The invention discloses a clamping mechanism and a rotor shifting gear, and relates to the technical field of aerospace, the clamping mechanism comprises a clamping shell, a first clamping plate, a second clamping plate and a locking structure, the first clamping plate, the second clamping plate and the locking structure are arranged on the clamping shell, and the first clamping plate is located on the outer side of the second clamping plate; one end of the first clamping plate is connected with the clamping shell, the middle of the second clamping plate is rotationally connected with the clamping shell, one end of the second clamping plate is used for being connected with the locking structure, and a gap between the first clamping plate and the second clamping plate is used for clamping a supporting plate. When the first clamping plate and the second clamping plate complete clamping, the locking structure locks the second clamping plate. The shifting mechanism can be fixed to a folding supporting plate in an airplane.
本发明公开了一种夹持机构及转子拨动装置,涉及航空航天技术领域,夹持机构包括夹持壳体以及设置在所述夹持壳体上的第一夹板、第二夹板和锁定结构,所述第一夹板位于所述第二夹板的外侧,所述第一夹板的一端与所述夹持壳体连接,所述第二夹板的中部与所述夹持壳体转动连接,所述第二夹板的一端用于与所述锁定结构连接,所述第一夹板和所述第二夹板之间的间隙用于夹持支撑板,所述第一夹板和所述第二夹板完成夹持的同时,所述锁定结构锁定所述第二夹板。本发明能够将拨动机构固定在飞机内部的折叠式支撑板上。
Clamping mechanism and rotor shifting device
一种夹持机构及转子拨动装置
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 |
Multi-rotor type aircraft, aircraft arm clamping device and clamping mechanism
Europäisches Patentamt | 2015
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