Two ways of bettering gravity feed system: reducing 25 to 35 F fuel temperature rise between tank and fuel line near engine, and keeping pressure drop from tank to carburetor bowl as low as possible; in military aircraft centrifugal pumps submerged in fuel tank should be used which keep fuel system under higher pressure than atmosphere.


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    Titel :

    Light aircraft vapor lock problems


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Colt, R.A. (Autor:in) / Whitney, L.M. (Autor:in) / Bollo, F.G. (Autor:in) / Cattaneo, A.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1949


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    LIGHT AIRCRAFT VAPOR-LOCK PROBLEMS

    Cattaneo, A. G. / Bollo, F. G. / Whitney, L. M. et al. | SAE Technical Papers | 1948


    Vapor lock vs. Aircraft engines

    Ying, W.Y. | Engineering Index Backfile | 1937


    Flight test research on problems of vapor lock

    Scudder, N.F. | Engineering Index Backfile | 1938


    Flight test research on problems of vapor lock

    Scudder, N.F. | Engineering Index Backfile | 1938


    Vapor lock in aircraft engines may come from fuel line design

    Nutt, A. | Engineering Index Backfile | 1930