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특허 상세정보

Inflatable airfoil device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-015/00   
미국특허분류(USC) 244/134A
출원번호 US-0666996 (2000-09-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, L.L.P.
인용정보 피인용 횟수 : 44  인용 특허 : 27
초록

An airfoil device (10) for attachment to the wing (14) of an aircraft (12). The airfoil device (10) has a chamber (30) which is inflatable to provide a lift-enhancing airfoil geometry to the wing (14) and other chambers (32) which are inflatable to provide deicing forces to remove ice accumulation on the wing (14). When installed on the wing (14), the airfoil device (10) closely conforms to the wing's airfoil geometry (e.g., low camber, sharp leading edge) when the lift-enhancing chamber (30) and the deicing chambers (32) are in a deflated condition. The...

대표
청구항

1. An airfoil device for attachment to the wing of an aircraft, said airfoil device comprising:a base layer for attachment to the wing of the aircraft; a lift-enhancing chamber positioned over said base layer which is inflatable to provide a lift-enhancing airfoil geometry to the wing; and deicing chambers positioned over said base layer which are inflatable to provide deicing forces to remove ice accumulation on the wing.

이 특허에 인용된 특허 (27)

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  2. Rauckhorst Richard L. (North Canton OH). Airfoil with integral de-icer using overlapped tubes. USP1993095248116.
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  7. Briscoe James A. (Doylestown OH) Putt James C. (Doylestown OH) Phillips ; II Ronald W. (Mogadore OH) Leffel Kevin L. (Akron OH). De-icer. USP1989064836474.
  8. Briscoe James A. (Doylestown OH) Putt James C. (Doylestown OH) Phillips ; II Ronald W. (Mogadore OH) Tenison Gary V. (Massillon OH) Leffel Kevin L. (Akron OH). De-icer. USP1989054826108.
  9. Putt James C. (Doylestown OH) Lefeel Kevin L. (Akron OH). De-icer. USP1988054747575.
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  14. Dorsett Kenneth Merle ; Stewart Christopher Sean. Inflatable structures to control aircraft. USP2000016015115.
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  16. Fahrner Alan J. (Canton OH) Weisend ; Jr. Norbert A. (Cuyahoga Falls OH). Leading edge pneumatic deicer assembly. USP1994085337978.
  17. Briscoe James A. (Doylestown OH) Putt James C. (Doylestown OH) Phillips ; II Ronald W. (Mogadore OH). Method and apparatus for deicing a leading edge. USP1989094865291.
  18. Rauckhorst ; III Richard L. (North Canton OH) Leffel Kevin L. (Akron OH). Modular ice protection assembly. USP1995065427332.
  19. Ely Duain N. (Uniontown OH) Macarchenia Joseph H. (Tallmadge OH). Pneumatic de-icer having improved aerodynamic characteristics. USP1995095449133.
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  21. Kageorge Pedro W. (Cuyahoga Falls OH). Pneumatic deicers with inextensible threads. USP1987084687159.
  22. Kageorge Pedro W. (Cuyahoga Falls OH). Pneumatic deicers with template. USP1986094613102.
  23. Weisend ; Jr. Norbert A. (Cuyahoga Falls OH) Fahrner Alan J. (Canton OH) Hohenshil Robert N. (Doylestown OH). Pneumatic deicing distribution valve and system. USP1995025393014.
  24. Hohenshil Robert N. (Doylestown OH) Putt James C. (Doylestown OH). Pneumatic impulse valve and separation system. USP1993125271598.
  25. Breitbach Elmar J.,DEX ; Bein Thilo,DEX. Profile edge of an aerodynamic profile. USP2000066076776.
  26. Leffel Kevin L. (Akron OH) Putt James C. (Doylestown OH) Rauckhorst Richard L. (North Canton OH). Structural airfoil having integral expulsive system. USP1992035098037.
  27. Crosby ; Jr. ; Edward L.. Variable lift inflatable airfoil for tethered balloons. USP1978074102519.

이 특허를 인용한 특허 피인용횟수: 44

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya. Actuation device positioning systems and associated methods, including aircraft spoiler droop systems. USP2007127309043.
  2. Shepshelovich, Michael; Nagel, Alex; Abramov, Danny. Aerofoil accessories and method for modifying the geometry of a wing element. USP20181210144499.
  3. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  4. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  5. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  6. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  8. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  9. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  10. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  11. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  12. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2010057708231.
  13. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2013108567726.
  14. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2011108038103.
  15. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
  16. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2009017475854.
  17. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  18. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  19. Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J.. Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information. USP2012028121745.
  20. Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J.. Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information. USP2011088005582.
  21. Hamilton, Brian K.; Hassan, Ahmed; Birchette, Terrence S.; Murrill, Robert R.. Composite material for geometric morphing wing. USP2010097798443.
  22. Hamilton,Brian K.; Guymon,Stephen Lewis; Dockter,Gregory E.; Hassan,Ahmed A.. Fiber matrix for a geometric morphing wing. USP2007037195210.
  23. Dockter, Gregory E.; Hamilton, Brian K.. Geometric morphing wing with layers. USP2004096786457.
  24. Giamati, Michael John. Health monitoring pneumatic deicer. USP2017089738397.
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  27. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  28. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  29. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  30. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  31. Beyer,Kevin W.; Fox,Stephen J.; Lacy,Douglas S.; Meredith,Paul T.; Prow,Clayton A.; Sakurai,Seiya; Wells,Stephen L.. Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. USP2007087258308.
  32. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  33. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick. Multi-function trailing edge devices and associated methods. USP2007077243881.
  34. Sanderson, Terry M.; Eisentraut, Rudy A.; Hatfield, David B.. Reinforced inflatable wings for fitment-constrained air vehicles. USP2012018104713.
  35. Kordel, Jan A.; Sakurai, Seiya; Bowers, Bret A.; Glassmoyer, Christopher G.; Williams, Darren B.. Seal assemblies for use with drooped spoilers and other control surfaces on aircraft. USP2009117611099.
  36. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  37. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  38. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2008037338018.
  39. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
  40. Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
  41. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  42. Shepshelovich, Michael; Abramov, Danny. Two-element airfoil configured for minimizing accretion of contaminant. USP2014078763959.
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  44. Nagel, Alexander; Bauminger, Shlomo. Wing and devices therefor. USP2015069061752.