The invention discloses a tending type rudder wing mechanism which comprises a movable rudder surface and a fixed rudder surface, the movable rudder surface and the fixed rudder surface are rotationally connected through a connecting shaft, a limiting component is arranged between the movable rudder surface and the fixed rudder surface and comprises a first clamping block, a second clamping block and a torsion spring, the first clamping block is arranged at the bottom of the movable rudder surface, and the second clamping block is arranged at the bottom of the fixed rudder surface. The first clamping block is arranged on the top of the fixed control surface, the second clamping block is arranged on the top of the fixed control surface, the first clamping block is fixedly connected with the connecting shaft through the fixing pin, the second clamping block is rotationally connected with the connecting shaft, a groove is formed in the first clamping block, convex teeth are arranged on the second clamping block and matched with the groove, one end of the torsional spring is connected with the fixed control surface, and the other end of the torsional spring is connected with the connecting shaft. And the other end is connected with the connecting shaft. A rotating shaft is arranged at the bottom of the fixed control surface. The problems that an existing folding wing is complex in control structure and high in cost are solved.
本发明公开了一种趋紧式舵翼机构,包括动舵面和定舵面,所述动舵面和定舵面通过连接轴转动连接,所述动舵面和定舵面之间设置有限位部件,所述限位部件包括第一卡块、第二卡块和扭簧,所述第一卡块设置于动舵面底部,所述第二卡块设置于定舵面的顶部,所述第一卡块通过固定销与连接轴固定连接,所述第二卡块与连接轴转动连接,所述第一卡块上开设有凹槽,所述第二卡块上设置有凸齿,所述凸齿与凹槽相匹配,所述扭簧一端与定舵面相连,另一端与连接轴相连。所述定舵面底部设置有转轴。解决了现有折叠翼控制结构复杂,成本较高的问题。
Tightening type rudder wing mechanism
一种趋紧式舵翼机构
2024-10-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
THREE-WING TYPE RUDDER AND SHIP WITH THREE-WING TYPE RUDDER
European Patent Office | 2016
|