Kanardia miniDaqu Manual

Kanardia miniDaqu Manual

Engine management system
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miniDaqu
Engine Management System
Manual
©
Kanardia d.o.o.
July 2020
Revision 1.2

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Summary of Contents for Kanardia miniDaqu

  • Page 1 Engine Management System Manual © Kanardia d.o.o. July 2020 Revision 1.2...
  • Page 3 In short, the license gives you right to copy, reproduce and modify this document if: ˆ you cite Kanardia d.o.o. as the author of the original work, ˆ you distribute the resulting work only under the same or similar license to this one.
  • Page 4 — Manual Revision History The following table shows the revision history of this document. Rev. Date Description January 2019 Initial release. March 2019 Unified DB9 markings. July 2020 Digital PNP sensor schema fix. © Kanardia 2019-2020...
  • Page 5: Table Of Contents

    2.2 Connectors and Cables ..... . . 10 2.2.1 Kanardia CAN Bus Connector ....11 2.2.2 ECU Connector .
  • Page 6 CONTENTS miniDaqu — Manual 5 RPM Signal 5.1 Connection ......22 5.2 Configuration ......22 6 Rotax iS 6.1 ECU CAN Bus Connection .
  • Page 7 — Manual CONTENTS 9.4 Current ....... 37 9.4.1 Installation ......37 9.4.2...
  • Page 8: Introduction

    CAN network, where other units can make use of these readings. In addtition, mini Daqu connects to engine ECU and reads data from it. The data is then transmitted on the Kanardia CAN network. We strongly recommend you to carefully read this manual, before you start connecting mini Daqu unit with your engine sensors.
  • Page 9: Technical Specifications

    — Manual 1.2 Technical Specifications uses information available from ECU and only minimal amount of additional sensors (if any) is required. Daqu electronics is enclosed in thin anodized aluminum case. Electronics is designed to sustain elevated ambient temperatures and with some care it can also be mounted in an engine compartment.
  • Page 10: Channels

    1.3 Channels miniDaqu — Manual Clearance for two CAN connectors and sensor wires Figure 1: Dimensions and connection clearence of mini Daqu – Top View. Figure 2: Dimensions and connection clearence of mini Daqu – Front View. Channels Daqu has digital type and analog type channels where each type has several versions.
  • Page 11: Digital Channels

    — Manual 1.3 Channels C – analog channel with 0 to +30 V input, used to read higher voltage levels. Only one such channel is available and is used to measure the system voltage. E – analog channels with 0 to +5 V input. They are mostly used to read active sensors.
  • Page 12: Installation

    Power, CAN and ECU connector details are presented in this section. Sensor connectors are described in a separate chapter. Mini Daqu has two D-SUB 9 connectors as shown on figure 3. The left connector is used to connect mini Daqu to Kanardia CAN bus, which also © Kanardia 2019-2020...
  • Page 13: Kanardia Can Bus Connector

    View from soldering side Figure 3: Details of the mini Daqu connectors. The left is used for Kanardia CAN bus and the right connects to an engine ECU. The 12 pin connector on top is used to connect additional sensors and probes.
  • Page 14: Ecu Connector

    2.2 Connectors and Cables miniDaqu — Manual +12V high Figure 4: Details of the RJ45 connector. Pins 5 and 9 on the D-SUB 9 can be used to send the RPM signal out, for some other instrument (e.g. propeller pitch controller). The pins are not connected to the CAN cable.
  • Page 15: Wiring In General

    There are also other sensors that Daqu can make use of and are not described here. When you encounter a problem, contact Kanardia and we will try to provide you with a solution.
  • Page 16: Resistive Sensors

    3.3 Resistive Sensors miniDaqu — Manual block will not damage Daqu, but will create unnecessary ground loops, which in turn may cause incorrect readings from the engine sensors, especially resis- tive ones. Daqu ground pin should be used only when: 1.
  • Page 17: Analog Active Sensors

    — Manual 3.5 Analog Active Sensors Analog Active Sensors Active sensors require external power to operate and provide some active signal. Some sensors require 12 V and some 5 V to operate. These sensors are often used to measure various pressures and, fuel levels, etc. An active sensor has its own built-in electronics, which takes care for voltage fluctuations.
  • Page 18: Current Output

    3.5 Analog Active Sensors miniDaqu — Manual +5 V FUEL Signal 0-5V ROTOR +12 V Figure 6: An example of active sensor with voltage output. 3.5.2 Current Output Some active sensors have varying current. The current vary between 4 mA when sensor is unloaded and 20 mA when sensor is fully loaded.
  • Page 19: Potentiometers

    — Manual 3.6 Potentiometers Potentiometers Some resistive sensors are in fact potentiometers (fuel level, trim, etc.). They can be connected as variable resistors or as variable voltage dividers. 3.6.1 Variable Resistor Section 3.3 applies, when they are connected as variable resistors. Figure 8 shows and example of variable resistor connection.
  • Page 20: Digital Active Sensors

