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특허 상세정보

Aircraft winglet design having a compound curve profile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06    B64C-003/58   
출원번호 US-0807579 (2015-07-23)
등록번호 US-10053209 (2018-08-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Magidoff, Barry G.
인용정보 피인용 횟수 : 0  인용 특허 : 17
초록

An improved winglet design is presented for aircraft wherein the winglet configuration is well suited for aircraft wings having moderate to no aft swept, or wings having forward swept. The winglets (302) are located at the outer end of each wing (300) and curve upwardly as they extend outwardly from their intersection (304) with the wings (300). The curvature profile (303) of the winglets (302) when viewed from the rear (or front) of the aircraft at least approximates a specified curve profile made up of more than one curved section, e.g. the winglet tra...

대표
청구항

1. An aircraft including a central fuselage and a pair of wings statically secured to the sides of the fuselage, each wing comprising: an inner end secured to the fuselage, an outer end, a leading edge, and a trailing edge; anda winglet having an inner end, or transition, section, an upper, or soil, section; a leading edge and a trailing edge;wherein the inner end of said winglet is connected to the outer end of said wing, and the leading and trailing edges of the winglet are continuations of the leading and trailing edges of the wing, respectively;where...

이 특허에 인용된 특허 (17)

  1. Jupp Jeffrey A. (Filton GBX) Rees Peter H. (Hatfield GBX). Aircraft wing and winglet arrangement. USP1987124714215.
  2. Speer, Stephen R.. Aircraft winglet design having a compound curve profile. USP2015099120562.
  3. Nelson Wilbur C. (1540 Cedar Bend Drive Ann Arbor MI 48103). Airfoil tip vortex control. USP1977044017041.
  4. Welles Stanley W. (3943 SW. Rose St. Seattle WA 98136). Airframe design. USP1987064674709.
  5. Alford, Jr., Lionel D.; Clayman, Jr., Gary J.. Blended winglet. USP2010017644892.
  6. Gratzer Louis B. (2201 3rd Ave. #2004 Seattle WA 98121). Blended winglet. USP1994095348253.
  7. Ishimitsu Kichio K. (Mercer Island WA). Minimum drag wing configuration for aircraft operating at transonic speeds. USP1980064205810.
  8. Ishimitsu Kichio K. (Mercer Island WA) Van Devender Neal R. (Renton WA). Minimum drag wing configuration for aircraft operating at transonic speeds. USP1981014245804.
  9. Kovalsky,David A.; Viola,Kevin P.. Mission replaceable rotor blade tip section. USP2007077246998.
  10. Gratzer Louis B. (2201 3rd Ave. #2004 Seattle WA 98121). Spiroid-tipped wing. USP1992045102068.
  11. Kirk Philip S. (Redmond WA) Whitcomb Richard (Hampton VA). System for increasing airplane fuel mileage and airplane wing modification kit. USP1995045407153.
  12. Hackett James E. (Smyrna GA). Vortex diffuser. USP1980024190219.
  13. Mann, Alan. Wing tip device. USP2011087988100.
  14. Hackett, Kevin Christopher; Pyne, Clive Robert. Wing tip devices. USP2011077971832.
  15. Theurich, Frank; Himisch, Jan. Wing tip shape for a wing, in particular of aircraft. USP2014058727285.
  16. Ellis Roger R. (Wichita KS) Gertsen W. Marvin (Wichita KS) Conley Norman E. (Wichita KS). Wing with improved leading edge for aircraft. USP1980124240597.
  17. Goldhammer Mark I. (Bellevue WA) Schippers Karel A. (Renton WA). Wing/winglet configurations and methods for aircraft. USP1994015275358.