The invention relates to structural design technologies of interior trim supports for aircrafts and discloses an interior trim support for an aircraft. A support body is a U-type structural part formed integrally and is composed of a long side, short sides and a transverse side. The long side is parallel to a structural frame of the aircraft and is connected with a structural stringer through angle pieces. The short sides are of a flange structure and are provided with grooves and used for clamping spring clip supporting plate nuts. Long-strip holes are formed in the transverse side, and screws are matched with the spring clip supporting plate nuts to fixedly connect the transverse side with an interior trim plate. The interior trim support for the aircraft is simple in structure and good in technology feasibility and can be formed through sheet metal parts. The U-shaped structure facilitates support and interior trim plate positioning on an installing site and ensures installing precision; the long-strip holes in the support can effectively eliminate errors accumulated in the installing process, rapid adjustment on the installing site is achieved, working efficiency is improved, and the cost is lowered.


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    Title :

    Interior trim support for aircraft


    Contributors:
    HUANG YIJIA (author) / SUN DI (author) / GU YU (author)

    Publication date :

    2015-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR



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