The invention belongs to the field of aircraft landing system design and relates to an aircraft cabin door separation mechanism. The aircraft cabin door separation mechanism adopts a multi-connecting-rod rotating throwing and pushing impact unlocking separation principle and comprises an aircraft body structure, an undercarriage cabin door, a short connecting rod, a long connecting rod, an actuating cylinder, a free hinge, a rotating unlocking hinge and an undercarriage cabin door lock.
本发明属于飞行器着陆系统设计领域,涉及飞行器舱门分离机构。所述的飞行器舱门分离机构,采用多连杆旋抛+推冲解锁分离原理,包括飞行器机体结构、起落架舱门、短连杆、长连杆、作动筒、自由铰链、旋转解锁铰链和起落架舱门锁。
Aircraft undercarriage cabin door separation mechanism
一种飞行器起落架舱门分离机构
14.03.2025
Patent
Elektronische Ressource
Chinesisch
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