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특허 상세정보

Morphing wing for an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38    B64C-003/44    B64C-003/54    B64C-003/52    B64C-003/40   
출원번호 US-0408722 (2013-06-21)
등록번호 US-9856012 (2018-01-02)
국제출원번호 PCT/US2013/046952 (2013-06-21)
국제공개번호 WO2013/192483 (2013-12-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Karceski IP Law, PLLC
인용정보 피인용 횟수 : 1  인용 특허 : 31
초록

A morphing wing for an aircraft includes first and second structural ribs with four active members and four passive members connected therebetween. First and second active members and third and fourth active members attach at first and second positions. The first and third active members and the second and fourth active members attach at third and fourth positions. A first passive member connects between third and fifth positions. A second passive member connects between second and seventh positions. A third passive member connects between fourth and six...

대표
청구항

1. A morphing wing for an aircraft, comprising: a top surface, a bottom surface, a leading edge, a trailing edge, a tip, and a root, wherein the root is adapted for connection to the aircraft;a plurality of structural ribs disposed between the root and tip, wherein the structural ribs extend between the top surface and the bottom surface;four active members connected between adjacent first and second structural ribs of the plurality of structural ribs, the four active members being actively adjustable, wherein: a first active member and a second active m...

이 특허에 인용된 특허 (31)

  1. McKnight, Geoffrey; Barvosa-Carter, Bill; Henry, Chris; Keefe, Andrew; Ross, Richard; Herrera, Guillermo. Actuation concepts for variable stiffness materials. USP2011037901524.
  2. Maclean Brian J. (Daniel WY) Carpenter Bernard F. (Littleton CO) Misra Mohan S. (Golden CO). Adaptive control surface using antagonistic shape memory alloy tendons. USP1997095662294.
  3. Gruenewald Michael,DEX ; Moeser Clemens,DEX ; Steigenberger Josef,DEX ; Mueller Guenther,DEX. Adaptive flow body. USP2001086276641.
  4. Frederick E. To CH; Res Kammer CH. Adaptive pneumatic wings for flying devices with fixed wings. USP2002026347769.
  5. Perez Sanchez,Juan. Adjustment mechanism for a variable-shape wing. USP2006097108231.
  6. Janker Peter,DEX ; Nitschke Felix,DEX. Aerodynamic body with internal actuating drives. USP2000066070834.
  7. Monner Hans Peter,DEX. Aerofoil profile with variable profile adaptation. USP2000106138956.
  8. Piening Matthias,DEX ; Monner Hans Peter,DEX. Aerofoil profile with variable profile adaptation. USP2000126164599.
  9. Ashill Patrick R. (Bedfordshire GB2) Fulker John L. (Bedfordshire GB2). Airfoil with variable geometry expansion surface. USP1995075433404.
  10. Austin Fred (Commack NY) Knowles Gareth J. (Smithtown NY) Rossi Michael J. (Huntington NY). Apparatus and method for controlling the shape of structures. USP1996075531407.
  11. Phillips, Warren F.. Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles. USP2011027883060.
  12. Pitt,Dale M.. Apparatus for increase of aircraft lift and maneuverability. USP2006047028948.
  13. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V.. Apparatus for variation of a wall skin. USP2003076588709.
  14. Cincotta Manuel (Tiverton RI) Nadolink Richard H. (Portsmouth RI). Articulated control surface. USP1992055114104.
  15. Hamilton, Brian K.; Hassan, Ahmed; Birchette, Terrence S.; Murrill, Robert R.. Composite material for geometric morphing wing. USP2010097798443.
  16. Dockter, Gregory E.; Hamilton, Brian K.. Geometric morphing wing. USP2005066910661.
  17. Dockter, Gregory E.; Hamilton, Brian K.. Geometric morphing wing with expandable spars. USP2003096622974.
  18. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  19. Martin Willi,DEX ; Siegling Hans-Friedrich,DEX ; Kuhn Marcel,DEX ; Himmel Norbert,DEX. Load carrying structure having variable flexibility. USP2001026182929.
  20. Schmittle Hugh (605 Carolyn Rd. Glen Burnie MD 21061). Lockable free wing aircraft. USP1994015280863.
  21. Grip, Robert Erik. Mechanism for changing the shape of a control surface. USP2011118056865.
  22. Igram Dale J. (4308 Brookside Dr. Kokomo IN 46902). Reconfigurable airfoil. USP1991045004189.
  23. Lutke, Kevin R.; Kutzmann, Aaron J.. System and method for pneumatically actuating a control surface of an airfoil. USP2011108042772.
  24. Sridhar Kota. System for varying a surface contour. USP2002126491262.
  25. Muscatell Ralph P. (2007 NE. 20th Ave. Fort Lauderdale FL 33305). Variable airfoil assembly. USP1984024432516.
  26. Brown Stephen T. (Bellevue WA). Variable camber flap end seal. USP1984014427169.
  27. Law, Barnaby. Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane. USP2009107607617.
  28. Law, Barnaby. Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane. USP2011037909292.
  29. Lonsinger, Hans; Perez-Sanchez, Juan. Wing, especially a carrier wing of an airplane, having an adaptable profile. USP2010047699270.
  30. Voglsinger, Martin; Perez-Sanchez, Juan. Wing, in particular airfoil of an aircraft, with a variable profile shape. USP2011047918421.
  31. Perez Sanchez, Juan Mauricio. Wing, particularly airfoil of an aircraft, having changeable profile. USP2009057530533.

이 특허를 인용한 특허 피인용횟수: 1

  1. Wigley, Alexander T.. Shape shifting foils. USP2018049944356.