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Three-position variable camber Krueger leading edge flap

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/50
출원번호 US-0782525 (1991-10-24)
발명자 / 주소
  • Sakurai Seiya (Seattle WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 59  인용 특허 : 0

초록

A variable camber flap assembly having first and second operative positions. A rotatable drive arm powers first and second linkage subassemblies. The first linkage subassembly extends the flap panel in a downward and forward direction to its operative positions, and also rotates a hinged bullnose ou

대표청구항

A linkage mechanism for extending a flap from a stowed position within the undersurface of an airfoil to a forward extended operative position, said linkage mechanism comprising: a first linkage subassembly comprising: a first drive arm portion mounted to fixed structure of said airfoil for rotation

이 특허를 인용한 특허 (59)

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  2. Johnson, Patterson; Sakurai, Seiya; Santini, Gregory M.; Konings, Christopher A.; Clark, Adam M., Actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps.
  3. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  4. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  5. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  6. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  8. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  9. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  10. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  11. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  12. Morgenstern, John M.; Arslan, Alan, Aircraft lift device for low sonic boom.
  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.
  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.
  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.
  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.
  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.
  18. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  19. Giamati, Michael J., Aircraft wing with electrothermal deicing and/or anti-icing device.
  20. Giamati,Michael J., Aircraft wing with electrothermal deicing and/or anti-icing device.
  21. Clark,Walter Dennis, Aircraft with forward opening inlay spoilers for yaw control.
  22. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  23. Hoffenberg, Robert, Compound leading edge device for aircraft.
  24. Holert, Ben, Drive and guide arrangement for a flap which is arranged on an aircraft mainplane.
  25. Rawdon, Blaine K.; Harber, Benjamin A.; Harrison, Neal A., Dual-rib morphing leading edge.
  26. Schröder, Karsten, High lift system for an aircraft.
  27. Hue, Xavier; Schlipf, Bernhard, High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft.
  28. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H., High-positioned 2-position variable camber Krueger.
  29. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H., High-positioned 2-position variable camber Krueger.
  30. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor; Charles, Kara Marie, High-positioned 3-position variable camber krueger.
  31. Brown, James; Kay, Edmund, Krueger.
  32. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  33. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  34. Jaggard, Philip Robert, Leading edge structure for an aerofoil.
  35. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  36. Beyer, Kevin W.; Sakurai, Seiya, Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods.
  37. 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.
  38. Beyer, Kevin W.; Fox, Stephen J.; Lacy, Douglas S.; Sakurai, Seiya, Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface.
  39. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  40. Grip, Robert E.; Brown, John J.; Harrison, Neal A.; Rawdon, Blaine K.; Vassberg, John C., Morphing airfoil leading edge.
  41. Gordon, Jason; Borgstrom, Carl; Fisher, Noah; Fuhrmeister, Cory; Madigan, Nathan; Parkins, Carly, Morphing wing leading edge.
  42. 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.
  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.
  44. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  45. Wollaston, Timothy David; Ribeiro, James Michael, Slat assembly.
  46. Mann, Alan, Slat deployment mechanism.
  47. Jaggard, Philip R.; West, Robert H., Slat support funk plate.
  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.
  49. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  50. Schlipf, Bernhard; Weiss, Tayson William, Systems and methods for load introduction element for a movable surface of an aircraft.
  51. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  52. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  53. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  54. Rey, Nancy M.; Miller, Robin Mihekun; Tillman, Thomas G.; Rukus, Robert M.; Kettle, John L., Variable area nozzle for gas turbine engines driven by shape memory alloy actuators.
  55. Seiya Sakurai ; Stephen John Fox, Variable camber leading edge for an airfoil.
  56. Kahara Bryan D. ; Priestley Richard T. ; Seho Kenneth E., Variable displacement fuel tank for aircraft.
  57. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  58. Schlipf, Bernhard; Triebl, Carsten, Wing assembly with a main wing and movable high-lift body and a method for adjusting a high-lift body relative to a main wing.
  59. Hinkleman Michael J., Wing leading edge flap and method therefor.
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