首页> 外国专利> Quad Rotor Aircraft With Fixed Wing And Variable Tail Surfaces

Quad Rotor Aircraft With Fixed Wing And Variable Tail Surfaces

机译:具有固定翼和可变尾翼面的四旋翼飞机

摘要

An aircraft with four rotors, a fixed wing, and an adjustable v-tail to allow for both vertical take-off and landing and the capability to fly in straight and level flight. The angle of each rotor and engine, with respect to the airfoil surfaces to which they are attached, is adjustable, allowing for thrust to be directed either downwards, allowing the craft to hover, or backwards, allowing the aircraft to travel horizontally while lift is provided and controlled by the wing and v-tail.
机译:一架具有四个旋翼,一个固定翼和一个可调式V型尾翼的飞机,既可以进行垂直起降,又可以进行直线和水平飞行。每个旋翼和发动机相对于其所连接的机翼表面的角度都是可调的,从而允许将推力指向下方,从而允许飞机悬停或向后倾斜,从而使飞机在提升时可以水平行进由机翼和V型尾翼提供和控制。

著录项

  • 公开/公告号US2017113795A1

    专利类型

  • 公开/公告日2017-04-27

    原文格式PDF

  • 申请/专利权人 JEREMY DUQUE;

    申请/专利号US201615210664

  • 发明设计人 JEREMY DUQUE;

    申请日2016-07-14

  • 分类号B64C29;B64C27/08;B64C39/02;B64C27/52;

  • 国家 US

  • 入库时间 2022-08-21 13:50:23

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