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Actuatable emergency exit door and an aircraft or space craft with a pressurized cabin having such an actuatable emergency exit door

机译:可致动的紧急出口门和具有加压舱室的飞机或航天器具有该可致动的紧急出口门

摘要

An actuatable emergency exit door with a door actuating device that comprises at least two connection rods that are pivotally mountable to an associated structural frame that is adapted for accommodating the actuatable emergency exit door in closed state, the at least two connection rods being provided for enabling an opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening, wherein at least one door-mounted goose neck-shaped structure is mountable to the associated structural frame for enabling an initial translational opening movement and subsequently a swiveling opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening. The invention is further related to an aircraft or space craft with a pressurized cabin having such an actuatable emergency exit door.
机译:具有门致动装置的可致动紧急出口门,该门致动装置包括至少两个可枢转地安装到相关联的结构框架的连接杆,该结构框架适于在关闭状态下容纳可致动紧急出口门,该至少两个连接杆被设置用于使能在打开期间可致动的紧急出口门相对于相关的结构框架的打开运动,其中至少一个安装在门上的鹅颈形结构可安装到相关的结构框架,以实现初始的平移打开运动以及随后的旋转打开在打开期间,可致动紧急出口门相对于相关结构框架的运动。本发明还涉及具有加压舱的飞机或航天器,该加压舱具有这种可致动的紧急出口门。

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