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Civil aircraft door interior trim lock catch assembly
The civil aircraft door interior trim lock catch assembly comprises a hasp, a cover plate, an opening and closing plate, hinge mechanisms and a lock catch mechanism, an opening and closing hole is formed in the cover plate, the hinge mechanisms are arranged on the cover plate, the working end of each hinge mechanism is connected with the opening and closing plate, the opening and closing plate is in butt joint with the interior of the opening and closing hole, the lock catch mechanism is arranged on the opening and closing plate, and the lock catch mechanism is in butt joint with the hasp. The aircraft slide trim cover can be connected with an aircraft structure through the locking assembly, the aircraft trim cover is prevented from shaking or even being opened in the bumping process of an aircraft, safety is improved, meanwhile, opening is convenient, the fixing plate is arranged so that the connecting stability of the locking assembly and trim can be improved, and the service life can be prolonged. And the opening and closing hole and the opening and closing plate are arranged to be square, so that the operation convenience is improved.
本发明公开了一种民用飞机门内饰锁扣组件，包括搭扣、盖板、开合板、铰链机构、锁扣机构，盖板上设有开合孔，盖板上设有若干铰链机构，每个铰链机构工作端和开合板连接，开合板对接于开合孔内，锁扣机构设于开合板上，锁扣机构和搭扣对接，锁定组件能将飞机滑梯装饰罩和飞机结构连接，防止飞机装饰罩在飞机颠簸中晃动甚至被打开，提升了安全性，同时也方便打开，设置固定板是为了使锁定组件和内饰连接的稳定性，提升使用寿命，将开合孔、开合板设置成方形提升了操作的便捷性。
Civil aircraft door interior trim lock catch assembly
The civil aircraft door interior trim lock catch assembly comprises a hasp, a cover plate, an opening and closing plate, hinge mechanisms and a lock catch mechanism, an opening and closing hole is formed in the cover plate, the hinge mechanisms are arranged on the cover plate, the working end of each hinge mechanism is connected with the opening and closing plate, the opening and closing plate is in butt joint with the interior of the opening and closing hole, the lock catch mechanism is arranged on the opening and closing plate, and the lock catch mechanism is in butt joint with the hasp. The aircraft slide trim cover can be connected with an aircraft structure through the locking assembly, the aircraft trim cover is prevented from shaking or even being opened in the bumping process of an aircraft, safety is improved, meanwhile, opening is convenient, the fixing plate is arranged so that the connecting stability of the locking assembly and trim can be improved, and the service life can be prolonged. And the opening and closing hole and the opening and closing plate are arranged to be square, so that the operation convenience is improved.
本发明公开了一种民用飞机门内饰锁扣组件，包括搭扣、盖板、开合板、铰链机构、锁扣机构，盖板上设有开合孔，盖板上设有若干铰链机构，每个铰链机构工作端和开合板连接，开合板对接于开合孔内，锁扣机构设于开合板上，锁扣机构和搭扣对接，锁定组件能将飞机滑梯装饰罩和飞机结构连接，防止飞机装饰罩在飞机颠簸中晃动甚至被打开，提升了安全性，同时也方便打开，设置固定板是为了使锁定组件和内饰连接的稳定性，提升使用寿命，将开合孔、开合板设置成方形提升了操作的便捷性。
Civil aircraft door interior trim lock catch assembly
一种民用飞机门内饰锁扣组件
MIAO PENG (author) / FENG QINGXIAO (author)
2023-08-25
Patent
Electronic Resource
Chinese
IPC:
E05C
Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster
,
BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
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