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    • 2. 发明公开
    • 비행체의 날개 구동장치
    • 用于驾驶飞机的设备
    • KR1020020065649A
    • 2002-08-14
    • KR1020010005764
    • 2001-02-07
    • 엘지이노텍 주식회사
    • 이원영
    • B64C9/24
    • B64C13/40F15B13/06F15B15/06F15B2211/4053
    • PURPOSE: A wing driving apparatus of an aircraft is provided to improve productivity, and to reduce the size and manufacturing cost by controlling the wings of the aircraft with supplying pneumatic pressure to pistons selectively in rotating. CONSTITUTION: A wing driving device of an aircraft is composed of first and second pistons(7,8) having an operating arm combined with wing shafts(3,4) through links(5), and adjusting the angle of wings(1,2); first and second passages(10,11) connected to a closing cover to close pistons to supply compressed air to first and second pistons in turning an operating body(14); a duct guiding air in flying; the operating body having a supply hole(13) supplying air from the duct to the first or second passage; and first and second magnets(15,16) turning the operating body to connect the supply hole to the first or second passage by magnetizing according to input current. The wings of the aircraft are controlled by supplying air to the piston with simple structure.
    • 目的:提供飞行器的机翼驱动装置,以通过在旋转中选择性地向活塞提供气动压力来控制飞行器的机翼来降低生产率并减小尺寸和制造成本。 构成:飞机的翼驱动装置由具有与通过连杆(5)的翼轴(3,4)组合的操作臂的第一和第二活塞(7,8)组成,并且调节翼的角度(1,2 ); 第一和第二通道(10,11),其连接到关闭盖以关闭活塞以在转动操作体(14)时向第一和第二活塞供应压缩空气; 引导空气飞行的导管; 所述操作体具有从所述管道向所述第一或第二通道供应空气的供应孔(13) 以及第一和第二磁体(15,16),其转动操作体,以根据输入电流进行磁化将供应孔连接到第一或第二通道。 飞机的机翼通过以简单的结构向活塞供应空气来控制。