A system and method to converting mechanical rotational energy of an aircraft input shaft of a transmission to electrical energy. The system includes an alternator having an inductor carried by the aircraft transmission and a magnet carried by the aircraft input shaft. The input shaft rotates the magnet in relation to the inductor, which in turn converts the mechanical rotational energy to electrical energy.


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    Titel :

    BRUSHLESS ALTERNATOR FOR HELICOPTER TRANSMISSION INSTALL


    Weitere Titelangaben:

    ALTERNATEUR SANS BALAI POUR TRANSMISSION D'HELICOPTERE


    Beteiligte:
    TURNER CRAIG (Autor:in) / STAMPS FRANK B (Autor:in) / GRIFFIN MAURICE (Autor:in)

    Erscheinungsdatum :

    22.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Enclosed Brushless Alternator

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    Enclosed Brushless Alternator

    Naghshineh, M. / Becker, J. / SAE | British Library Conference Proceedings | 1998



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    Pillai, K.P.P. / Nair, A.S. / Bindu, G.R. | Tema Archiv | 2005


    Constant speed transmission for aircraft alternator drive

    Faisandier, J. | Engineering Index Backfile | 1950