The invention relates to an aircraft, an actuation system for a cargo door of an aircraft and a method of opening a cargo door of an aircraft. The aircraft comprises: a body having an opening to a cargo compartment; and a cargo door covering the opening when it is in the closed position. The cargo door is rotated outwardly from a closed position to a first open position with a first actuator. Then, in a first open position, the actuator rod is mounted by coupling a first end of the actuator rod to the body and a second end of the actuator rod to the cargo door. Then, by increasing the distance between the first end and the second end of the actuator rod, the cargo door is rotated outwardly from the first open position to the second open position with the actuator rod.
本发明涉及飞行器、用于飞行器的货物门的致动系统和打开飞行器的货物门的方法。该飞行器包括:本体,该本体具有通向货物舱的开口;以及货物门,该货物门在其处于关闭位置时覆盖开口。利用第一致动器将货物门从关闭位置向外旋转至第一打开位置。然后,在第一打开位置,通过将致动器杆的第一端部联接至本体并且将致动器杆的第二端部联接至货物门来安装致动器杆。然后,通过增加致动器杆的第一端部与第二端部之间的距离,利用致动器杆将货物门从第一打开位置向外旋转至第二打开位置。
Aircraft, actuation system for cargo door of aircraft, and method of opening cargo door of aircraft
飞行器、用于飞行器的货物门的致动系统和打开飞行器的货物门的方法
29.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2025
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