The invention relates to a quick-mounting and quick-dismounting structure of an aircraft interior panel, which comprises profiles arranged in parallel relatively, the profiles are fixedly connected with an aircraft body, each profile comprises a first panel body positioned above and a second panel body positioned below the first panel body, an insertion gap is reserved between the first panel body and the second panel body, and the first panel body is fixedly connected with the second panel body. An inner decoration plate is inserted between the opposite sectional materials, the two ends of the inner decoration plate are arranged in the insertion gaps in a penetrating mode, the inner decoration plate and the sectional materials are connected in a sliding mode, and clamping and fixing structures used for clamping and fixing the inner decoration plate are arranged at the positions, opposite to the inner decoration plate, of the sectional materials. The device has the effect that an installation worker can conveniently install and fix the interior trim panel in the machine body.
本申请涉及一种飞机内装板的快装快卸结构,包括有相对平行设置的型材,型材与机体之间固定连接,型材包括有位于上方的第一板体和位于所述第一板体下方的第二板体,所述第一板体和所述第二板体之间留有插接空隙,且相对的型材之间插装有内饰板,所述内饰板的两端穿设在所述插接空隙中,内饰板和型材之间滑动连接,且型材相对于内饰板的位置设置用于卡固所述内饰板的卡固结构。本申请具有便于安装人员将内饰板安装固定在机体的内部的效果。
Quick-assembly and quick-disassembly structure of aircraft interior trim panel
一种飞机内装板的快装快卸结构
2022-11-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Propeller quick disassembly and assembly structure and aircraft provided with same
European Patent Office | 2021
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