首页> 外国专利> FLAPPING TYPE FLIGHT VEHICLE, CAPABLE OF GENERATING A LIFT FORCE DUE TO AN OPERATION VERTICALLY SWINGING A WING IN A PREDETERMINED RANGE

FLAPPING TYPE FLIGHT VEHICLE, CAPABLE OF GENERATING A LIFT FORCE DUE TO AN OPERATION VERTICALLY SWINGING A WING IN A PREDETERMINED RANGE

机译:襟翼飞行器,由于在预定范围内垂直摆动机翼,因此能够产生升力

摘要

PURPOSE: A flapping type flight vehicle is provided to improve flight stability and to maintain a stable and continuous lift force by generating the lift force while four wings vertically swing in opposite directions as two groups.;CONSTITUTION: A flapping type flight vehicle comprises a hub(10), a first wing unit(21), a second wing unit(22), and a driving unit. The hub is installed in the flight vehicle. The first wing unit is rotatably and vertically connected around a rotary shaft(11) which is horizontal to the hub. The first wing unit comprises two wings(21a,21b) extended to opposite directions around the hub. The second wing unit is vertically and rotatably connected around the rotary shaft which is horizontal to the hub. The second wing unit comprises two wings(22a,22b) extended to the opposite directions around the hub. The first and second wing units simultaneously reciprocate in the opposite direction by the driving unit.;COPYRIGHT KIPO 2013
机译:目的:提供一种拍打式飞行器,通过产生升力同时四个机翼以两组相反的方向垂直摆动,从而提高飞行稳定性并保持稳定且连续的升力。构成:拍打式飞行器包括一个轮毂(10),第一机翼单元(21),第二机翼单元(22)和驱动单元。轮毂安装在飞行器中。第一机翼单元绕水平于轮毂的旋转轴(11)可旋转且垂直地连接。第一机翼单元包括围绕机壳沿相反方向延伸的两个机翼(21a,21b)。第二机翼单元围绕与轮毂水平的旋转轴竖直且可旋转地连接。第二机翼单元包括围绕机壳沿相反方向延伸的两个机翼(22a,22b)。第一和第二翼单元同时由驱动单元沿相反方向往复运动。; COPYRIGHT KIPO 2013

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号