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Variable camber wing mechanism

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214 ; 244/219
출원번호 US-0973260 (1997-12-02)
우선권정보 GB-0021194 (1996-10-11)
국제출원번호 PCT/GB97/00979 (1997-04-09)
§371/§102 date 19971202 (19971202)
국제공개번호 WO-9738900 (1997-10-23)
발명자 / 주소
대리인 / 주소
    Schindler
인용정보 피인용 횟수 : 46  인용 특허 : 3
초록

The present invention relates to a variable camber wing mechanism. The mechanism includes a main wing, a slat member connected by swing arm members to the main wing, slots in the leading edge of the main wing for the swing arms to pass through, and a shutter member for sealing the slot around each swing arm member by means of a sliding movement parallel to the leading edge. This sealing of the slots prevents ingress of ice and water into the main wing.

대표
청구항
▼

[ I claim:] [1.] A variable camber wing mechanism, comprising:a main wing section having a leading edge;a slat member connected by at least two swing arm members to said main wing section, each of said swing arm members being pivotally connected to said main wing section at a first end thereof and connected to said slat member at a second end thereof, and passing through a slot in the leading edge of said main wing section and arranged for pivotal movement along the length of the slot; and,a shutter member for sealing the slot around each of said swing a...

이 특허에 인용된 특허 (3)

  1. Day Roger A. (Bristol GB2). Device for closing and opening in the leading edge of a wing. USP1989114880189.
  2. Williams Anthony J. (Filton GBX). Flexible closing device for a wing leading edge. USP1991095044580.
  3. Brown Robert B. (Kent WA). Wing leading edge slat. USP1982114360176.

이 특허를 인용한 특허 피인용횟수: 46

  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. Morgenstern, John M.; Arslan, Alan. Aircraft lift device for low sonic boom. USP2005086935592.
  13. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  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. USP2010057708231.
  15. 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.
  16. 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.
  17. 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.
  18. 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.
  19. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  20. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  21. Broadbent, Michael Craig. Contiguous variable camber device. USP2004016682023.
  22. Broadbent, Michael Craig. Deployment system for a moveable wing surface. USP2005126974112.
  23. Teague, Phillip Vincent. Electrical connector. USP2011027883337.
  24. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  25. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  26. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  27. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  28. Ding, Huifeng; Wu, Jiaju; Wu, Yubin; Zhu, Yi; Tang, Minjie; Huang, Zhiping; Chen, Lei; Yuan, Jiang. Method for detecting the landing quality of an aircraft. USP2015059026280.
  29. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  30. 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.
  31. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP2016039297264.
  32. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP20190110190572.
  33. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP2013128608441.
  34. 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.
  35. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  36. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  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. Wayne T. Bliesner. Tailored wing assembly for an aircraft moveable slat system. USP2002086435458.
  42. Brakes, David. Track container. USP20190110179641.
  43. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  44. Coughlin, Ray F.. Translating flap drive door. USP2010067744034.
  45. Shepshelovich, Michael; Abramov, Danny. Two-element airfoil configured for minimizing accretion of contaminant. USP2014078763959.
  46. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.

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