sub-index supported Entry Category Mandatory Access PDO Mapping Value Default Value Sub-Index Description COB-ID used by PDO Entry Category Mandatory Access PDO Mapping Value UNSIGNED32 The actual COB-ID is configurable with WINgauge for each of the 7 RPDOs.
Page 123 CANopen-Specification for CANcockpit Product Manual CANcockpit ENTRY DESCRIPTION 1st RPDO: 8x8 Digital outputs: Index Sub-Index Comment Value/ hex 1600h Number of mapped objects Write Digital Output 1 to 8 6200 01 08 Write Digital Output 9 to 16 6200 02 08 Write Digital Output 17 to 24 6200 03 08 Write Digital Output 25 to 32...
Page 124 CANopen-Specification for CANcockpit Product Manual CANcockpit Transmit PDO communication parameters (1800h to 1802h) Contains the communication parameters for the PDOs the device is able to transmit. The parameters are read only. OBJECT DESCRIPTION Index 1800h to 1802h Name Transmit PDO parameter Object Code RECORD Data Type...
Page 125 CANopen-Specification for CANcockpit Product Manual CANcockpit 2nd TPDO: 4 Analogue Inputs Index Sub-Index Comment Value/ hex 1A01h Number of mapped objects Read Analogue Input 1 6401 01 10 Read Analogue Input 2 6401 02 10 Read Analogue Input 3 6401 03 10 Read Analogue Input 4 6401 04 10 3rd TPDO: 4 Analogue Inputs...
Page 126 CANopen-Specification for CANcockpit Product Manual CANcockpit MSB = Byte3 F: Format Bit 1-> 4lines x 16character (only Alarm or Warning) 0 -> 2lines x 8character (Alarm and/ or Warning) R: Reserved Bit, set to 0. Alarm Bit 1-> Alarm Display is activated (if configured) 0 ->...
Page 127 CANopen-Specification for CANcockpit Product Manual CANcockpit ENTRY DESCRIPTION Access PDO Mapping Value Range 20h to 7Fh " Default Value " Write Alarm or (but not and) Warning Display 4x16 (2003h) This visible string object provides the text to be displayed on the CANopen Alarm or Warning Display (only one of the two). It has a length of 64bytes.
Page 128 CANopen-Specification for CANcockpit Product Manual CANcockpit Read and Write an EEPROM Data Record from and to EEPROM access buffer (2005h). This object is required to transfer data records to and from CANcockpit via the CANopen interface. The data is contained in Data Records as specified below.
Page 129 CANopen-Specification for CANcockpit Product Manual CANcockpit Write EEPROM Data Record to EEPROM Writing a data record to EEPROM involves the following steps: 1. Check object 2006h and if the EEPROM is not busy, write one Record as specified above into this object of CANcockpit. 2.
Page 130 CANopen-Specification for CANcockpit Product Manual CANcockpit Standardised Device Profile Area Read 64 digital Inputs byte wise (6000h) This object shall read groups of 8 input lines as 8-bit information. Up to eight 8-Bit inputs are addressable in CANcockpit. The CANcockpit main gauge has no hardware digital inputs. However it is possible to select internal variables via configuration, for example the status of the 16 SAT- and 16 external warning lamps, plus the switch outputs as digital input signals to be transmitted to the CANopen bus.
Page 131 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Read Input 33 to 40 Access Entry Category Mandatory PDO Mapping Default Value Range Unsigned8 Default Value Sub-Index Description Read Input 41 to 48 Access Entry Category Mandatory PDO Mapping Default Value Range Unsigned8 Default Value Sub-Index...
Page 132 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Polarity Input 9 to 16 Access Entry Category Mandatory PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description Polarity Input 17 to 24 Access Entry Category Mandatory PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description...
Page 133 CANopen-Specification for CANcockpit Product Manual CANcockpit Write 64 digital Outputs byte wise (6200h) Values written via SDO will overwrite PDO values and vice versa. Digital outputs of the CANopen network are actually digital inputs for CANcockpit. The result of the polarity processing (object 6202h) and timeout control (object 6206h and object 6207h) is available in the result array "Copen_abDO[8]".
