A seal for sealing an aircraft fuel tank, an aircraft wing rib and stringer seal assembly, an aircraft wing fuel tank, an aircraft structure wing box, an aircraft wing, and a method for sealing holesare disclosed. The seal is used to seal the aircraft wing rib to the stringer, which passes through the hole at a variable position in the hole in the rib. The seal includes a self-adjusting device toabsorb any tolerances when the stringer is assembled into the hole in the rib to form the seal.

    公开了用于对飞机燃油箱进行密封的密封件、飞机翼肋和桁条密封组件、飞机机翼燃油箱、飞机结构翼盒、飞机机翼、以及用于对孔进行密封的方法。该密封件用于将飞机翼肋密封至桁条,该桁条在位于翼肋中的孔中的可变位置处穿过该孔。该密封件包括自调节装置,该自调节装置用以吸收当在桁条组装到翼肋中的孔中时候形成该密封件时的任何公差。


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    Titel :

    Aircraft fuel tank aperture sealing


    Weitere Titelangaben:

    飞机燃油箱孔密封


    Beteiligte:
    PAUL EDWARDS (Autor:in) / ANTONY PEACOCK (Autor:in) / TIMOTHY SANDERSON (Autor:in)

    Erscheinungsdatum :

    02.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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