The JT9D turbofan engine, soon to be in airline service on the next generation of advanced jet aircraft, will incorporate the Hamilton Standard JFC 68 main fuel control and EVC 3 engine vane control. Now in production, this control system embodies advanced control technology while retaining the basic advantages of present operational systems. Its specific advantages are improvements in weight, performance, reliability, and durability over present commercial jet engine control systems. This paper presents a discussion of the design philosophy used in creating the system, a description of the system and some advanced techniques used in its development.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The JT9D Engine Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Air Transportation Meeting ; 1969



    Erscheinungsdatum :

    01.02.1969




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    JT9D Engine Operating Experience

    Jackson, H. Alden / Pohlmann, Horst O. | SAE Technical Papers | 1970


    The JT9D Jet Engine Diagnostics Program

    Olsson, W. J. | NTRS | 1982


    JT9D jet engine diagnostics program

    Olsson, W. J. / Stromberg, W. J. | NTRS | 1981


    An introduction to the JT9D engine

    JACKSON, H. | AIAA | 1967


    JT9D-7A /SP/ jet engine performance deterioration trends

    Richter, G. P. / Olsson, W. J. / Andersen, N. B. | NTRS | 1980