The invention discloses an aircraft skin connecting piece and relates to the technical field of aircraft skin, the aircraft skin connecting piece comprises a skin body and a connecting piece body, a glue filling opening is formed in the middle of the top of the connecting piece body, and a plurality of lower flow guide grooves distributed at equal intervals are formed in the bottom of the connecting piece body; a transverse groove hole communicated with the glue filling opening is formed in the connecting piece body, a plurality of flow guide cavities are fixedly communicated between the bottom of the transverse groove hole and a lower flow guide groove located in the middle of the bottom of the skin body, and upper flow guide grooves distributed at equal intervals are formed in the top of the connecting piece body; through holes distributed at equal intervals are formed in one end of the top of the skin body. The flatness of the skin is good, the assembling difficulty is increased, and the working efficiency is reduced.

    本发明公开了一种飞机蒙皮连接件,涉及飞机蒙皮技术领域,包括蒙皮本体和连接件本体,所述连接件本体的顶部中间开设有填胶口,所述连接件本体的底部开设有若干等距离分布的下导流槽,所述连接件本体的内部开设有与填胶口相通的横向槽孔,所述横向槽孔的底部与位于蒙皮本体底部中间的下导流槽之间固定连通若干导流腔,所述连接件本体的顶部开设有等距离分布的上导流槽,所述蒙皮本体的顶部一端开设有等距离分布的通孔。本发明使得蒙皮本身的平整度较好,且增加了装配的难度,降低了工作效率。


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    Title :

    Aircraft skin connecting piece


    Additional title:

    一种飞机蒙皮连接件


    Contributors:
    WU XIAOPING (author)

    Publication date :

    2022-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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