    3.7 Digital Active Sensors miniDaqu — Manual +5 V FUEL ROTOR +12 V Figure 9: An example of potentiometer, connected as variable voltage divider. Digital Active Sensors Digital active sensors require external power to operate. They produce a step like signal, which can be viewed at as pulses. Daqu measures time between these pulses.
  • Page 21: Pnp - Open Drain Output

    — Manual 4. Alarm Signal +5 V FUEL ROTOR +12 V Figure 10: An example of NPN digital sensor connection. 3.7.2 PNP – Open Drain Output Figure 11 illustrates a typical connection for the PNP case. Here, an addi- tional 10 kΩ...
  • Page 22: Direct Connection

    4.1 Direct Connection miniDaqu — Manual be then used to trigger some action (e.g. illuminate a warning light on the instrument panel). Alarm signal option can not be used in parallel with Automatic start power switch relay. The function of these pins must be specified in the configuration.
  • Page 23: Configuration

    — Manual 4.3 Configuration shows connection schematics. The relay signal lines must be protected by a flyback diode. Use a diode, which reverse voltage is rated higher than the system voltage. Wire Colour Function Black CAN A LOW CAN A HIGH...
  • Page 24: Rpm Signal

    Daqu reads the engine RPM value from ECU and creates digital pulses on the pins 5 and 9 of the Kanardia CAN bus connector. See Figure 3 and Table 2 . It creates one digital pulse per RPM. Third party instrument can connect to these pins and detect pulses in order to obtain RPMs.
  • Page 25: Rotax Is

    — Manual 6. Rotax iS Rotax iS This section gives some specific installation tips for the Rotax iS engines. Rotax has two iS models, 912 iS and 915 iS. Although the engines are different, the ECU and connection principles are the same for both engine types.
  • Page 26: Configuration

    6.2 Configuration miniDaqu — Manual Configuration Daqu must be correctly configured to read data from the ECU. When con- figuring Daqu correct Engine model must be selected. Select Rotax 912iS. Example of configuration dialog is ilustrated on Figure 18. Automatic Start Power Switch This topic is experimental.
  • Page 27: Configuration

    — Manual 6.3 Automatic Start Power Switch Backup Battery Rotax 912iS FuseBox Switch (S3) Start Power Start Power Relay Switch iS EMS GND iS EMS GND Airframe GND Airframe GND Relay Out - Relay Out + (Daqu) (Daqu) Figure 17: Automatic start power switch with a relay and connection from Daqu.
  • Page 28: Operation

    7. ULPower Engines miniDaqu — Manual start. In addition, the iS start switch RPM threshold must be set. The later defines engine RPMs, which must be reached to disconnect the relay. At the time of the writing only Nesis and Aetos support this option. Figure 18 illustrates settings for Rotax 912 iS engine.
  • Page 29 — Manual 7. ULPower Engines ULPower engines may also use an AUX box for reading various sensors not directly related to ECU. This AUX box is connected directly to one ECU or to both ECUs (when two ECUs are used). The ECU combines data from AUX box with its own data and outputs the combined data over CAN or RS-232.
  • Page 30: Ecu And Aux Parameters

    7.1 ECU and AUX Parameters miniDaqu — Manual TPS, MAT, OilP, OilT, FuelP Baro pressure ECU A miniDaqu AUXBOX Baro pressure ECU B TPS, MAT, OilP, OilT, FuelP Figure 21: Block view of dual ECU connection CAN bus. ECU and AUX Parameters...
  • Page 31: Two Ecus

    ECU RS-232 Connection The serial port interface can be connected to only one ECU. Daqu receives data stream from ECU, decodes data and send it over Kanardia CAN bus protocol. Please refer to Table 6, for connecting ULPower ECU to Daqu via serial protocol.
  • Page 32: Configuration

    7.4 Configuration miniDaqu — Manual Table 6: Connection table for serial bus. DB9-ECU Daqu Function Pin 2 RS232 RX RS232 TX Pin 3 RS232 TX RS232 RX (connection not required) Pin 1 Configuration When configuring Daqu, correct Engine model must be selected. An example of configuration dialog is ilustrated on Figure 22.
  • Page 33: Cc-M Module

    — Manual 8.1 CC-m Module This section gives some specific installation tips for the MWfly engines. MWfly engines are equipped with ECU that has a CAN output. However, Daqu can not be directly connected to this ECU and an interface is needed. This inter- face is called CC-m CAN to CAN module and it is provided by MWfly.
  • Page 34: Fuel Pressure

