Requirements in application of propellers to gas turbine engines, three current types discussed, being direct connected engine, compound compressor type, and free propeller turbine type; typical braking propeller circuit for direct connected turbine engine propeller shown diagrammatically; reference to magnitude of hydraulic and inertia loads associated with variable pitch propellers. (See also - (discussion) p 121-4; Engineer v 189 n 4917 Apr 21 1950 p 476-7 (discussion) 481; Aircraft Eng v 22 n 259 Sept 1950 p 264-72)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Recent developments of mechanism of hydraulic variable-pitch aircraft propeller


    Weitere Titelangaben:

    Instn Mech Engrs -- Proc (War Emergency Proc)


    Beteiligte:
    Milner, H.L. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





    Double-variable-pitch-propeller aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff

    Electro-hydraulic servo constant-speed variable-pitch propeller mechanism

    SHI LI / HONG JUN / PAN XINQI | Europäisches Patentamt | 2021

    Freier Zugriff