发明申请
US20130092799A1 FIXED-WING AND ELECTRIC MULTI-ROTOR COMPOSITE AIRCRAFT 审中-公开
固定式和电动多转子复合飞机

  • 专利标题: FIXED-WING AND ELECTRIC MULTI-ROTOR COMPOSITE AIRCRAFT
  • 专利标题(中): 固定式和电动多转子复合飞机
  • 申请号: US13704056
    申请日: 2011-12-01
  • 公开(公告)号: US20130092799A1
    公开(公告)日: 2013-04-18
  • 发明人: Yu TianWenyan Jiang
  • 申请人: Yu TianWenyan Jiang
  • 优先权: CN201110316929.1 20111017; CN201120397886.X 20111017
  • 国际申请: PCT/CN11/83305 WO 20111201
  • 主分类号: B64C27/26
  • IPC分类号: B64C27/26
FIXED-WING AND ELECTRIC MULTI-ROTOR COMPOSITE AIRCRAFT
摘要:
The present invention discloses a fixed-wing and electric multi-rotor composite aircraft, including an electric multi-rotor dynamic system and a main controller, the fixed-wing dynamic system and electric multi-rotor dynamic system are mutually independent structurally, the main controller includes the fixed-wing control system and an electric multi-rotor control system which is used for controlling the operation of the electric multi-rotor dynamic system, the main controller is also used for controlling the fixed-wing control system and the electric multi-rotor control system to operate independently or synergistically, the rotor rotating plane of the electric multi-rotor dynamic system is parallel to the airframe central shaft. The aircraft is able to shift between two flying modes freely, and takes off, lands and flies like a helicopter as well as a fixed-wing aircraft. A fixed-wing aircraft-helicopter mixed mode can also be used in the take-off, landing and flying process.
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