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특허 상세정보

Wing leading edge flap and method therefor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44    B64C-009/22    B64C-013/16   
미국특허분류(USC) 244/203 ; 244/214 ; 244/219 ; 244/076A ; 244/076B
출원번호 US-0673675 (1996-06-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sproule
인용정보 피인용 횟수 : 56  인용 특허 : 17
초록

A leading edge flap system for an airplane includes a flap which is rotated about a single hinge point between (i) a retracted position, (ii) an intermediate extended position for high speed maneuvering, and (iii) a fully extended position for low speed maneuvering. In the high speed intermediate position, there is no slot between the flap and the wing leading edge. This position provides additional lift to improve the airplane's turning performance. On the other hand, in the low speed fully extended position, the flap is rotated a greater amount than in...

대표
청구항

[ What is claimed is:] [1.] A leading edge flap system for a wing, the flap system comprising:a. a wing leading edge having an upper corner surface and a lower nose surface;b. a flap having an upper trailing edge and a lower trailing edge that has a rearward extending portion with a rearward dimension;c. means, connected to the wing, for supporting the flap from the wing leading edge in a manner that the flap is allowed to rotate relative to the wing leading edge;d. means, connected to the wing, for rotating the flap relative to the wing leading edge bet...

이 특허에 인용된 특허 (17)

  1. Bliesner Wayne T. (Snohomish WA) Wang Timothy (Bellevue WA) Stoner Ronald C. (Bellevue WA). Apparatus and method for aircraft wing stall control. USP1991105056741.
  2. Johnson Edward N. (King County WA) Puncoch Miloslav (King County WA). Apparatus for supporting an aircraft guide track for a movable airfoil. USP1987084687162.
  3. Cole James B. (King County WA). Biased leading edge slat apparatus. USP1988064753402.
  4. Anderson Leonard R. (Phoenix AZ) DeCamp Ronald W. (Dayton OH). Camber control system. USP1988054741503.
  5. Pace James W. (Mercer Island WA). Closing device for an airfoil. USP1987024640477.
  6. Day Roger A. (Bristol GB2). Device for closing and opening in the leading edge of a wing. USP1989114880189.
  7. Clifford-Jones John B. (Hatfield GB2). Leading edge arrangements for aircraft wings. USP1986044585192.
  8. Bliesner Wayne T. (Snohomish WA). Leading edge slat/wing combination. USP1996085544847.
  9. Middleton Wilbur D. (Bellevue WA) Paulson John A. (Bellevue WA). Leading edge vortex flap for wings. USP1981104293110.
  10. Ellmers Wilfried (Achim DEX) Martens Wilhelm (Delmenhorst DEX). Slat actuation and steering. USP1990044915327.
  11. Sakurai Seiya (Seattle WA). Three-position variable camber Krueger leading edge flap. USP1992105158252.
  12. Cole James B. (Mercer Island WA). Variable camber flap. USP1979064159089.
  13. Wang Timothy (Bellevue WA). Variable camber leading edge flap. USP1980024189120.
  14. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
  15. Lewis Delbert S. (Bellevue WA). Wing leading edge high lift device. USP1981084285482.
  16. Brown Robert B. (Kent WA). Wing leading edge slat. USP1982114360176.
  17. Lewis George E. (Renton WA) Thomasson Robert E. (Seattle WA) Nelson David W. (Redmond WA). Wing lift/drag optimizing system. USP1990024899284.

이 특허를 인용한 특허 피인용횟수: 56

  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. Cathelain, Francois; Kay, Edmund. Actuation system for leading edge high-lift device. USP2015038967549.
  3. Shaheen, Milad A.; Dreher, Robert V.. Actuator for aircraft stabilizers with a failure responsive lock control mechanism. USP2004016672540.
  4. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  5. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  6. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  7. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  8. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  9. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  10. Jones,Kelly T.. Aircraft control surface drive system and associated methods. USP2009037506842.
  11. Rampton,Scott N.; Amorosi,Stephen R.. Aircraft leading edge apparatuses and corresponding methods. USP2007097270305.
  12. Lacy,Douglas S.; Wyatt,Greg H.. Aircraft leading edge device systems and corresponding sizing methods. USP2008047357358.
  13. Morgenstern, John M.; Arslan, Alan. Aircraft lift device for low sonic boom. USP2005086935592.
  14. Peirce, Robert James. Aircraft slat assembly. USP2013078474762.
  15. 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.
  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. USP2010057708231.
  17. 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.
  18. 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.
  19. 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.
  20. 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.
  21. Collett Edward,GBX. Aircraft wing leading edge high lift device with suction. USP2000106135395.
  22. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  23. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  24. Werner Dobrzynski DE; Burkhard Gehlhar DE. Auxiliary airfoil for aircraft main wings. USP2002106457680.
  25. Hoffenberg, Robert. Compound leading edge device for aircraft. USP2014018622350.
  26. Broadbent, Michael Craig. Contiguous variable camber device. USP2004016682023.
  27. Moser, Matthew A.; Finn, Michael R.; Thoreen, Adam. Control interface for leading and trailing edge devices. USP2017059656741.
  28. Whitehouse, Ian Roy; Kay, Edmund; Dodd, Daniel. High-lift device for an aircraft. USP2012038128038.
  29. Hirai, Makoto; Maeda, Ichiro. High-lift device, wing, and noise reduction structure for high-lift device. USP2015049010692.
  30. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  31. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  32. Moser, Matthew A.; Finn, Michael R.; Park, Duk; Konings, Christopher A.. Leading edge system and method for approach noise reduction. USP2017099771141.
  33. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  34. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  35. Pitt, Dale M.; Eckstein, Nicholas Stephen. Method and apparatus for a leading edge slat on a wing of an aircraft. USP2013098534610.
  36. Pitt, Dale M.; Eckstein, Nicholas Stephen. Method for a leading edge slat on a wing of an aircraft. USP2016099446836.
  37. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  38. Pitt, Dale M.; Eckstein, Nicholas Stephen. Moveable leading edge device for a wing. USP2013098534611.
  39. 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.
  40. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP2016039297264.
  41. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP20190110190572.
  42. Hotto, Robert. Rotatable blade apparatus with individually adjustable blades. USP2013128608441.
  43. 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.
  44. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  45. Jaggard, Philip R.; West, Robert H.. Slat support funk plate. USP2012058181913.
  46. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  47. 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.
  48. 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.
  49. 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.
  50. Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
  51. Wayne T. Bliesner. Tailored wing assembly for an aircraft moveable slat system. USP2002086435458.
  52. Brakes, David. Track container. USP20190110179641.
  53. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  54. Grove, Darren V.. Transonic flow shockwave position stabilizer. USP2003026513754.
  55. Cunningham ; Jr. Atlee Marion. Trapped vortex airfoil nose. USP2000126161802.
  56. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.