The invention discloses a self-locking control handle structure which comprises a T-shaped handle, a pull rod, a fixing sleeve assembly and a self-locking structure, one end of the pull rod is connected with the T-shaped handle, the other end of the pull rod penetrates through the fixing sleeve assembly to be connected with a steel cable or a hydraulic valve, and a cylindrical pin is arranged in the middle of the pull rod; the fixing sleeve assembly comprises an upper fixing sleeve and a lower fixing sleeve, and the upper fixing sleeve and the lower fixing sleeve can be connected together through a sunk screw; and an end cover is arranged at the upper end of the upper fixing sleeve. The self-locking control handle structure can realize a self-locking function for a specific aircraft in a working state and a non-working state.
本发明公开了一种能够自锁的操纵手柄结构,包括T型手柄、拉杆、固定套组件、自锁结构,所述拉杆一端与所述T型手柄连接,另一端穿过固定套组件与钢索或液压阀连接,所述拉杆中部位置设有圆柱销;所述固定套组件包括上固定套、下固定套,所述上固定套和下固定套可通过沉头螺钉连接在一起;所述上固定套上端设有端盖。该发明对于特定的飞行器在工作与非工作状态能够实现具有自锁功能。
Self-locking control handle structure
一种能够自锁的操纵手柄结构
2022-02-25
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Handle locking and connecting structure of baby carrier
Europäisches Patentamt | 2016
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