The present invention relates to a structure for supporting spaced components in an axial direction, and more specifically, to an axial force support structure between aircraft components, which is very easy for adjustment of the whole length and is easy for cap adjustment between a lower panel support and a lower panel. The axial force support structure includes a load tube, a first clevis and a second clevis.

    본 발명은 이격된 부품을 축방향으로 지지하기 위한 구조물에 관한 것으로, 보다 상세하게는 전체 길이 조절이 매우 용이하고, 특히 하부 패널 서포트와 하부 패널 간의 갭 조절이 용이한 항공기 부품 간의 축력지지구조물에 관한 것이다.


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    Titel :

    Strut for supporting aircraft wing parts


    Weitere Titelangaben:

    항공기 부품 간의 축력지지구조물


    Beteiligte:
    KIM CHI SOO (Autor:in) / KIM HYUNGSEOK (Autor:in)

    Erscheinungsdatum :

    11.10.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16C SHAFTS , Wellen



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