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A Vertical Take off and Landing Quadrotor Drone having A Fixed Wing

机译:具有固定翼的垂直起降四旋翼无人机

摘要

The present invention relates to a dock having a fixed wing shape capable of vertical takeoff and landing including a main wing having an upper curvature larger than a lower curvature so as to generate lifting force for supporting the weight in the air on both sides of the flying body, And more particularly to a propulsion device provided with left and right propellers on the middle portion of the main wing provided on both sides of the fixed wing flight body and having upper and lower propellers respectively on the upper and lower portions of the tail portion of the flying body, And the vertical takeoff and landing characteristics of the multi-copter with the vertical takeoff and landing of the fixed-wing aircraft and the vertical takeoff and landing with the vertical take-off and landing characteristics of the multi- It is about drone.
机译:本发明涉及一种具有能够垂直升降的固定翼形状的船坞,其包括主翼,该主翼的上曲率大于下曲率,从而产生用于在飞行的两侧支撑空气中的重量的升力。特别是涉及一种在主翼的中部设有左右螺旋桨的推进装置,该主翼的中部设在固定翼飞行体的两侧,尾部的上部和下部分别具有上下螺旋桨。固定翼飞机的垂直起降,多翼飞机的垂直起降特性以及多翼飞机的垂直起降特性关于无人机。

著录项

  • 公开/公告号KR101933003B1

    专利类型

  • 公开/公告日2018-12-27

    原文格式PDF

  • 申请/专利权人 (주)지이에스;

    申请/专利号KR20170013729

  • 发明设计人 이승우;

    申请日2017-01-31

  • 分类号B64C39/02;B64C23/06;B64C29/02;

  • 国家 KR

  • 入库时间 2022-08-21 11:51:55

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