- 专利标题: VERTICAL TAKE-OFF AND LANDING (VTOL) WINGED AIR VEHICLE WITH COMPLEMENTARY ANGLED ROTORS
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申请号: US17573353申请日: 2022-01-11
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公开(公告)号: US20220297828A1公开(公告)日: 2022-09-22
- 发明人: Henry Thome Won , Quentin Lindsey
- 申请人: AeroVironment, Inc.
- 申请人地址: US VA Arlington
- 专利权人: AeroVironment, Inc.
- 当前专利权人: AeroVironment, Inc.
- 当前专利权人地址: US VA Arlington
- 主分类号: B64C27/26
- IPC分类号: B64C27/26 ; B64D27/06 ; B64C29/02 ; B64C39/02
摘要:
Systems, devices, and methods for an aircraft having a fuselage; a wing extending from both sides of the fuselage; a first pair of motors disposed at a first end of the wing; and a second pair of motors disposed at a second end of the wing; where each motor is angled to provide a component of thrust by a propeller attached thereto that for a desired aircraft movement applies a resulting torque additive to the resulting torque created by rotating the propellers.