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Aeroplane with a mechanical primary flight control and an electric flight stabilizer

机译:飞机带有机械初级飞行控制和电动飞行稳定剂

摘要

Aeroplane (1) withA trunk (3) with a pilot cabin (9) with a main structure (2),a height, cross and/or side wheel, which is movably located on the main structure (2), 6, 7, 8;a steering wheel (10) in the pilot cab (9), which is moveably located at the main structure (2) and connected to the height, cross and/or side wheel by mechanical elements (11, 12) (6, 7, 8); andA flight stabilizer (16) having an electric motor with a stator located on the main structure (2) to adjust the height, cross and/or side wheel (6, 7, 8);where the electric motor has a runner fixed to or integrated in one of the mechanical elements (11, 12), characterised by the fact that one of the mechanical elements (11, 12) is a control rod (14, 15) and the electric motor is a linear engine (18, 19).
机译:飞机(1)与带有主结构(2)的试点舱(9)的行李箱(3),高度,交叉和/或侧轮,可移动地位于主结构(2),6,7,8上;导驾驶室(9)中的方向盘(10),其在主结构(2)处可移动,并且通过机械元件(11,12)连接到高度,交叉和/或侧轮(6,7, 8);和具有电动机的飞行稳定器(16),该电动机具有位于主结构(2)上的定子,以调节高度,交叉和/或侧轮(6,7,8);当电动机具有固定在一个机械元件(11,12)中的转轮固定或集成的那里,其特征在于机械元件(11,12)中的一个是控制杆(14,15)和电动电动机是线性发动机(18,19)。

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