Hydraulic drive for 400-cycle alternator at constant speed, regardless of engine speed, to provide electric power required by large multi-engine aircraft; flight test experience in test B-29, B-36 and modified B-36 applications; drive design and requirements; performance data; schematic illustration of drive.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Constant speed drive for aircraft alternators


    Weitere Titelangaben:

    Applied Hydraulics


    Beteiligte:
    Schuette, L.H. (Autor:in) / Chrzanowski, R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1948


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Constant-speed drive sought for aircraft alternators

    Holliday, T.B. | Engineering Index Backfile | 1946


    Constant speed transmission for aircraft alternator drive

    Faisandier, J. | Engineering Index Backfile | 1950


    Alternators

    Robert Bosch GmbH | Springer Verlag | 2014


    Electric vechicle drive mechanism for driving multiple alternators

    RAYNOR MAURICE W | Europäisches Patentamt | 2015

    Freier Zugriff

    The theory of governing for aircraft turbo alternators

    BURNS, D.O. | Emerald Group Publishing | 1972