Page 134 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Write Output 33 to 40 Access Entry Category Optional PDO Mapping Default Value Range Unsigned8 Default Value Sub-Index Description Write Output 41 to 48 Access Entry Category Optional PDO Mapping Default Value Range Unsigned8 Default Value Sub-Index...
Page 135 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Polarity Output 9 to 16 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description Polarity Output 17 to 24 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description...
Page 136 CANopen-Specification for CANcockpit Product Manual CANcockpit Error Mode Output 8-Bit (6206h) This object indicates, whether an output is set to a pre-defined error value (see 6207 object) in case of a message time out. 1 = output value shall take the pre-defined condition specified in 6207 object 0 = output value shall be kept if an error occurs Actual values can be configured with WINgauge (EEPROM parameters).
Page 137 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Error Mode Output 41 to 48 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description Error Mode Output 49 to 56 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index...
Page 138 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Error Value Output 17 to 24 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index Description Error Value Output 25 to 32 Access Entry Category Optional PDO Mapping Value Range Unsigned8 Default Value Sub-Index...
Page 139 CANopen-Specification for CANcockpit Product Manual CANcockpit ENTRY DESCRIPTION Sub-Index Description Number of Analogue Inputs 16-Bit Access Entry Category Mandatory PDO Mapping Value Default Value Sub-Index Description Analogue Input 1 Access Entry Category Mandatory PDO Mapping Default Value Range Integer16 Default Value Sub-Index Description Analogue Input 2...
Page 140 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Analogue Input 8 Access Entry Category Optional PDO Mapping Default Value Range Integer16 Default Value Write analogue Outputs word wise (6411h) This object shall write an Integer16 value to the output channel 'n'. The value shall be always left adjusted. Here the variables represent physical values (process values), before the output characteristic of the gauges or the conversion for a PVD.
Page 141 CANopen-Specification for CANcockpit Product Manual CANcockpit Sub-Index Description Analogue Output 4 Access Entry Category Optional PDO Mapping Default Value Range Integer16 Default Value Sub-Index Description Analogue Output 5 Access Entry Category Optional PDO Mapping Default Value Range Integer16 Default Value Sub-Index Description Analogue Output 6...
Page 142 CANopen-Specification for CANcockpit Product Manual CANcockpit 5.2.5 Appendix Literature 1 CANopen, Holger Zeltwanger, 2001 VDE Verlag GmbH, Berlin, ISBN 3-8007-2448-0 2 Embedded Networking with CAN and CANopen, Olaf Pfeiffer, Andrew Ayre and Christian Keydel, 2003 RTC Books, San Clemente CA USA, ISBN 0-929392-78-7 References [1] CiA DS301: CANopen Application Layer and Communication Profile, Version 4.02.
Page 143 Product Manual System Components, Spare Parts and Accessories Contents Contents System Components 6.1.1 Master Gauges 6.1.2 Satelitte Gauges 6.1.3 Master Black Box 6.1.4 Articel description Spare Parts and Accessories 6.2.1 Spare Parts Clamp rings 6.2.2 Accessories Wiring harnesses Parts for own installation of the wiring harnesses Software Accessories 0609 6 - 1...
Page 144 Product Manual System Components, Spare Parts and Accessories 6.1 System Components 6.1.1Master Gauges Example: Tachometer Housing dia. 80 mm Master gauge Sealing ring Clamp ring Partnumber Description Master 80 mm A2C60000020 CCM 80 Tacho 0-3*1000/min S tb A2C60000021 CCM 80 Tacho 0-4*1000/min S tb A2C60000022 CCM 80 Speedo 0-60km/h S tb A2C60000023...
Page 145 Product Manual System Components, Spare Parts and Accessories 6.1 System Components 6.1.2Satelitte Gauges Example: Pressure gauge Housing dia. 52 mm Satelitte gauge Sealing ring Clamp ring Partnumber Description Slave 52 mm A2C60000251 CCS 52 PressOil 0-5bar S tb A2C60000252 CCS 52 PressOil 0-10bar S tb A2C60000253 CCS 52 PressOil 0-500kPa S tb A2C60000254...
