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

  • Patent Title: Aerodynamic noise reducing structure for aircraft wing slats
  • Patent Title (中): 飞机机翼板条的气动降噪结构
  • Application No.: US09837638
    Application Date: 2001-04-17
  • Publication No.: US06394396B2
    Publication Date: 2002-05-28
  • Inventor: Wolfgang GleineKnut MauUdo Carl
  • Applicant: Wolfgang GleineKnut MauUdo Carl
  • Priority: DE10019185 20000417
  • Main IPC: B64C300
  • IPC: B64C300
Aerodynamic noise reducing structure for aircraft wing slats
Abstract:
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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