发明授权
US06394396B2 Aerodynamic noise reducing structure for aircraft wing slats 失效
飞机机翼板条的气动降噪结构

  • 专利标题: Aerodynamic noise reducing structure for aircraft wing slats
  • 专利标题(中): 飞机机翼板条的气动降噪结构
  • 申请号: US09837638
    申请日: 2001-04-17
  • 公开(公告)号: US06394396B2
    公开(公告)日: 2002-05-28
  • 发明人: Wolfgang GleineKnut MauUdo Carl
  • 申请人: Wolfgang GleineKnut MauUdo Carl
  • 优先权: DE10019185 20000417
  • 主分类号: B64C300
  • IPC分类号: B64C300
Aerodynamic noise reducing structure for aircraft wing slats
摘要:
A hollow expandable and contractible displacement element is secured onto the concave rear surface of a slat facing the leading edge of an aircraft wing. A bleed air line supplies engine bleed air into the hollow displacement element to selectively expand or contract the displacement element, which is preferably elastically expandable. When the slat is extended, the displacement element is expanded to fill-out the concave cavity on the rear surface of the slat so as to prevent formation of a vortex in the slat air gap and thereby to reduce aero-acoustic noise. When the slat is retracted, the displacement element is contracted to be conformingly accommodated in the sickle-shaped space between the slat and the leading edge of the wing.
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