首页> 外国专利> VERTICAL TAKING-OFF AND LANDING TYPE HYBRID DRONE

VERTICAL TAKING-OFF AND LANDING TYPE HYBRID DRONE

机译:垂直起降式混合动力无人机

摘要

The present invention relates to a vertical taking-off and landing type hybrid drone, including: a pair of front rotary rotors performing vertical rotation operation so that vertical taking-off and landing are performed and respectively performing independent control for control of a rockshaft of a drone; a rear rotary rotor formed on a tail wing and providing thrust thereto during flight of the drone; a dual receiver receiving a plurality of flight control signals; and a rotor control unit analyzing the plurality of flight control signals transmitted from the dual receiver and sorting the flight control signal having low error to control drive of the front and rear rotary rotors.;COPYRIGHT KIPO 2019
机译:垂直起降式混合动力无人机技术领域本发明涉及一种垂直起降式混合动力无人机,包括:一对前旋转转子,其进行垂直旋转操作,从而进行垂直起降,并分别进行独立控制,以控制飞机的摇轴。无人机后旋转转子形成在尾翼上并且在无人机飞行期间向其提供推力;双接收器,接收多个飞行控制信号; COPYRIGHT KIPO 2019;以及转子控制单元,分析从双接收器发送的多个飞行控制信号,并对具有低误差的飞行控制信号进行分类,以控制前后旋转转子的驱动。

著录项

  • 公开/公告号KR102010964B1

    专利类型

  • 公开/公告日2019-08-16

    原文格式PDF

  • 申请/专利权人 KOREAUAV CO. LTD.;

    申请/专利号KR20180164739

  • 发明设计人 KIM MU SEON;

    申请日2018-12-19

  • 分类号B64C39/02;B64C11/46;B64C29;B64D27/24;B64D45;

  • 国家 KR

  • 入库时间 2022-08-21 11:47:58

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