Page 146 Product Manual System Components, Spare Parts and Accessories 6.1 System Components 6.1.2Satelitte Gauges Partnumber Description Slave 52 mm A2C60000278 CCS 52 LevelFuel 0-1 S tb A2C60000279 CCS 52 LevelFuel E-F S tb A2C60000280 CCS 52 LevelFw 0-1 S tb A2C60000281 CCS 52 LevelWw 0-1 S tb A2C60000282 CCS 52 Volt 8-16V S tb...
Page 147 Product Manual System Components, Spare Parts and Accessories 6.1 System Components 6.1.4Articel description 0609 0609 6 - 5 6 - 5 TU00-0736-0000002 TU00-0736-0000002 Technische Änderungen vorbehalten Technische Änderungen vorbehalten Technical details subject to change Technical details subject to change...
Page 148 Product Manual System Components, Spare Parts and Accessories 6.2 Spare Parts and Accessories 6.2.1Spare Parts Clamp rings for gauges dia. 52 mm / dia. 80 mm Pos. Designation Items / Package Order No. Clamp ring dia. 52 mm 800-005-015G Clamp ring dia. 80 mm 800-005-005G 0609 6 - 6...
Page 149 Product Manual System Components, Spare Parts and Accessories 6.2 Spare Parts and Accessories 6.2.2Accessories Wiring harnesses Pos. Designation Items / Package Order No. Wiring harness master (26-pole), 3000 mm long A2C53041729 Wiring harness master-satelitte, 200 mm long A2C53344035 Wiring harness satelitte-satelitte, 200 mm long A2C53344036 0609 6 - 7...
Page 150 Product Manual System Components, Spare Parts and Accessories 6.2 Spare Parts and Accessories 6.2.2Accessories Parts for own installation of the wiring harnesses Pos. Designation Items / Package Order No. Hand tool AMPMODU (AMP-Nr. 0-0169481-1) — — Housing AMPMODU X11-602-000-002 Draw-off bracket AMPMODU X11-602-000-005 Contact seal...
Page 151 Product Manual System Components, Spare Parts and Accessories 6.2 Spare Parts and Accessories 6.2.2Accessories Software Accessories Pos. Designation Items / Package Order No. CANcockpit Interface (Wingauge CMD Line) X11-602-000-009 CANcockpit Interface (Wingauge) X11-602-000-010 CANcockpit Demo Case X10-110-397-006 Demo Case 0609 6 - 9 TU00-0736-0000002 Technische Änderungen vorbehalten...
Page 152 Datenblätter I Data Sheets www.vdo.com CANcockpit Neue Generation I New Generation 2009 VDO - eine Marke des Continental-Konzerns / VDO - A trademark of the Continental Corporation...
Page 153 Datenblätter I Data Sheets Produkt Doku-Nr. Seiten Product Documentation No. Pages Master-Geräte CANcockpit TU00-0736-5104620 0509 1 - 4 Master Gauges Slave-Geräte CANcockpit TU00-0736-5304620 0509 1 - 4 Satelitte Gauges Master Black Box TU00-0736-5404620 0509 1 - 3 TU00-0736-7004620 0509 (1-2) 2 Technische Änderungen vorbehalten Technical details subject to change...
Page 154 Master-Geräte Master Gauges Systemkomponenten System Components Tachometer oder Drehzahlmesser Speedometer or Tachometer (Gehäuse Ø 80 / 85 / 100 mm) (Housing dia. 80 / 85 / 100 mm) Beispiel: Gehäuse Ø 80 mm Example: housing dia. 80 mm Drehzahlmesser / Tachometer Tachometer / Speedometer Beschreibung: Description:...
Page 155 Master-Geräte Master Gauges Systemkomponenten System Components Tachometer oder Drehzahlmesser Speedometer or Tachometer (Gehäuse Ø 80 / 85 / 100 mm) (Housing dia. 80 / 85 / 100 mm) Beispiel: Gehäuse Ø 80 mm Example: housing dia. 80 mm Master-Gerät Dichtungsring Schraubring Master gauge Sealing ring...
