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특허 상세정보

Variable control aircraft control surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/52   
미국특허분류(USC) 244/213 ; 244/90R ; 244/215 ; 244/219
출원번호 US-0509521 (1990-04-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 56  인용 특허 : 0
초록

A variable contour control surface (30a) and a transition section (30a) are designed to eliminate the discontinuities that exist between an aircraft wing control surface and the wing itself. The variable contour is provided by translating the top skin of the control surface relative to the top surface of the wing with the bottom surfaces of the wing and control surface being joined as a single surface. This movement results in a change in the camber of the control surface. The transition section (30a) is a flexible connection between the inboard and outb...

대표
청구항

An aircraft wing assembly comprising: (a) a main wing portion having a top skin and a bottom skin; (b) a variable contour control surface having a top skin and a bottom skin, either said top skin of said variable contour control surface or said bottom skin of said variable contour control surface being attached to the corresponding top or bottom skin of the main wing portion and the other skin of said variable contour control surface being translatable relative to the corresponding other skin of the main wing portion; (c) means for translating said trans...

이 특허를 인용한 특허 피인용횟수: 56

  1. Whalen, Edward A.; Goldhammer, Mark I.. Active flow control on a vertical stabilizer and rudder. USP2015079090326.
  2. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard. Active reinforced elastomer system. USP1999085931422.
  3. Young Kendall G. ; Zimmerman Phil S.. Adaptive control surface apparatus. USP2000126164598.
  4. Kendall G. Young ; Steven L. Pauletti. Aerodynamic control surface system. USP2002106467733.
  5. Wille Robert Henry. Aircraft hinge. USP2001086276026.
  6. Morgenstern, John M.; Arslan, Alan. Aircraft lift device for low sonic boom. USP2005086935592.
  7. Gruensfelder Cynthia Ann ; Geiger Micael Watson ; Jacobs Jack Howard ; Wille Robert Henry. Apparatus for eliminating gaps in an aircraft. USP1999115979828.
  8. Gruensfelder Cynthia Ann. Auxiliary inlet for a jet engine. USP2000066079667.
  9. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry. Blade seal for an aircraft. USP1999065913494.
  10. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Braking assembly and system. USP2003126655504.
  11. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Concealed air vents. USP2003066571820.
  12. Wille Robert Henry. Conformable weapons platform. USP1999115988567.
  13. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Container holder that utilizes moldline structures. USP2003046547117.
  14. Geders, Paul F.. Continuous moldline technology (CMT) elastomeric control surface. USP2014088814100.
  15. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
  16. Caton John Harold ; Hobey Michael James ; Groeneveld John David ; Jacobs Jack Howard ; Wille Robert Henry ; Brase ; Jr. Lawrence Otto. Control surface for an aircraft. USP2001046209824.
  17. John Harold Caton ; Michael James Hobey ; John David Groeneveld ; Jack Howard Jacobs ; Robert Henry Wille ; Lawrence Otto. Brase, Jr.. Control surface for an aircraft. USP2002026349903.
  18. Nastasi Richard F. ; Soeder Walter S.. Delta-shaped aircraft with variable camber fuselage and wing. USP2000106129308.
  19. John Cleveland Waldrop, III ES. Elastic ground plane. USP2002016337294.
  20. Waldrop ; III John Cleveland,ESX. Elastic ground plane and method. USP2000046048581.
  21. Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A.. Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction. USP2014048695925.
  22. Arata, Allen A.. Elastomeric transition. USP2018059975623.
  23. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP2000116145791.
  24. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  25. Geiger Michael Watson. Environmental coating for an elastomer panel. USP1999095958803.
  26. Gruensfelder Cynthia Ann ; Wille Robert Henry. Expandable aircraft bay and method. USP1999115975463.
  27. Gruensfelder Cynthia Ann ; Wille Robert Henry ; Ellis James Richard ; Diller Joseph Brice. Expandable aircraft cargo bay and method. USP2000056068215.
  28. Ellis James R. ; Diller Joseph B.. Expandable aircraft section. USP1998095803405.
  29. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry. Expandable fuel cell. USP1999075927651.
  30. Gruensfelder Cynthia Ann. Folding wing for an aircraft. USP2000066076766.
  31. Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
  32. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
  33. Gruensfelder Cynthia Ann ; Brase ; Jr. Lawrence O.. Leading edge for an aircraft. USP2001046213433.
  34. Young Kendall Gardner ; Pauletti Steven Louis. Low density flexible edge transition. USP2001016173924.
  35. Gruensfelder Cynthia Ann ; Wille Robert Henry. Mission adaptive inlet. USP2000076089505.
  36. Gruensfelder Cynthia Ann ; Wille Robert Henry. Mission adaptive inlet. USP2001076260567.
  37. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  38. Arata, Allen A.. Multi-purpose aircraft cavity. USP2003126663047.
  39. Becker, Juergen. Process for designing flight controllers. USP2004116816823.
  40. Cameron Dean Emory ; Geders Paul Francis ; Geiger Michael Watson ; Roberts Dennis Allan ; Wille Robert Henry. Reinforced elastomer panel. USP2000026027074.
  41. Dean Emory Cameron ; Paul Francis Geders ; Michael Watson Geiger ; Dennis Allan Roberts ; Robert Henry Wille. Reinforced elastomer panel. USP2002046375122.
  42. Beier Theodor Harry ; Haake John Martin ; Wille Robert Henry ; Jacobs Jack Howard. Reinforced elastomer panel with embedded strain and pressure sensors. USP1999045896191.
  43. Sommer William Arthur ; Wille Robert Henry. Retractable sensor system for an aircraft. USP1999075918834.
  44. Kenneth D. Hill. Rotatable wave-forming apparatus. USP2002016336771.
  45. Young Kendall Gardner ; Pauletti Steven Louis. Rotor driven edge. USP2001066244542.
  46. Martin Hernandez, Agustín Mariano. Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser. USP2010127850119.
  47. Appa Kari. Seamless mission adaptive control surface. USP1999035887828.
  48. Volk John Alan. Selectively rotatable and torsionally flexible aerodynamic control apparatus. USP2000076089503.
  49. Jasklowski, Christopher T.. Shape memory alloy actuation system for variable area fan nozzle. USP2017029581145.
  50. Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
  51. Da Rocha-Schmidt, Luiz. Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts. USP20181210150557.
  52. Conway, Jr., George Louis; Young, Kendall G.; Stroud, Ron L.. Single aperture conformal aircraft bays. USP2003036536711.
  53. McCallum, Brent N.; Young, Kendall G.. Subdermally-reinforced elastomeric transitions. USP2003066575407.
  54. Wille Robert Henry. Tail for an aircraft. USP1999095947422.
  55. Kahara Bryan D. ; Priestley Richard T. ; Seho Kenneth E.. Variable displacement fuel tank for aircraft. USP1999115975466.
  56. Hill Kenneth D.. Wave-forming apparatus. USP2000026019547.