Influence of aircraft and installation characteristics on design of propellers in 500 to 1000 shp class is shown; these characteristics have significant effect on propeller performance, weight, and stress levels; effects of aircraft geometry and flight conditions on propeller blade selection and pitch change system design are considered; selection of propeller blade is based on desired propeller performance, propeller diameter limitation, and steady and vibratory stress levels; magnitude of steady stress depends upon power loading of blade; magnitude of vibratory stress depends upon nacelle tilt, gross weight, lift characteristics and other aircraft parameters; examples of installations.


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    Titel :

    Propeller design consideration for turbine powered aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Currie, D.P. (Autor:in)

    Kongress:

    SAE Meeting ; 1968 Propellers



    Erscheinungsdatum :

    1968


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Propeller Design Consideration for Turbine Powered Aircraft

    Currie, Daniel P. | SAE Technical Papers | 1968


    Flight experience with turbine propeller powered aircraft

    Loomis, R.C. / Shannon, E.D. | Engineering Index Backfile | 1951


    “Flight Experience With Turbine Propeller Powered Aircraft”

    SHANNON, E. D. / LOOMIS, R. C. | SAE Technical Papers | 1951


    Flight experience with turbine propeller powered aircraft

    Loomis, R.C. / Shannon, E.D. | Engineering Index Backfile | 1951


    "Python" propeller-turbine aircraft engine

    Engineering Index Backfile | 1949