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특허 상세정보

High efficiency, supersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38    B64C-021/00   
미국특허분류(USC) 244/36 ; 244/35A ; 244/204 ; 244/45R
출원번호 US-0013065 (1993-02-03)
발명자 / 주소
인용정보 피인용 횟수 : 35  인용 특허 : 0
초록

A supersonic flight aircraft having a longitudinally forwardly extending axis in the direction of flight, and a wing, comprising a 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 WW

대표
청구항

A wing for use on an airplane designed for efficient supersonic flight, said wing having leading and trailing edges, a longitudinal axis extending directionally between said edges wing tip ends and upper and lower surfaces, said wing having a main portion and a tip portion: a) said main portion of the wing having leading edge sweep angularity W30 degrees at all spanwise locations, wherein said leading edge sweep angularity at any spanwise location is defined as the angle between the tangent to the leading edge of said wing at said location, and the plane...

이 특허를 인용한 특허 피인용횟수: 35

  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. Tracy Richard R.. Aircraft wing and fuselage contours. USP2000116149101.
  4. Kosheleff, Patrick Andrew. Compression-lift aircraft. USP2014038672259.
  5. Nastasi Richard F. ; Soeder Walter S.. Delta-shaped aircraft with variable camber fuselage and wing. USP2000106129308.
  6. Tracy Richard R.. High-efficiency, supersonic aircraft. USP1999045897076.
  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. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  13. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2003066575406.
  14. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  15. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  16. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  17. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  18. Tracy,Richard R.; Chase,James D.; Kroo,Ilan. Laminar flow wing for transonic cruise. USP2006027000870.
  19. Tracy, Richard R.; Sturdza, Peter; Chase, James D.. Laminar flow wing optimized for supersonic cruise aircraft. USP2012098272594.
  20. Tracy, Richard R.; Chase, James D.. Laminar flow wing optimized for transonic cruise aircraft. USP2013058448893.
  21. Tracy, Richard R.; Chase, James D.. Laminar flow wing optimized for transonic cruise aircraft. USP2012118317128.
  22. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  23. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  24. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  25. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  26. Arata Allen A.. Single surface multi axis aircraft control. USP2000056068219.
  27. Landmann, Alan E. Structural mode shape alignment. USP2013088511609.
  28. Landmann, Alan E.. Structural mode shape alignment. USP2014118882039.
  29. Nelson, Chester P.. Supersonic aircraft. USP200307D477561.
  30. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  31. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  32. Lugg, Richard H.. Supersonic aircraft with shockwave canceling aerodynamic configuration. USP2013068453961.
  33. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  34. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  35. Northam, Robert; Lyons, Neil. Wing tip pod. USP2018029884677.