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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Constant speed drive for aircraft alternators


    Additional title:

    Applied Hydraulics


    Contributors:

    Published in:

    Publication date :

    1948


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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 | European Patent Office | 2015

    Free access

    The theory of governing for aircraft turbo alternators

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