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특허 상세정보

Oblique-wing supersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/40   
미국특허분류(USC) 244/46
출원번호 US-0496779 (1974-08-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 38  인용 특허 : 0
초록

An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage. The pivotal attachments allow the airfoils to be yawed relative to the fuselage for high speed flight, and to be positioned at right angles with respect to the fuselage during take-off, landing, and low speed flight. The main wing and the horizontal stabilizer are upwardly curved from their center pivotal connections towards their ends to form curvilinear dihedrals.

대표
청구항

An aircraft having variable airframe geometry for accommodating efficient flight at subsonic, transonic, and supersonic speeds, comprising: a wing having an approximately elliptic planform, and a curvilinear dihedral formed by the lateral extremities of said wing being curved upwardly from the midspan so as to obtain a substantially elliptical lift coefficient distribution along its length; a single elongated fuselage pivotally connected to said wing; means for rotating said wing relative to said fuselage such that in the transonic and supersonic speed r...

이 특허를 인용한 특허 피인용횟수: 38

  1. Criswell David R. (4003 Camino Lindo San Diego CA 92122). Aerospace vehicle having multiple propulsion systems on a relatively rotatable flying wing. USP1989064836470.
  2. Cummings, Darold B.. Air vehicle having rotatable and retractable pairs of wings. USP201408D710782.
  3. Cummings, Darold B.. Air vehicle having rotating wings. USP201409D713321.
  4. Chen, Zhuo. Air vehicle having rotor/scissors wing. USP2003126669137.
  5. Chen, Zhuo. Air vehicle having scissors wings. USP2003086601795.
  6. Liu, Danny D.; Chen, Ping-Chih; Sarhaddi, Darius. Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles. USP2005086923404.
  7. Pflug, William; Tillotson, Brian J.. Bilaterally asymmetric design for minimizing wave drag. USP2016129522727.
  8. Sommer, Geoffrey S.; Cote, Kenneth A.. Canard-locked oblique wing aircraft. USP2015079079663.
  9. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  10. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  11. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  12. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  13. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  14. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  15. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  16. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  17. Piasecki, John W.; Piasecki, Frederick W.; Geiger, Brian; Johnson, Douglas; Pitcairn, David. Modular and morphable air vehicle. USP2015069045226.
  18. Piasecki, John W.; Piasecki, Frederick W.; Geiger, Brian; Johnson, Douglas; Pitcairn, David. Modular and morphable air vehicle. USP2018049944389.
  19. Piasecki, John W.; Piasecki, Frederick W.; Geiger, Brian; Johnson, Douglas; Pitcairn, David. Modular and morphable air vehicle. USP2017049610817.
  20. Piasecki, John W.; Piasecki, Frederick W.; Geiger, Brian; Johnson, Douglas; Pitcairn, David. Modular and morphable air vehicle. USP2016079393847.
  21. Corbett Marshall J. (E. Northport NY). Nuclear powered drone. USP1988114786008.
  22. McDonnell, William R. Oblique blended wing body aircraft. USP2013048408490.
  23. McDonnell, William Randall. Oblique blended wing body aircraft. USP2016099440740.
  24. Groutage Frederick D. (Laramie WY) Conjerti Samuel N. (San Diego CA) Shaw Lockburn S. (San Diego CA). Pivotal mono wing cruise missile with wing deployment and fastener mechanism. USP1989064842218.
  25. Stuhr,Victor Ken. Pivoting aircraft wing and associated method. USP2006057051974.
  26. Llamas Sandin, Raul Carlos. Pivoting stabilising surface for aircraft. USP2013078474747.
  27. Chen, Zhuo. Spacecraft and aerospace plane having scissors wings. USP2004066745979.
  28. Miller Chester W. (St. Louis County MO) Herring Ray N. (Overland MO). Staggerwing aircraft. USP1979024139172.
  29. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  30. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  31. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  32. Pflug, William; Tillotson, Brian J.. System and method for minimizing wave drag through bilaterally asymmetric design. USP2015038979018.
  33. Tyree, Anthony K.. System and method for navigating an object. USP2013088502126.
  34. Vaughan John C. (Rockville MD) Perkins ; Jr. Russel G. (Alexandria VA). Tilt-rotor wing fold mechanism and method. USP1987094691878.
  35. Miller ; Jr. John A. ; Losey ; deceased William A. ; Losey ; executor by Marion E.. Universal fluid-dynamic body for aircraft and watercraft. USP1998035730391.
  36. Melton, John E.; Dudley, Michael R.. Variable geometry aircraft wing supported by struts and/or trusses. USP2016059327822.
  37. Scheerer, David E.; Joyce, Patrick F.. Wing lift system capability expansion. USP20180910065749.
  38. Abell Clarence L. (Seattle WA). Wing pivot location and structure for oblique wing airplane. USP1979014132374.