The invention belongs to the technical field of aviation, and particularly relates to a side opening type service door serving as an emergency exit for an airplane and a mechanism of the side opening type service door. A pressure relief cam, a latch cam, a lifting cam and an inner handle for driving the first rotating shaft to rotate are arranged on the first rotating shaft; the pressure relief cam is connected with a pressurization prevention mechanism used for blocking a cabin door opening frame through a connecting rod mechanism, the latch cam is connected with a second rotating shaft through a connecting rod mechanism, and the lifting cam is connected with a lifting assisting mechanism through a connecting rod. The pressurization prevention mechanism is connected with a lock mechanism used for limiting movement of the second rotating shaft through a connecting rod mechanism. One end of the second rotating shaft is provided with a latch mechanism rotating by a preset angle to latch the cabin door body, the outer handle is in linkage with the inner handle through the connecting rod mechanism, mechanical logic control of all sub-mechanisms meeting the clause requirements is achieved through the cam mechanism, the limited space of the structure is fully utilized to complete arrangement of multiple mechanisms, and it is guaranteed that the cabin door is reliably locked when closed.
本申请属于航空技术领域,特别涉及一种飞机用兼作应急出口的侧开式服务门及其机构,舱门主体通过铰链臂机构铰接在机身舱门框上;第一转轴上具有泄压凸轮、闩凸轮、提升凸轮以及驱动第一转轴旋转的内手柄;泄压凸轮通过连杆机构与用于将舱门口框封堵的增压预防机构连接,闩凸轮通过连杆机构与第二转轴连接,提升凸轮通过连杆与提升助力机构连接;增压预防机构通过连杆机构与用于限制第二转轴运动的锁机构连接;第二转轴一端具有旋转预设角度将舱门主体上闩的闩机构,外手柄通过连杆机构与内手柄联动,通过凸轮机构实现了满足条款要求的各子机构的机械式逻辑控制,充分利用结构有限空间完成众多机构布置,保证舱门关闭时可靠锁定。
Side-opening service door serving as emergency exit for airplane and mechanism of side-opening service door
一种飞机用兼作应急出口的侧开式服务门及其机构
2024-10-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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