Page 156 Master-Geräte Master Gauges Systemkomponenten System Components Tachometer oder Drehzahlmesser Speedometer or Tachometer (Gehäuse Ø 80 / 85 / 100 mm) (Housing dia. 80 / 85 / 100 mm) Technische Daten: Technical Data: Nennspannung: 12V und 24V DC Rated voltage: 12V and 24V DC Betriebsspannung: 10,5V bis 32V DC Operating voltage:...
Page 157 Master-Geräte Master Gauges Systemkomponenten System Components Tachometer oder Drehzahlmesser Speedometer or Tachometer (Gehäuse Ø 80 / 85 / 100 mm) (Housing dia. 80 / 85 / 100 mm) Beispiel: Gehäuse Ø 80 mm Exemple: housing dia. 80 mm Abmaße (mm) Dimensions (mm) 11,4 Ø...
Page 158 Slave-Geräte Satellite Gauges Systemkomponenten System Components Analoge Anzeigegeräte Various versions of in verschiedenen Versionen analog indication gauges (Gehäuse Ø 52 / 80 / 100 mm) (Housing dia. 52 / 80 / 100 mm) Beispiel / Examples: Druckanzeiger / Pressure gauge Temperaturanzeiger / Vorratsanzeiger / Fuel level gauge Temperature gauge...
Page 159 Slave-Geräte Satellite Gauges Systemkomponenten System Components Analoge Anzeigegeräte Various versions of in verschiedenen Versionen analog indication gauges (Gehäuse Ø 52 / 80 / 100 mm) (Housing dia. 52 / 80 / 100 mm) Beispiel: Gehäuse Ø 52 mm Example: housing dia. 52 mm Slave-Gerät Dichtungsring Schraubring...
Page 160 Slave-Geräte Satellite Gauges Systemkomponenten System Components Analoge Anzeigegeräte Various versions of in verschiedenen Versionen analog indication gauges (Gehäuse Ø 52 / 80 / 100 mm) (Housing dia. 52 / 80 / 100 mm) Technische Daten: Technical Data: Versorgungsspannung: 10,5 - 32V DC von Master Power supply: 10.5 - 32V DC from Master Stromaufnahme:...
Page 161 Slave-Geräte Satellite Gauges Systemkomponenten System Components Analoge Anzeigegeräte Various versions of in verschiedenen Versionen analog indication gauges Gehäuse Ø 52 mm Housing dia. 52 mm Partnumber Description Slave 52 mm A2C60000251 CCS 52 PressOil 0-5bar S tb A2C60000252 CCS 52 PressOil 0-10bar S tb A2C60000253 CCS 52 PressOil 0-500kPa S tb A2C60000254...
Page 162 Master Black Box Master Black Box Systemkomponenten System Components Gehäuse 100 x 100 x 41,3 mm Housing 100 x 100 x 41,3 mm Beschreibung: Description: Empfang und Verarbeitung sowohl von CANbus-Daten (SAE Reception and processing of both CANbus-data (SAE J1939 J1939 / CANopen) als auch von analogen Signalen zur / CANopen) and analog signals for indication on slave Anzeige in Slave Instrumenten über SATbus.
Page 163 Master Black Box Master Black Box Systemkomponenten System Components Gehäuse 100 x 100 x 41,3 mm Housing 100 x 100 x 41,3 mm Ausführung: Design: Gehäuse: Kunststoff, flammhemmend Housing: plastic, flame retardant Befestigung: 4 Schrauben Mounting: 4 screws Anschlussart: AMP 26 Pins MODU II, Type of connection: AMP 26 pins MODU II, MATE-N-LOK 4 Pins MATE-N-LOK 4 pins...
Page 164 Master Black Box Master Black Box Systemkomponenten System Components Gehäuse 100 x 100 x 41,3 mm Housing 100 x 100 x 41,3 mm Technische Daten: Technical Data: Nennspannung: 12V und 24V DC Rated voltage: 12V and 24V DC Betriebsspannung: 10,5V bis 32V DC Operating voltage: 10,5V to 32V DC Stromaufnahme:...
