System selected for military logistics airplane consists of four General Electric TF39-GE-1 turbofan engines, installed in short fan duct nacelles, which are pylon mounted beneath wings; propulsion installation includes pylon, nacelle, engine air induction and exhaust systems, thrust reverser, and various other subsystems and accessories; integration of these systems results in nacelle of long slender profile having diameter of 102.5 in. and length of 314.6 in.; description of structural features and various subsystems, including air bleed, engine starting, and fire protection systems; installation requirements and parameters to consider; high bypass ratio, short duct, and turbofan engine configuration; accessibility and maintenance features.


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    Titel :

    C-5A propulsion system installation


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Herring, H.W. (Autor:in) / Lee, G.G. (Autor:in) / Reynolds, B.I. (Autor:in)

    Kongress:

    SAE Meeting ; 1968 Engine mounting



    Erscheinungsdatum :

    1968


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    C-5A Propulsion System Installation

    Reynolds, B. I. / Lee, G. G. / Herring, H. W. | SAE Technical Papers | 1968


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