Pylon Restraint Systemln an embodiment, a rotorcraft (101) includes an airframe (301); a main rotor transmission (205); one or more brackets (305) mounting the main rotor transmission (205) to the airframe (301), longitudinal axes (Lo) of the one or more brackets (305) being substantially parallel with a longitudinal axis (Lo) of the rotorcraft (101); and one or more restraints (303) mounting the main rotor transmission (205) to the airframe (301), the one or more restraints (303) being mounted at an angle non-orthogonal to the longitudinal axis (Lo) of the rotorcraft (101) and a lateral axis (La) of the rotorcraft (101).


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    Title :

    PYLON RESTRAINT SYSTEM


    Additional title:

    PYLON-RÜCKHALTESYSTEM
    SYSTÈME DE RETENUE DE PYLÔNE



    Publication date :

    2021-03-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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