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특허 상세정보

Wing with a wing grid as the end section

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/42    B64C-003/54    B64C-023/06   
미국특허분류(USC) 244/199 ; 244/048 ; 244/218
출원번호 US-0595588 (1996-02-01)
우선권정보 WOCH-00067 (1994-03-30)
발명자 / 주소
대리인 / 주소
    Farley
인용정보 피인용 횟수 : 23  인용 특허 : 3
초록

A wing with a wing span (b) has a main part (1), which has a substantially closed surface with respect to the flow (v) and is provided at its free end with an end section in the form of a wing grid. The wing grid has at least two parallel-staggered winglets (2). The wing grid as part of the wing span (b) takes over the intended profile circulation at the attachment point to the main part and subdivides that circulation approximately uniformly over the winglets. The same lift is produced in the end section with the at least two winglets. Thus, for the win...

대표
청구항

[ What is claimed is:] [1.] A wing comprising the combination ofa main wing part having a substantially closed surface, a distal end, a chord, a first predetermined span and a predetermined orientation and predetermined attack angle relative to incident fluid flow for producing lift; anda tip portion at said distal end of said main wing part, said tip portion comprising:a grid of at least two spaced-apart winglets having a second predetermined span, said grid being attached to said distal end of said main wing part and extending the same lift per span un...

이 특허를 인용한 특허 피인용횟수: 23

  1. Mau, Knut; Grünewald, Michael; Reichenberger, Johann; Borchers, Ingo; Drobietz, Roger. Aerodynamic flap of an aircraft having a device which influences the flap vortex. USP2012018096513.
  2. Oleson, Richard A.; Aynsley, Richard M.; Jury, Dale R.. Angled airfoil extension for fan blade. USP2012048162613.
  3. Oleson, Richard A.; Aynsley, Richard M.; Jury, Dale R.. Angled airfoil extension for fan blade. USP2014098821126.
  4. Schaber, Sven. Device for the generation of aerodynamic vortices and also a regulating flap and wing with a device for the generation of aerodynamic vortices. USP2014078783623.
  5. Aynsley, Richard M.. Fan blade modifications. USP2010027654798.
  6. Aynsley, Richard Michael. Fan blade modifications. USP2011128075273.
  7. Aynsley,Richard Michael. Fan blade modifications. USP2007087252478.
  8. Aynsley,Richard M.. Fan blades. USP2007107284960.
  9. Whitley, L. Blake; Hoofard, Richard K.. Fan blades and associated blade tips. USP2017089726192.
  10. Whitley, L. Blake. Fan with fan blade mounting structure. USP2018019874214.
  11. Day, Daryl; Hoofard, Richard K.; Walford, Brett A.. Fire control systems. USP2014098842000.
  12. Fairchild, Mark D.. Flight control method and apparatus to produce induced yaw. USP2010087780120.
  13. Fairchild,Mark D.. Flight control method and apparatus to produce induced yaw. USP2009037503527.
  14. Long, Donald James. Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow. USP2014028651813.
  15. Witte, Philipp; Campbell, Jr., Darrell D.; Tung, Billy P.; Kleshchev, Fedor. Method for attaching a split winglet to a wing. USP20190410246181.
  16. Takanori Tsukahara JP; Masahiro Obukata JP. Rotary blade of helicopter. USP2002106467732.
  17. Bussom, Richard; McVeigh, Michael A.; Narducci, Robert P.; Zientek, Thomas A.. System and method for improved rotor tip performance. USP2010077757992.
  18. Bussom,Richard; McVeigh,Michael A.; Narducci,Robert P.; Zientek,Thomas A.. System and method for improved rotor tip performance. USP2007097264200.
  19. Ulrich La Roche CH; Lucas La Roche CH. Wing comprising a distal wing grid. USP2002086431499.
  20. Witte, Philipp; Campbell, Jr., Darrell D.; Tung, Billy P.; Kleshchev, Fedor. Winglet attach fitting for attaching a split winglet to a wing. USP2016099452825.
  21. Oleson, Richard A.. Winglet for a fan blade. USP2011080642674.
  22. Oleson,Richard A.. Winglet for a fan blade. USP200903D587799.
  23. Williams, Jason Andrew. Winglet for fan blade. USP201212D672868.