Problem of propellers for use on geared-down engines; installation of reduction gearing between crankshaft of engine and propeller hub when increase of airplane performance characteristics more than offsets added complications of installation; advantages and disadvantages of reduction gearing; decision of when to use gears must result from compromise between gains and losses involved; amount of net gain depends largely upon particular engine and airplane combination and its designed performance. (See also Soc. Automotive Engrs. Jl vol. 25, no. 6, Dec. 1929 pp. 667-671, 3 figs (discussion) p 671-672, 3 figs)


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    Titel :

    Gearing of aircraft propellers


    Weitere Titelangaben:

    West. Flying


    Beteiligte:
    Wright, T.P. (Autor:in) / Johnson, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1929


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gearing of Aircraft Propellers

    JOHNSON, R. E. / WRIGHT, T. P. | SAE Technical Papers | 1929


    Gearing of aircraft propellers

    Wright, T.P. / Johnson, R.E. | Engineering Index Backfile | 1929


    Aircraft Propellers

    HAVILL, CLINTON H. | SAE Technical Papers | 1929


    Aircraft propellers

    Havill, C.H. | Engineering Index Backfile | 1929


    Aircraft propellers

    Havill, C.H. | Engineering Index Backfile | 1929