The augmented turbofan engine, currently being developed for several advanced military applications, presents new challenges to the control designer. A fresh approach to the engine control design is necessary to exploit the promising characteristics of this propulsion system in the far-ranging areas of the flight spectrum. The General Electric Company has been developing an integrated electrical/hydromechanical control system designed expressly for this new breed of propulsion system. This paper discusses the requirements for the system, the results of control mode studies, and the highlights of the resulting control design. Special features of the control, including new sensing requirements, are discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Engine Control Concepts for the Augmented Turbofan


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    French, M. W. (Autor:in)

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970



    Erscheinungsdatum :

    1970-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Water-augmented turbofan engine

    Davison, W.R. / Sadowski, T.J. | Engineering Index Backfile | 1968


    Water-Augmented Turbofan Engine

    W. Richard Davison / Thomas J. Sadowski | AIAA | 1968


    Control Concepts for a High Bypass Aircraft Turbofan Engine

    Evens, David A. | SAE Technical Papers | 1969


    Turbofan engine and aircraft comprising turbofan engine

    GARDES PASCAL / MENOU FABIEN / GOUGEON PASCAL et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Turbofan engine

    NICHOLAS GRECH / CHRISTOPHER A MOSLEY / JOHN R WELLS | Europäisches Patentamt | 2020

    Freier Zugriff