The invention discloses a clamping mechanism, and relates to the technical field of aerospace, the clamping mechanism comprises a clamping shell, a front hook, a rear hook and a locking structure, the front hook, the rear hook and the locking structure are arranged on the clamping shell, the front hook and the rear hook are connected through a connecting rod, and one end of the front hook and one end of the rear hook are used for clamping a supporting plate; and when the front hook and the rear hook finish clamping, the locking structure is used for locking the front hook and the rear hook. According to the clamping mechanism, the shifting device can be fixed to a supporting plate in an airplane.
本发明公开了一种夹持机构,涉及航空航天技术领域,包括夹持壳体以及设置在所述夹持壳体上的前挂钩、后挂钩和锁定结构,所述前挂钩和所述后挂钩通过连杆连接,所述前挂钩的一端和所述后挂钩的一端用于夹持支撑板,所述前挂钩与所述后挂钩完成夹持的同时,所述锁定结构用于锁定所述前挂钩和所述后挂钩。本发明的夹持机构,能够将拨动装置固定在飞机内部的支撑板上。
Clamping mechanism
一种夹持机构
16.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |