The invention belongs to the field of aircraft valve structures, and particularly relates to an aircraft valve opening mechanism. The aircraft valve opening mechanism comprises a valve (1), a sliding rail (2), a sliding block (3) and a driver (4). The sliding rail (2) comprises a sliding section and a rotating section; the sliding block (3) is mounted in the sliding rail (2) and connected with the valve (1) through a connecting rod; the driver (4) is connected with the connecting rod; and the driver (4) drives the sliding block (3) to slide in the sliding section of the sliding rail (2) to control the opening position of the valve (1), and the driver (4) drives the sliding block (3) to rotate in the rotating section of the sliding rail (2) to control the opening angle of the valve (1). According to the aircraft valve opening mechanism, the valve can be opened according to the specified position, the opening interference problem caused by the hidden zigzag design is eliminated, the structure is simple, and operation is easy.
本申请属于飞机活门结构领域,特别涉及一种飞机活门开启机构。包括:活门(1)、滑轨(2)、滑块(3)以及驱动器(4)。所述滑轨(2)包括滑动段以及旋转段;所述滑块(3)安装在所述滑轨(2)中,所述滑块(3)通过连接杆与所述活门(1)连接;所述驱动器(4)与所述连接杆连接;其中,通过所述驱动器(4)驱动所述滑块(3)在所述滑轨(2)的滑动段中滑动,控制所述活门(1)的打开位置,通过所述驱动器(4)驱动所述滑块(3)在所述滑轨(2)的旋转段中旋转,控制所述活门(1)的打开角度。本申请的飞机活门开启机构,能够使活门按照规定的位置打开,并消除了隐身锯齿化设计带来的打开干涉问题,结构简单易操作。
Aircraft valve opening mechanism
一种飞机活门开启机构
2021-04-09
Patent
Elektronische Ressource
Chinesisch
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