The invention relates to an aircraft wing, a method of deploying a spoiler and a method of retracting a spoiler. In particular, an aircraft wing is provided having a wing structure and a spoiler movable between a stowed configuration and a deployed configuration. The spoiler includes an actuator configurable between an engaged mode and a disengaged mode. When the actuator is in the engaged mode, the actuator may limit movement of the spoiler and move the spoiler between the stowed configuration and the deployed configuration. In the disengaged mode, the actuator allows the spoiler to move freely so that the spoiler can pop out due to a decrease in air pressure on the aircraft wing.
本发明涉及飞行器机翼、将扰流板展开的方法和将扰流板收回的方法。特别地,提供了一种飞行器机翼,该飞行器机翼具有机翼结构和可以在收起构型与展开构型之间移动的扰流板。扰流板包括能够构造成在接合模式与断开接合模式之间的致动器。当致动器处于接合模式时,致动器可以限制扰流板的移动并使扰流板在收起构型与展开构型之间移动。在断开接合模式中,致动器允许扰流板自由移动,使得扰流板可以由于飞行器机翼上的空气压力减小而弹出。
AIRCRAFT WING, METHOD OF DEPLOYING A SPOILER AND METHOD OF RETRACTING A SPOILER
飞行器机翼、将扰流板展开的方法和将扰流板收回的方法
2022-05-10
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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