A full authority, dual channel, fault tolerant digital electronic control system for aircraft gas turbine engines has been designed by the Bendix Energy Controls Division and flight-tested on the Boeing 747 research aircraft. These efforts were part of a cooperative program between Boeing Commercial Airplane Company, Pratt & Whitney Aircraft (Commercial Products Division), Bendix Energy Controls Division, and Hamilton Standard to demonstrate the improved capability of a totally Electronic Propulsion Control System (EPCS).Interest in fully electronic engine control systems was generated by their potential for low weight, high operational reliability, easy maintenance, and low life-cycle cost. The Bendix EPCS fulfills all these potentials.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Application of Redundancy in Digital Electronic Engine Control


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Kniat, John (Autor:in) / Bluish, Joseph A. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1980



    Erscheinungsdatum :

    01.09.1980




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Control system and control method of dual-redundancy electric steering engine and dual-redundancy electric steering engine

    HUANG LI / YI AIQING / FANG HENG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Dual-redundancy control structure of steering engine

    WU GANG / MOU TONGTONG / REN WEIDONG et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Digital Flight Control System Redundancy Study

    J. McGough / K. Moses / W. Platt et al. | NTIS | 1974


    Electrical redundancy electric steering engine

    BI PEIXIN / GUO QING / DI SHIJIE et al. | Europäisches Patentamt | 2021

    Freier Zugriff