- 专利标题: Vortex generator arrangement for an aircraft
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申请号: US15365133申请日: 2016-11-30
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公开(公告)号: US10543908B2公开(公告)日: 2020-01-28
- 发明人: Bruno Stefes , Wolfgang Eilken , Erich Paul
- 申请人: Airbus Operations GmbH
- 申请人地址: DE Hamburg
- 专利权人: Airbus Operations GmbH
- 当前专利权人: Airbus Operations GmbH
- 当前专利权人地址: DE Hamburg
- 代理机构: Jenkins, Wilson, Taylor & Hunt, P.A.
- 优先权: EP15197297 20151201
- 主分类号: B64C23/06
- IPC分类号: B64C23/06 ; B64C3/00 ; B64C5/02 ; B64C9/00 ; B64C9/14
摘要:
A vortex generator arrangement for an aircraft, a flow control system and an aircraft comprising such vortex generator arrangement. The arrangement includes a surface portion facing a first region of space to constitute a flow surface, a vortex generating element, an element support structure connected to the element, a mounting structure. The element support structure and the element together are rotatable between first and second positions and a biasing device, retainer and release are provided. The rotational axis extends transversely with respect to the surface portion. The projection of the element onto a projection plane is smaller in the first rotational position than in the second rotational position, the projection plane extending perpendicularly to a tangent plane of the surface portion at a reference point of the surface portion and to a predetermined direction parallel to the extension of the tangent plane.
公开/授权文献
- US20170152025A1 VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT 公开/授权日:2017-06-01
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