• DocumentCode
    280939
  • Title

    Application of parallel processing in fault tolerant gas turbine engine control

  • Author

    Thompson, H.A.

  • Author_Institution
    Dowty Controls, Loudwater, UK
  • fYear
    1990
  • fDate
    33217
  • Firstpage
    42370
  • Lastpage
    42374
  • Abstract
    Describes a demonstrator project investigating the use of parallel processing in fault-tolerant gas turbine engine control undertaken by Dowty Controls. The vehicle for this work is the Inmos transputer. As a multiple processor architecture is to be used there is inherent redundancy within the system and the aim of this work is to try and exploit this redundancy to introduce fault tolerance into the system while efficiently utilising the processing power available. A system simulator is under development which uses multiprocessor arrays. This simulator allows engine and controller simulations to be operated in closed-loop and allows different fault tolerant strategies and dynamic reconfiguration to be investigated. A user interface is used to alter system parameters during operation and for inducing failures in the system. Among the concepts being investigated are load balancing, dynamic scheduling, fault detection and recovery strategies
  • Keywords
    computerised control; fault tolerant computing; gas turbines; parallel processing; transputers; Dowty Controls; Inmos transputer; aero-engines; dynamic scheduling; fault detection; fault tolerance; gas turbine engine control; load balancing; multiple processor architecture; parallel processing; recovery strategies; simulator; system simulator; user interface;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    System Architectures for Failure Management, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    191418