Device is fitted on extension of crankshaft instead of usual propeller hub, and carries propeller in such a way that propeller is in same position as with usual method of fitting. Dynamometer hub consists of gages with automatic regulations fitted between two main parts of device, moving independently one of the other; one of these is connected to crankshaft and the other is connected solid to propeller. Extract from 18th Report of "Deutschen Versuchsanstalt fur Luftfahrt" issued in Technical Memorandum No. 19 by Controller of Information, Department of Controller-General of Civil Aviation, Air Ministry.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The aircraft dynamometer hub


    Weitere Titelangaben:

    Eng


    Erschienen in:

    Engineering ; 110 , n 2851


    Erscheinungsdatum :

    1920


    Format / Umfang :

    3 pages


    Anmerkungen:

    10 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Dynamometer for aircraft wheel assemblies

    Engineering Index Backfile | 1956



    Dynamometer evaluation of aircraft wheel microinspection techniques

    Stanton, G.E. | Engineering Index Backfile | 1962



    Dynamometer Simulation of Aircraft Tire Wear Due to Braking

    Medzorian, John P. / Shea, Mark A. | SAE Technical Papers | 2001