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특허 상세정보

Canard-locked oblique wing aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/40    B64C-039/12    B64C-005/04    B64C-030/00   
출원번호 US-0185465 (2014-02-20)
등록번호 US-9079663 (2015-07-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lenart, Esq., Robert P.
인용정보 피인용 횟수 : 1  인용 특허 : 23

An aircraft includes a fuselage, a main wing pivotally coupled to an aft portion of the fuselage, and a canard coupled to a forward portion of fuselage, wherein the main wing and the canard are configured to be connected together for supersonic flight and disconnected from each other for subsonic flight.


1. An aircraft comprising: a fuselage;a main wing pivotally coupled to an aft portion of the fuselage; anda canard coupled to a forward portion of fuselage;wherein the main wing and the canard are configured to be connected together for supersonic flight and disconnected from each other for subsonic flight. 2. The aircraft of claim 1, further comprising: one or more turbojet engines and a turboprop engine. 3. The aircraft of claim 2, wherein the turboprop engine includes a propeller having foldable blades. 4. The aircraft of claim 1, wherein the main win...

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  1. Woodcock Robert R. (Sylmar CA). 90 degree rotation aircraft wing. USP1991034998689.
  2. O'Shea, Hank. Aerial vehicle with variable aspect ratio deployable wings. USP2010117841559.
  3. Garrett Timothy M.. Aerodynamic body having coplanar joined wings. USP1999055899410.
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  5. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft presenting two pairs of wings and fuel tanks in fluid communication. USP2013058439310.
  6. Cabrol, Lucien. Aircraft providing with a lift structure incorporating multiple superposed wings. USP1985094541593.
  7. Alvarez Calderon F., Alberto. Aircraft with dual flight regimes. USP2014048690096.
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  10. 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.
  11. Hall Eric B. (135 ; Spring Grove Crescent Hounslow Middlesex TW3 4DA GB2). Compound wing aircraft. USP1982064336913.
  12. Ferman,Marty Allen. Device and method of control of fixed and variable geometry rhomboid wings. USP2006117131611.
  13. Heuberger Lawrence K. (Reno NV). Double cam mounting assembly for mounting an aircraft wing to a fuselage to provide an adjustable angle of attack. USP1984044444365.
  14. Fanucci,Jerome P.; King,Michael J.; Maass,David P.; Bystricky,Pavel. Extendable joined wing system for a fluid-born body. USP2006016986481.
  15. Foch, Richard J. High performance ‘X’-configuration airplane for storage and launch from a tubular container. USP2013058444082.
  16. Wolkovitch Julian (2109 Prestonwood Dr. Arlington TX 76012). Joined wing aircraft. USP1982124365773.
  17. Wolkovitch Julian (28603 Trailriders Drive Rancho Palos Verdes CA 90274). Joined wing aircraft. USP1976033942747.
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  19. Jerry E. Carlow. Mobius-like joining structure for fluid dynamic foils. USP2002116474604.
  20. Jones Robert T. (Los Altos Hills CA). Oblique-wing supersonic aircraft. USP1976073971535.
  21. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.
  22. Wood, Ryan S.; Cummings, Darold B.; Hall, David W.. VTOL aerial vehicle. USP2012078220737.
  23. Abell Clarence L. (Seattle WA). Wing pivot location and structure for oblique wing airplane. USP1979014132374.