The invention belongs to the field of the design of a structure. The invention provides a four-link opening mechanism of a radar cover of an airplane. The mechanism comprises a strip-shaped fixed member, an n-shaped movable member, a strip-shaped direct connecting rod and a V-shaped bent connecting rod, wherein one end of the strip-shaped fixed member is fixed on the airplane body, and the other end of the strip-shaped fixed member is hinged to one end of the strip-shaped direct connecting rod; the other end of the strip-shaped direct connecting rod is hinged to one fork ear of the n-shaped movable member, the mounting surface of the n-shaped movable member is fixedly connected with the inner side of the radar cover, the other fork ear of the n-shaped movable member is hinged to one end of the V-shaped bent connecting rod, and the other end of the V-shaped bent connecting rod is hinged to a middle fork ear of the strip-shaped fixed member.


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    Titel :

    Four-link opening mechanism of radar cover of airplane


    Beteiligte:
    SUN YADONG (Autor:in) / SHEN WEI (Autor:in) / WU JINXIANG (Autor:in) / DU JIEQIONG (Autor:in) / LI CAIXIA (Autor:in)

    Erscheinungsdatum :

    15.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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