Page 165 CANcockpit article description CCS 52 PressOil 0-5bar S on tb ABCDE 1 Device type 2 Diameter 5 Main scale CANcockpit BlackBox - CCB 52 mm - 52 min. "-" max. unit CANcockpit Master - CCM 80 mm - 80 6 Dial scale CANcockpit Slave - CCS 85 mm...
Page 166 MONTAGEANLEITUNG / INSTALLATION INSTRUCTIONS X12-397-041-601, X12-397-041-001, X12-397-046-001, 03/09 K-line Adapter TU00-0777-5107120 X11-602-000-009, X11-602-000-010 K-line Adapter Gelb / yellow = Diagnoseleitung / Diagnosis line Rot + grün / red + green = + 12-24V Blau + schwarz / blue + black = Masse / Ground 9 pol.
Page 169 VCA Headquarters 1 The Eastgate Office Centre Eastgate Road Bristol, BS5 6XX United Kingdom Switchboard: +44 (0) 117 951 5151 Main Fax: +44 (0) 117 952 4103 Email: enquiries@vca.gov.uk Web: www.vca.gov.uk THE UNITED KINGDOM VEHICLE APPROVAL AUTHORITY COMMUNICATION CONCERNING THE APPLICATION OF THE COUNCIL DIRECTIVE OF 20 JUNE 1972 ON THE APPROXIMATION OF THE LAWS OF THE MEMBER STATES RELATING TO A TYPE OF COMPONENT WITH REGARD TO RADIO INTERFERENCE SUPPRESSION (72/245/EEC) AS LAST AMENDED BY 2006/28/EC .
Page 170 e11*72/245*2006/28*4935*00 SECTION II Additional information (where applicable): Not applicable Technical service responsible for carrying out the tests: Vehicle Certification Agency Date of test report: 7 June 2009 Number of test report: OSJ194266 (4935) Remarks (if any): None Place: BRISTOL Date: 8 JUNE 2009 Signature: M.
Page 171 VCA Headquarters 1 The Eastgate Office Centre Eastgate Road Bristol, BS5 6XX United Kingdom Switchboard: +44 (0) 117 951 5151 Main Fax: +44 (0) 117 952 4103 Email: enquiries@vca.gov.uk Web: www.vca.gov.uk THE UNITED KINGDOM VEHICLE APPROVAL AUTHORITY COMMUNICATION CONCERNING THE APPLICATION OF THE COUNCIL DIRECTIVE OF 20 JUNE 1972 ON THE APPROXIMATION OF THE LAWS OF THE MEMBER STATES RELATING TO A TYPE OF COMPONENT WITH REGARD TO RADIO INTERFERENCE SUPPRESSION (72/245/EEC) AS LAST AMENDED BY 2006/28/EC .
Page 172 e11*72/245*2006/28*4936*00 SECTION II Additional information (where applicable): Not applicable Technical service responsible for carrying out the tests: Vehicle Certification Agency Date of test report: 7 June 2009 Number of test report: OSJ194266 (4936) Remarks (if any): None Place: BRISTOL Date: 8 JUNE 2009 Signature: M.
Page 173 VCA Headquarters 1 The Eastgate Office Centre Eastgate Road Bristol, BS5 6XX United Kingdom Switchboard: +44 (0) 117 951 5151 Main Fax: +44 (0) 117 952 4103 Email: enquiries@vca.gov.uk Web: www.vca.gov.uk THE UNITED KINGDOM VEHICLE APPROVAL AUTHORITY COMMUNICATION CONCERNING THE APPLICATION OF THE COUNCIL DIRECTIVE OF 20 JUNE 1972 ON THE APPROXIMATION OF THE LAWS OF THE MEMBER STATES RELATING TO A TYPE OF COMPONENT WITH REGARD TO RADIO INTERFERENCE SUPPRESSION (72/245/EEC) AS LAST AMENDED BY 2006/28/EC .
Page 174 e11*72/245*2006/28*4937*00 SECTION II Additional information (where applicable): Not applicable Technical service responsible for carrying out the tests: Vehicle Certification Agency Date of test report: 7 June 2009 Number of test report: OSJ194266 (4937) Remarks (if any): None Place: BRISTOL Date: 8 JUNE 2009 Signature: M.

VDO CANcockpit Series Product Manual

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