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특허 상세정보

Aircraft wing provided with a high-lift system in its leading edge

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/04    B64C-003/50   
미국특허분류(USC) 244/207; 244/130; 244/214; 244/218
출원번호 US-0309233 (1981-10-07)
우선권정보 FR-0022154 (1980-10-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Merriam, Marshall & Bicknell
인용정보 피인용 횟수 : 45  인용 특허 : 2
초록

The invention relates to aircraft wings, wherein the fairing element between the leading edge of a wing and the fuselage comprises a streamlining flap movable between a folded position in which it is housed in a recess in the fairing element and forms a part of the leading edge and the part adjacent the lower surface of said fairing element, and an extended position in which it ensures continuity of the leading edge between the fuselage and the high-lift spoiler likewise in extended position. Moreover, there is a communication between the housing of the ...

대표
청구항

1. In an aircraft wing provided in its leading edge, with a high-lift system of which part is disposed in the vicinity of the join of said wing to the fuselage of the aircraft, but separated from said fuselage by a fairing element improving the air flow on the zone of connection of said wing when it is in smooth configuration, said system comprising at least one high-lift spoiler movable between a folded position in which it is housed in a recess in the wing and forms part of the leading edge and the part adjacent the upper surface of said wing and an ex...

이 특허를 인용한 특허 피인용횟수: 45

  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. Voogt, Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2010057721999.
  3. Voogt,Nicolaas. Aerospace vehicle fairing systems and associated methods. USP2007117300021.
  4. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  5. Konings,Christopher A.. Aerospace vehicle leading edge slat devices and corresponding methods. USP2008017322547.
  6. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  8. Peter May DE. Aircraft airfoil with close-mounted engine and leading edge high lift system. USP2002046364254.
  9. Fol, Thierry; Jimenez, Philippe; Namer, Arnaud. Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations. USP2012058177170.
  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. 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. Dodd, Daniel; Cathelain, Francois. Aircraft wing. USP2013018353483.
  20. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  21. Arata,Allen A.; Graham,David H.. Aircraft with articulated leading edge of fuselage and wings. USP2007047204454.
  22. Arata,Allen A.. Aircraft with extendable leading edge of fuselage and wings. USP2007057216835.
  23. Arata,Allen A.. Aircraft with rotatable leading edge of fuselage and wings. USP2007077246770.
  24. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas. Airplane with unswept slotted cruise wing airfoil. USP201306RE44313.
  25. Kunz Rdiger (Munich DEX). Apparatus for closing an air gap between a flap and an aircraft. USP1984094471925.
  26. Flaig Axel,DEX ; Schwetzler Detlev,DEX ; Stache ; deceased Ulrich,DEXITX by Ronald Seiler ; legal representative. Apparatus for influencing a wing root airflow in an aircraft. USP2000116152404.
  27. Ferrari, Marcello do Areal Souto. Devices and methods to improve wing aerodynamics at low airspeeds. USP2012028118265.
  28. Wheaton, James M.; Amorosi, Stephen R.. Leading edge flap apparatuses and associated methods. USP2010117828250.
  29. Wheaton,James M.; Amorosi,Stephen R.. Leading edge flap apparatuses and associated methods. USP2007097264206.
  30. Fox, Stephen J.; Sakurai, Seiya. Link mechanisms for gapped rigid krueger flaps, and associated systems and methods. USP2009087578484.
  31. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  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. 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. 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.
  36. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  37. Kafyeke, Fassi; Langlois, Marc; Kho, Cedric. Slat configuration for fixed-wing aircraft. USP2014078789798.
  38. De Conto, Sébastien; Rival, Fabrice; Bernes, Romain; Coll, Frédéric. Supporting set for a wing flap system of an aircraft. USP2017059637220.
  39. 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.
  40. 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.
  41. 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.
  42. Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
  43. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
  44. Speer,Thomas E.. Vehicle control systems and corresponding sizing methods. USP2008097424350.
  45. Dees Paul W. ; Irish Michael J. ; Zierten Thomas A.. Wing flap seal bump. USP2000066073889.