A drive shaft for an aircraft according to an example of the present disclosure includes, among other things, an elongated core extending between a pair of opposed couplings, an energy absorption layer made of a composite comprising metal, the energy absorption layer disposed on the core, and a first composite ballistic layer disposed along a length of the core.


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    Titel :

    BALLISTIC RESISTANT DRIVE SHAFT


    Beteiligte:
    GURVICH MARK R (Autor:in) / ZAFIRIS GEORGIOS S (Autor:in) / MARRON EDWARD P (Autor:in) / REED BRAYTON (Autor:in) / SCHAEFER JOYEL M (Autor:in) / KING MICHAEL (Autor:in)

    Erscheinungsdatum :

    2020-02-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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