The present embodiments relate to a boom for an aircraft, and more particularly to a tail boom (3) for a helicopter (1). The tail boom (3) may comprise a watertight compartment (7) and watertight bulkheads (5, 6). The watertight bulkheads (5, 6) may close at least one end of the watertight compartment (7). The watertight bulkhead (5, 6) may include an attachment device (8), a frame (12), and a watertight fabric (11).

    본 실시예들은 항공기에 대한 붐, 및 보다 구체적으로 헬리콥터(1)에 대한 테일 붐(3)에 관한 것으로, 테일 붐(3)은 수밀 격실(7) 및 수밀 격벽(5, 6)을 포함할 수 있다. 수밀 격벽들(5, 6)은 수밀 격실(7) 중 적어도 하나의 단부를 폐쇄할 수 있다. 수밀 격벽(5, 6)은 부착 디바이스(8), 프레임(12), 및 수밀 직물(11)을 포함할 수 있다.


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    Titel :

    A BULKHEAD FOR A BOOM OF AN AIRCRAFT


    Weitere Titelangaben:

    항공기의 붐을 위한 격벽


    Beteiligte:
    DR FINK AXEL (Autor:in)

    Erscheinungsdatum :

    14.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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