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Aircraft with a mechanical primary flight expensive device and an electrical flight stabilization, the direction of

机译:具有机械主飞行昂贵装置和电飞行稳定装置的飞机,方向

摘要

In the case of an aircraft, in particular a glider, with a a fuselage with a pilot cabin comprehensive main part (2), with a movable on the main part (2) is supported on the side of the heights -, - and / or vertical rudder, with a control (10) in the cockpit, the movable on the main part (2) and supported by way of mechanical elements (11, 12) to the heights -, - and rudders is coupled, and with a flight stabilization, the direction (16), the an electric motor (18, 19) connected with one of the main part (2) is supported on the side of the stator (20) for adjusting the heights -, - and / or lateral rudder, the electric motor (18, 19) at a (14, 15) of the mechanical elements (11, 12) attached to or integrated rotor (21) on.
机译:对于飞机,尤其是滑翔机,其机身具有飞行员座舱的主要主体(2),主体上具有可移动部件(2)的高度为-,-和/或垂直方向舵,在驾驶舱内带有控制装置(10),在主部件(2)上可移动,并通过机械元件(11、12)支撑到一定高度,并且方向舵与飞行稳定装置相连在方向(16)上,与主要部分(2)之一相连的电动机(18、19)被支撑在定子(20)的侧面上,用于调节高度-,-和/或侧向舵,电动机(18、19)的机械元件(11、12)的(14、15)固定在转子(21)上或与转子(21)集成在一起。

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