首页> 外国专利> AN AIRCRAFT WING WITH A MOVEABLE WING TIP DEVICE FOR LOAD ALLEVIATION

AN AIRCRAFT WING WITH A MOVEABLE WING TIP DEVICE FOR LOAD ALLEVIATION

机译:具有可移动翼尖装置的飞机机翼,用于负荷缓解

摘要

An aircraft (1) comprising a wing (5) the wing having a fixed wing (7) with a wing tip device (9) moveably mounted about a hinge (11) at the tip thereof. The wing tip device (9) is operable between a flight configuration, and a load alleviating configuration for load alleviation during flight. The aircraft (1) comprises a restraining assembly (17) operable between a restraining mode in which the wing tip device is held in the flight configuration using a restraining force such as by a brake (19), and a releasing mode in which the restraining force on the wing tip device is released, such that the wing tip device (9) may adopt the load alleviating configuration. When the wing tip device is in the flight configuration, a biasing member (23) exerts a biasing force to urge the wing tip device towards the load alleviating configuration.
机译:一种飞机(1),该飞机(1)包括机翼(5)所述的机翼,所述机翼具有固定翼(7),所述翼装置(7)具有翼尖装置(9)在其尖端的铰链(11)上可移动地安装在铰链(11)上。 翼尖装置(9)可在飞行配置之间操作,以及在飞行期间负载缓解的负荷缓解配置。 飞机(1)包括束缚组件(17),该抑制组件(17)可操作,其中翼尖装置在飞行配置中使用诸如制动器(19)的抑制力以及抑制的释放模式 释放机翼尖端装置上的力,使得机翼尖端装置(9)可以采用负载减轻配置。 当机翼尖端装置处于飞行配置时,偏置构件(23)施加偏置力以推动翼尖装置朝向负荷缓解配置。

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