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An actuator device based on a shape memory alloy, and a wing flap assembly fitted with such an actuator device

机译:基于形状记忆合金的致动器装置以及装配有这种致动器装置的机翼襟翼组件

摘要

A wing-flap assembly comprises a flap (20; 200) made up of a plurality of flap sections (21, 22, 23; 201, 202, 203, 204), in which each flap section is connected to the preceding one in a rotatable manner, and one or more actuator devices (10) adapted to control the rotation of the flap sections. Each actuator device comprises an extended element (11) made of shape memory alloy and an arch-shaped framework (12) made of elastic material, to which the extended element is fixedly connected under tension. Each end (11a, 11b) of the extended element is fixed to a respective end (12a, 12b, 12ab) of the arch-shaped framework. At least one of the actuator devices is connected at one end to the first of the flap sections, and on the other side it is adapted to be connected to a wing structure (W).
机译:机翼-襟翼组件包括由多个襟翼部分(21、22、23; 201、202、203、204)组成的襟翼(20; 200),其中每个襟翼部分在一个方向上与前一个襟翼部分连接。旋转方式,以及一个或多个致动器装置(10),用于控制襟翼部分的旋转。每个致动器装置包括由形状记忆合金制成的延伸元件(11)和由弹性材料制成的弓形框架(12),该延伸元件在张力下固定地连接至该框架。延伸元件的每个端部(11a,11b)固定到拱形框架的相应端部(12a,12b,12ab)。致动器装置中的至少一个在一端连接至第一个襟翼部分,并且在另一侧,其适于连接至机翼结构(W)。

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