- 专利标题: ELEVON CONTROL SYSTEM
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申请号: US17177974申请日: 2021-02-17
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公开(公告)号: US20210261235A1公开(公告)日: 2021-08-26
- 发明人: Carlos Thomas Miralles , Robert Nickerson Plumb , Tony Shuo Tao , Nathan Olson
- 申请人: AeroVironment, Inc.
- 申请人地址: US CA Simi Valley
- 专利权人: AeroVironment, Inc.
- 当前专利权人: AeroVironment, Inc.
- 当前专利权人地址: US CA Simi Valley
- 主分类号: B64C3/56
- IPC分类号: B64C3/56 ; B64C13/34 ; B64C3/44 ; B64C3/50 ; B64C5/12 ; B64C13/18 ; B64C9/36 ; B64C39/02 ; B64C9/02 ; B64C9/08 ; B64C9/18 ; B64C11/00
摘要:
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.