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Retractable aerodynamic device permitting the control of the wake trajectory of an aircraft trap

机译:可伸缩的空气动力学装置,可控制飞机陷阱的尾流轨迹

摘要

An aircraft provided with a wall having an exterior surface in contact with air flows external to the aircraft, an internal cavity in the aircraft, recessed relative to the exterior surface of the wall, at least one mobile trapdoor, which in closed position prolongs the exterior surface in such a way as to shut off the cavity from the exterior, and which in open position projects relative to the exterior surface in such a way as to open the cavity to the exterior, and provided with at least one mobile aerodynamic deflector, whose movement is slaved to that of the at least one trapdoor, the at least one aerodynamic deflector projecting relative to the exterior surface in a zone thereof situated outside the zone covered by the at least one trapdoor when the at least one trapdoor is open.
机译:一种具有壁的飞机,该壁具有与飞机外部的空气流接触的外表面,相对于壁的外表面凹入的飞机内腔,至少一个活动活板门,该活板活门在关闭位置延长了外部空间该表面具有从外部关闭空腔的方式,并且在打开位置相对于外表面以向外部打开空腔的方式突出,并且设有至少一个可移动的空气偏转器,至少一个活板门的运动是从动的,当至少一个活板门打开时,至少一个空气动力学偏转器在其区域中相对于外表面突出,该区域位于由至少一个活板门覆盖的区域之外。

著录项

  • 公开/公告号US8286916B2

    专利类型

  • 公开/公告日2012-10-16

    原文格式PDF

  • 申请/专利权人 BERNARD PAULY;BRUNO CHAUVEAU;

    申请/专利号US20080165965

  • 发明设计人 BERNARD PAULY;BRUNO CHAUVEAU;

    申请日2008-07-01

  • 分类号B64C1/14;

  • 国家 US

  • 入库时间 2022-08-21 17:32:03

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