    9.1 Fuel Pressure miniDaqu — Manual Fuel Pressure In most cases, ECUs do not have fuel pressure information. In order to get it, a fuel pressure sensors must be connected to Daqu. Rotax iS is a bit special here and it is explained in a separate section 9.2.
  • Page 35: Variable Voltage

    — Manual 9.2 Fuel Pressure - Rotax iS 9.1.3 Variable Voltage Sensors with variable voltage output were described in section 3.5.1. Connec- tion example is given on Figure 6. It shows an active sensor with 0.5 – 4.5 V output.
  • Page 36: Configuration For Vented Gage Sensor

    9.2 Fuel Pressure - Rotax iS miniDaqu — Manual Option Selection/Setting Channel Any F Function Fuel pressure Sensor 4-20 mA Int Res Report time 0.5 – 1.0 s Filter 2.0 s Max value (at 20 mA) 10 (depends on sensor) Table 8: Typical fuel pressure configuration for sensors with current output.
  • Page 37: Configuration For Absolute Sensor

    — Manual 9.2 Fuel Pressure - Rotax iS Table 9: Rotax iS engine with vented gage fuel pressure sensor. Option Selection/Setting Channel Any E or F Function Fuel P. cmp. Sensor Active 0.5-4.5 V Report time 0.5 – 1.0 s Filter 2.0 s...
  • Page 38: Voltage

    9.3 Voltage miniDaqu — Manual Voltage Daqu can measure voltages from 0 to +30 V DC on the channel C. The system voltage is usually measured on this channel. Some engines, Rotax iS, for example, transmit their own system voltage, which is obtained from engine ECU.
  • Page 39: Current

    Table 11: Channel C configuration for system voltage. Current In order to measure electrical current a CT-30 sensor or a CT-60 sensor is required. These sensors are produced by Kanardia. Standard shunts are not supported. CT-30 measures current between -30 and +30 A and CT-60 measures current between -60 and +60 A.
  • Page 40: Configuration

    9.5 Fuel Level miniDaqu — Manual BLACK GND RED +5V +5 V WHITE FUEL ROTOR +12 V Figure 26: CT-30 sensor connection schematics. 9.4.2 Configuration The table 12 shows possible channel settings. Alternatively, El. current 2 can be also selected for the second current sensor.
  • Page 41: Configuration

    — Manual 9.5 Fuel Level In the case of resistive fuel level sensor, the sensor is connected according to principles described in section 3.3 and in the case of active (or capacitive) sensor with voltage output, the sensor is connected according to section 3.5.1.
  • Page 42: Trim, Flap And Other Position Sensors

    9.6 Trim, Flap And Other Position Sensors miniDaqu — Manual Please consult the display manual (Nesis/Aetos/Emsis/Digi/etc.) for details on the tank shape calibration procedure. Trim, Flap And Other Position Sensors Different position sensors/potentiometers can be connected to Daqu in order to provide control position information for one of the following functions: ˆ...
  • Page 43: Variable Voltage Divider

    — Manual 9.6 Trim, Flap And Other Position Sensors 9.6.2 Variable Voltage Divider Figure 9 shows typical schematics for the variable voltage divider. The cor- responding channel is configured something like shown by Table 16. Option Selection/Setting Channel Any E or F...
  • Page 44: Fuel Flow

    9.7 Fuel Flow miniDaqu — Manual Option Selection/Setting Channel Y only Function Rotor RPM Sensor Digital Pulse Report time 0.2 – 0.5 s Filter about 0.5 s Pulses Reduction Table 17: An example for rotor RPM connected to Y channel. Sensor is in rotor head, hence the reduction ratio is set to 1.0.
  • Page 45: Installation

    — Manual 9.7 Fuel Flow Daqu. Daqu expects number of pulses per liter. Almost all sensors are NPN type (FlosScan, FT-60). Connection schematics is given on figure 10. Refer to the sensor documentation for proper connection and operating voltage.
  • Page 46: Configuration

    Please read the following sections about the warranty and the limited opera- tion to get more information about the subject. 10.1 Warranty Kanardia d.o.o. warrants the Product manufactured by it against defects in material and workmanship for a period of twenty-four (24) months from retail © Kanardia 2019-2020...
  • Page 47 Warranty. Refer to the licensing agreement accompanying such software for details of your rights with respect to its use. This warranty does not apply: (a) to damage caused by use with non-Kanardia products; (b) to damage caused by accident, abuse, misuse, flood, fire, earth- quake or other external causes;...
  • Page 48 No Kanardia reseller, agent, or employee is authorized to make any modification, extension, or addition to this warranty, and if any of the foregoing are made, they are void with respect to Kanardia. Limitation of Liability...
  • Page 49: 10.2 Tso Information

    This product is not TSO approved as a flight instrument. Therefore, the manufacturer will not be held responsible for any damage caused by its use. The Kanardia is not responsible for any possible damage or destruction of any part on the airplane caused by default operation of instrument.

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