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특허 상세정보

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Aircraft providing with a lift structure incorporating multiple superposed wings

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-039/08    B64C-039/12   
미국특허분류(USC) 244/045.R; 244/123; 244/045.A; 244/091
출원번호 US-0471059 (1983-03-01)
우선권정보 FR-0003961 (1982-03-09)
발명자 / 주소
대리인 / 주소
    Fisher, Christen & Sabol
인용정보 피인용 횟수 : 33  인용 특허 : 3
초록
▼

The invention relates to an aircraft provided on either side of its fuselage with at least one lift structure constituted by at least two wings whose distal ends are connected either to each other or to at least one wing element, each structure forming in front elevation of said fuselage a closed polygon, and comprising an upper wing and a lower wing, the zone of attachment of the latter on the fuselage possibly being offset in the direction of the streamline flow with respect to the zone of attachment of the upper wing. According to the invention, each ...

대표
청구항
▼

1. An aircraft, comprising in combination: a fuselage having two sides; including on each said side of said fuselage at least one lift structure constituted by at least an upper wing and a lower wing, each said wing being connected at one end thereof to the fuselage and at the other end to at least one wing element, such that each lift structure forms in front elevation with the side of the fuselage a closed polygon; each said wing being hingedly secured to said fuselage and to a portion of said element so as to form a semi-rigid embedding, allowing...

이 특허에 인용된 특허 (3)

  1. Zimmer ; Herbert. Airplane with two superposed wings. USP1978054090681.
  2. Wolkovitch Julian (2109 Prestonwood Dr. Arlington TX 76012). Joined wing aircraft. USP1982124365773.
  3. Geraci Alexander (5221 N. Lind Ave. Chicago IL 60630) DeLouise Joseph (6 E. Monroe St. Chicago IL 60606). Short coupled airplane with variable wing lift. USP1976103985317.

이 특허를 인용한 특허 피인용횟수: 33

  1. O'Shea, Hank. Aerial vehicle with variable aspect ratio deployable wings. USP2010117841559.
  2. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft presenting two pairs of wings and fuel tanks in fluid communication. USP2013058439310.
  3. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  4. Alford, Jr., Lionel D.; Clayman, Jr., Gary J.. Blended winglet. USP2010017644892.
  5. Sommer, Geoffrey S.; Cote, Kenneth A.. Canard-locked oblique wing aircraft. USP2015079079663.
  6. Ferman,Marty Allen. Device and method of control of fixed and variable geometry rhomboid wings. USP2006117131611.
  7. Suokas, Aki. Flying device and a wing construction for the same. USP2016049308984.
  8. Frediani Aldo,ITX. Large dimension aircraft. USP1999055899409.
  9. Houck, II, Ronald G.. Lifting foil. USP2013038387912.
  10. Houck, II,Ronald G.. Lifting foil. USP2006097100867.
  11. Gall, Pierre-Emmanuel; Cros, Christophe; Lallemand, Mickaël. Method and device for the lateral stabilization of an aircraft. USP2014118888039.
  12. Jerry E. Carlow. Mobius-like joining structure for fluid dynamic foils. USP2002116474604.
  13. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Performance-enhancing winglet system and method. USP2015018936219.
  14. Gratzer, Louis B.. Split blended winglet. USP20190410252793.
  15. Gratzer, Louis B.. Split blended winglet. USP20180610005546.
  16. Gratzer, Louis B.. Split blended winglet. USP2016049302766.
  17. Gratzer, Louis B.. Split blended winglet. USP2015028944386.
  18. Gratzer, Louis B.. Split blended winglet. USP20181010106247.
  19. Gratzer, Louis B.. Split spiroid. USP2017029580170.
  20. Gratzer, Louis B.. Split spiroid. USP2015059038963.
  21. Gratzer, Louis B.. Split spiroid. USP2016099434470.
  22. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Split winglet system. USP2017059637226.
  23. August, Henry. Survivable and reusable launch vehicle. USP2004066749153.
  24. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.
  25. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015119193445.
  26. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015129199727.
  27. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015059033282.
  28. Zaman, AbuMuhammed A.. Wing tip device for an aircraft wing. USP2016129511850.
  29. Gratzer, Louis B.. Wing tip with optimum loading. USP2016079381999.
  30. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system. USP2016059346537.
  31. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system and method. USP2015129216817.
  32. Roman, Dino L.; Vassberg, John C.; Friedman, Douglas M.; Malachowski, Adam P.; Vegter, Christopher A.. Winglet system having upper and lower winglet. USP2016109463871.
  33. Malachowski, Adam P.; Chaney, Stephen R.; Ebner, Norman K.; LeDoux, Stephen T.. Winglets with recessed surfaces, and associated systems and methods. USP2012038128035.

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