THIRD GENERATION DIGITAL LIQUID MANAGEMENT SYSTEM (DISTRIBUTED CONTROL SYSTEM FOR FUEL MANAGEMENT)
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1 THIRD GENERATION DIGITAL LIQUID MANAGEMENT SYSTEM (DISTRIBUTED CONTROL SYSTEM FOR FUEL MANAGEMENT) prepared by Jörn Unteutsch Axel Kiens 20th June 2006 copyright 2006 by AUTOFLUG GmbH 1
2 Brno University of Technology This project is partly funded within the 5th framework programme by the European Commission 20th June 2006 copyright 2006 by AUTOFLUG GmbH 2
3 An European Project Research partners from 6 european countries Airframer / System House: Eurocopter (D) Airbus (GB) Universities: Complutense Madrid (E) Alcalá (E), Brno (CZ) Fuel Components and Systems Manufacturer: Autoflug (D), Secondo Mona (I) Goodrich (F), ASG (D) 20th June 2006 copyright 2006 by AUTOFLUG GmbH 3
4 SmartFuel, a Distributed Control System For Fuel Management Main Project Target: Fuel Fuel Management Computer Valve Valve Sensor Pump Pump Sensor From the conventional solution: Central Computer Point-to-Point Connections node CANbus node node node node To a new distributed solution: CANbus No Central Computer Smart Components Advantages: Less wiring, less weigth Improved maintenanability Extended functionality 20th June 2006 copyright 2006 by AUTOFLUG GmbH 4
5 Fuel Management System (FMS) Components Sensors Valves Pumps Controllers Cockpit Fuel Panels 20th June 2006 copyright 2006 by AUTOFLUG GmbH 5
6 Fuel Management System Typical FMS Functions for Fixed Wing Aircraft : Pressure Refueling Engine Supply Trimming, Balancing Centre of Gravity (COG) Management Wing Bending 20th June 2006 copyright 2006 by AUTOFLUG GmbH 6
7 Fuel Management System Typical FMS Functions for Rotary Winged Aircraft : Pressure Refueling Engine Supply Balancing 20th June 2006 copyright 2006 by AUTOFLUG GmbH 7
8 Typical Helicopter FMS Architecture Balance pump & valve Front Tank Engine Supply Left Tank Right Tank Legend Engine Supply Rear Tank Refueling inlet BP - Balance Pump BV - Balance valve FGT- Fuel Gauge Transmitter FMC- Fuel Management Controller HLS - High Level Sensor LLS - Low Level Sensor RV - Refueling Valve SP - Supply Pump 20th June 2006 copyright 2006 by AUTOFLUG GmbH 8
9 Smart Components Sensor or Actuator (with internal electronics) Mechatronics: Internal Interface Micro-Controller Transducers and mechanics Embedded electronics Digital processing Added functionality: Built-in-Test Self-calibration Maintenance data (History) CANbus interface CANbus 20th June 2006 copyright 2006 by AUTOFLUG GmbH 9
10 Distributed Control Concept System Valve 1 Pump 7 Valve 11 Mode 2 closed running fails Valve 3 If system mode = 2 and Valve 1 = closed Valve 3 open closed closed Statemachine Each smart component reacts in accordance with local automata State-vector broadcasting When a component, reading the state vector, decides an action, it notifies this new event changing pertinent bits in the state-vector 20th June 2006 copyright 2006 by AUTOFLUG GmbH 10
11 Smart Components For Helicopter Full Scale Fuel Test Rig Provision of smart valves. Provision of smart pumps (AC and DC). Provision of smart sensors. 2 supply pumps 1 balance pump 2 refuel valves 1 balance valve 6 fuel gauge transmitters 2 level sensors (high and low) 1 fuel compensator 20th June 2006 copyright 2006 by AUTOFLUG GmbH 11
12 Simulation Support for the Project Viability studies of new concepts Checking of operational scenarios SW/HW development & testing Bus messages monitoring Validation Fault analysis 20th June 2006 copyright 2006 by AUTOFLUG GmbH 12
13 Fixed Wing Aircraft Laboratory Simulators (downscaled test rig) Gravity transfers 20th June 2006 copyright 2006 by AUTOFLUG GmbH 13
14 Laboratory Simulators (downscaled test rig ) Helicopter Physical tank simulation Electronic modules 20th June 2006 copyright 2006 by AUTOFLUG GmbH 14
15 Industrial Rig (Helicopter full scale fuel test rig ) 20th June 2006 copyright 2006 by AUTOFLUG GmbH 15
16 SmartFuel Automated Design and Simulation Process (ADSP) SmartFuel ADSP is the SmartFuel Follow Up programme This project is candidate for partly funding within the 6th framework programme by the European Commission ADSP researches a tool-supported automated design and verification process for digital fuel systems Planned Duration: 4 th quarter 2006 until 3 rd quarter 2009 Partner Companies: Autoflug GmbH ASG-Luftfahrttechnik und Sensorik GmbH Eurocopter Deutschland GmbH Secondo Mona Spa Goodrich Actuation Systems SAS Vysoke Uceni Technicke v Brne Universidad Complutense de Madrid University of Alcala Czech Space Research Centre Piaggio Aero Industries Spa 20th June 2006 copyright 2006 by AUTOFLUG GmbH 16
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