发明申请
US20070246611A1 Triboelectric treatment of wing and blade surfaces to reduce wake and BVI/HSS noise 审中-公开
机翼和叶片表面的摩擦电处理,以减少尾流和BVI / HSS噪声

  • 专利标题: Triboelectric treatment of wing and blade surfaces to reduce wake and BVI/HSS noise
  • 专利标题(中): 机翼和叶片表面的摩擦电处理,以减少尾流和BVI / HSS噪声
  • 申请号: US11509782
    申请日: 2006-08-25
  • 公开(公告)号: US20070246611A1
    公开(公告)日: 2007-10-25
  • 发明人: Anadish Kumar Pal
  • 申请人: Anadish Kumar Pal
  • 优先权: IN1016/DEL/2006 20060419
  • 主分类号: B64C3/14
  • IPC分类号: B64C3/14
Triboelectric treatment of wing and blade surfaces to reduce wake and BVI/HSS noise
摘要:
Triboelectric treatment of or addition to a wing tip and an airfoil upper and lower surfaces is selectively done to electrostatically mutually charge the wing tip and the airfoil upper and lower surfaces with the atmospheric air frictionally coming in contact, in order to reduce trailing-edge vorticity and to promote interlayer mixing in the downwash. Electrostatic forces impede air rollup around the wing tip by first pulling the rolling up air from the airfoil lower surface to the wing tip side face, holding, charging and then repelling the rolling up air to the airfoil upper surface. Triboelectric layers with opposite charges, stacked chord-wise or thickness-wise, form flat and rounded wing tips for vorticity and BVI-noise reduction. For similar effects, opposite triboelectric layers, stacked span-wise, form a rounded wing tip. Lining of thick trailing edge of an airfoil is done with a triboelectric beading to reduce trailing-edge vorticity and form drag.
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