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특허 상세정보

Joined wing aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-039/08    B64C-003/00   
미국특허분류(USC) 244/45R ; 244/199 ; 244/123
출원번호 US-0189069 (1980-09-22)
발명자 / 주소
인용정보 피인용 횟수 : 54  인용 특허 : 3
초록

An aircraft having a fuselage and a pair of first airfoils in the form of wings extending outwardly from the vertical tail and a pair of second airfoils in the form of wings extending outwardly from the forward portion of the fuselage at a lower elevation than the first airfoils. The second wings extend rearwardly having a positive dihedral so that the tip ends of the second airfoil are located in close proximity to and may overlap the tip ends of the first wings. The pairs of wings along with the fuselage present a double triangle or diamond shape in bo...

대표
청구항

An aircraft comprising: a fuselage having an extended fin in proximity to the rearward end thereof; a first pair of airfoils connected to said fin; and a second pair of airfoils connected to said fuselage forward of and at a lower elevation than said first pair of airfoils, each of said first pair of airfoils is connected to a corresponding airfoil of said second pair by a streamlined element wherein the extended ends of said first pair of airfoils are in generally the same elevational plane as those corresponding portions of said second pair of airfoils...

이 특허를 인용한 특허 피인용횟수: 54

  1. Guida, Nicholas R.. Active winglet. USP2014048684315.
  2. Guida, Nicholas R.. Active winglet. USP2017099764825.
  3. O'Shea, Hank. Aerial vehicle with variable aspect ratio deployable wings. USP2010117841559.
  4. Garrett Timothy M.. Aerodynamic body having coplanar joined wings. USP1999055899410.
  5. Yurkovich,Rudolph N.. Aerodynamic vehicle having a variable geometry, co-planar, joined wing. USP2007077249734.
  6. Llamas Sandin, Raul Carlos. Aircraft having a lambda-box wing configuration. USP2012058186617.
  7. Carr, Robert Jonathan. Aircraft internal wing and design. USP2005016840478.
  8. Carr,Robert Jonathan; Higgins,James Michael. Aircraft internal wing and design. USP2007087258302.
  9. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft presenting two pairs of wings and fuel tanks in fluid communication. USP2013058439310.
  10. Cabrol, Lucien. Aircraft providing with a lift structure incorporating multiple superposed wings. USP1985094541593.
  11. McGinnis, John William. Aircraft stability and efficient control through induced drag reduction. USP2017019545993.
  12. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  13. Jupp Jeffrey A. (Filton GBX) Rees Peter H. (Hatfield GBX). Aircraft wing and winglet arrangement. USP1987124714215.
  14. Suciu, Gabriel L.; Chandler, Jesse M.. Aircraft with forward sweeping T-tail. USP2017059637218.
  15. August, Henry. Arch wing and forward steering for an advanced air vehicle. USP2003126659396.
  16. Alford, Jr., Lionel D.; Clayman, Jr., Gary J.. Blended winglet. USP2010017644892.
  17. Chandler, Jesse M.; Suciu, Gabriel L.. Box wing with angled gas turbine engine cores. USP2017029567062.
  18. Sommer, Geoffrey S.; Cote, Kenneth A.. Canard-locked oblique wing aircraft. USP2015079079663.
  19. Suciu, Gabriel L.; Merry, Brian D.. Conjoined reverse core flow engine arrangement. USP2017129845159.
  20. Guida, Nicholas R.. Controllable airflow modification device periodic load control. USP2017029567066.
  21. Hernadi, Andras. Decagonal box-wing aircraft. USP201904D844538.
  22. Hernadi, Andras. Decagonal boxed-wing for aircraft. USP201903D843920.
  23. McGinnis, John William. Efficient control and stall prevention in advanced configuration aircraft. USP2014028657226.
  24. Lawrence,Brian Douglas; Attaway Young,Andrea Michelle. Flier. USP200705D542708.
  25. Suokas, Aki. Flying device and a wing construction for the same. USP2016049308984.
  26. Im, Sunstar. Foldable swan-wings aircraft. USP2013068464979.
  27. Garreau, Oliver F.. Joined-wing tilt-wing aircraft. USP201503D724001.
  28. Carr,Robert Jonathan; Higgins,James Michael. Lift system for an aerial crane and propulsion system for a vehicle. USP2006127147183.
  29. Houck, II, Ronald G.. Lifting foil. USP2013038387912.
  30. Houck, II,Ronald G.. Lifting foil. USP200608D526951.
  31. Houck, II,Ronald G.. Lifting foil. USP2006097100867.
  32. Morgenstern,John M.; Arslan,Alan E.; Moose,Garret A.. Methods for incorporating area ruled surfaces in a supersonic aircraft. USP2007127311287.
  33. Jerry E. Carlow. Mobius-like joining structure for fluid dynamic foils. USP2002116474604.
  34. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2015109162755.
  35. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2018059969487.
  36. Kolom Aaron L. (Los Angeles CA). Pressure vessel with a non-circular axial cross-section. USP1991085042751.
  37. Gratzer, Louis B.. Split blended winglet. USP20190410252793.
  38. Gratzer, Louis B.. Split blended winglet. USP20180610005546.
  39. Gratzer, Louis B.. Split blended winglet. USP2016049302766.
  40. Gratzer, Louis B.. Split blended winglet. USP2015028944386.
  41. Gratzer, Louis B.. Split blended winglet. USP20181010106247.
  42. Gratzer, Louis B.. Split spiroid. USP2017029580170.
  43. Gratzer, Louis B.. Split spiroid. USP2015059038963.
  44. Gratzer, Louis B.. Split spiroid. USP2016099434470.
  45. Cellini Vito. Submersible vehicle. USP200105D442540.
  46. August, Henry. Survivable and reusable launch vehicle. USP2004066749153.
  47. August, Henry. Survivable and reusable launch vehicle. USP2005016845937.
  48. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.
  49. Wood, Ryan S.; Cummings, Darold B.; Hall, David W.. VTOL aerial vehicle. USP2012078220737.
  50. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015119193445.
  51. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015129199727.
  52. Wright, Christopher; Chu, James K.; Himisch, Jan. Wing tip device. USP2015059033282.
  53. Zaman, AbuMuhammed A.. Wing tip device for an aircraft wing. USP2016129511850.
  54. Gratzer, Louis B.. Wing tip with optimum loading. USP2016079381999.