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특허 상세정보

High-efficiency, supersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44    B64C-003/54    B64C-003/50   
미국특허분류(USC) 244/117A ; 244/035A ; 244/036 ; 244/046 ; 244/214 ; 244/218 ; 244/048 ; 244/158A
출원번호 US-0650686 (1996-05-20)
발명자 / 주소
대리인 / 주소
    Haefliger
인용정보 피인용 횟수 : 37  인용 특허 : 6
초록

A supersonic flight aircraft having a longitudinally forwardly extending fuselage having an axis in the direction of flight, and a wing, and which comprises the wing extending generally laterally relative to the axis, and having a leading edge angled forward or rearwardly relative to a normal to the axis at an angle , and the wing having leading edge sharpness defined by upper and lower wing surfaces, which taper toward the leading edge to define an angle .delta., closely proximate the leading edge at all spanwise locations; the angle and sharpness .delt...

대표
청구항

[ I claim:] [1.] In a supersonic flight aircraft having a longitudinally forwardly extending fuselage having an axis in the direction of flight, and a wing, the combination comprising:a) said wing extending generally laterally relative to said axis, and having a leading edge angled forward or rearwardly relative to a normal to said axis at an angle , and said wing having a leading edge sharpness defined by upper and lower wing surfaces, which taper toward the leading edge to define an angle, .delta., closely proximate the leading edge at all spanwise loc...

이 특허를 인용한 특허 피인용횟수: 37

  1. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2003116651928.
  2. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2005116966524.
  3. Arata,Allen A.; Graham,David H.. Aircraft with articulated leading edge of fuselage and wings. USP2007047204454.
  4. Arata,Allen A.. Aircraft with extendable leading edge of fuselage and wings. USP2007057216835.
  5. Arata,Allen A.. Aircraft with rotatable leading edge of fuselage and wings. USP2007077246770.
  6. Nastasi Richard F. ; Soeder Walter S.. Delta-shaped aircraft with variable camber fuselage and wing. USP2000106129308.
  7. Nelson, Chester P.. High-speed aircraft. USP200309D479501.
  8. Eakins, Mark E.; Wojciechowski, Paul M.. High-speed aircraft and methods for their manufacture. USP2010017644888.
  9. Chase, James D.; Henderson, Michael; Peter, Sturdza. Highly efficient supersonic laminar flow wing structure. USP2016019233755.
  10. Chase, James D.; Henderson, Michael; Peter, Sturdza. Highly efficient transonic laminar flow wing. USP2015038991768.
  11. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
  12. Bowcutt, Kevin G.. Hypersonic waverider variable leading edge flaps. USP2003106634594.
  13. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  14. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2003066575406.
  15. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  16. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  17. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  18. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  19. Tracy,Richard R.; Chase,James D.; Kroo,Ilan. Laminar flow wing for transonic cruise. USP2006027000870.
  20. Tracy, Richard R.; Sturdza, Peter; Chase, James D.. Laminar flow wing optimized for supersonic cruise aircraft. USP2012098272594.
  21. Tracy, Richard R.; Chase, James D.. Laminar flow wing optimized for transonic cruise aircraft. USP2013058448893.
  22. Tracy, Richard R.; Chase, James D.. Laminar flow wing optimized for transonic cruise aircraft. USP2012118317128.
  23. Tracy,Richard R.; Chase,James D.. Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings. USP2006027004428.
  24. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  25. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  26. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  27. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  28. Morgenstern,John M.; Arslan,Alan E.; Moose,Garret A.. Methods for incorporating area ruled surfaces in a supersonic aircraft. USP2007127311287.
  29. Wood, Norman. Morphing aerofoil. USP2017089745048.
  30. McGaffigan Thomas H.. Optical light pipes with laser light appearance. USP2000026031958.
  31. Arata Allen A.. Single surface multi axis aircraft control. USP2000056068219.
  32. Nelson, Chester P.. Supersonic aircraft. USP200307D477561.
  33. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  34. Lugg, Richard H.. Supersonic aircraft with shockwave canceling aerodynamic configuration. USP2013068453961.
  35. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  36. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  37. Morgenstern,John M.; Arslan,Alan E.. Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance. USP2009017475848.