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Apparatus and method for aircraft wing stall control

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/50
출원번호 US-0415178 (1989-09-29)
발명자 / 주소
  • Bliesner Wayne T. (Snohomish WA) Wang Timothy (Bellevue WA) Stoner Ronald C. (Bellevue WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 53  인용 특허 : 0

초록

An aircraft swept wing which provides pitch stability during stall conditions. In a swept wing aircraft which has leading edge flaps which in their deployed position forms a slot between the slot and the leading edge portion of a fixed main wing structure, the configuration of said leading edge port

대표청구항

In a wing of an aircraft where the wing comprises: a. a main wing structure having a leading edge portion, a trailing edge portion, an upper aerodynamic surface, a lower aerodynamic surface, and a forward gap forming surface portion which extends along the leading edge; b. a leading edge member whic

이 특허를 인용한 특허 (53)

  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. Wolfgang Gleine DE; Knut Mau DE; Udo Carl DE, Aerodynamic noise reducing structure for aircraft wing slats.
  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. Peter May DE, Aircraft airfoil with close-mounted engine and leading edge high lift system.
  8. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  9. Couffignal, Jean-Pierre; Vinches, Frederic, Aircraft horizontal stabilizer.
  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. 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.
  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.; 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.
  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.
  16. Dodd, Daniel; Cathelain, Francois, Aircraft wing.
  17. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  18. Arata,Allen A.; Graham,David H., Aircraft with articulated leading edge of fuselage and wings.
  19. Arata,Allen A., Aircraft with extendable leading edge of fuselage and wings.
  20. Arata,Allen A., Aircraft with rotatable leading edge of fuselage and wings.
  21. Pachikara, Abraham J.; Moser, Matthew A.; Carpenter, Paul H.; Finn, Michael R.; Koch, Thomas S.; Bieniawski, Stefan R.; Whitehead, Brian T., Closed loop control of aircraft control surfaces.
  22. Moser, Matthew A.; Finn, Michael R.; Thoreen, Adam, Control interface for leading and trailing edge devices.
  23. Ferrari, Marcello do Areal Souto, Devices and methods to improve wing aerodynamics at low airspeeds.
  24. Mau, Knut; Dobrzynski, Werner, Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing.
  25. Reckzeh, Daniel; Schindler, Klaus, High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap.
  26. Whitehouse, Ian Roy; Kay, Edmund; Dodd, Daniel, High-lift device for an aircraft.
  27. Moser, Matthew A.; Liu, Benjamin M.; Finn, Michael R., Leading and trailing edge device deflections during descent of an aircraft.
  28. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  29. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  30. Dunavan, Marcus A., Leading edge snag for exposed propeller engine installation.
  31. Moser, Matthew A.; Finn, Michael R.; Park, Duk; Konings, Christopher A., Leading edge system and method for approach noise reduction.
  32. Moser, Matthew A.; Gardner, Mark J.; Finn, Michael R.; Good, Mark S.; Malachowski, Adam P.; Thommen, Monica E.; Amorosi, Stephen R.; Onu, Dan, Leading edge variable camber system and method.
  33. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  34. 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.
  35. 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.
  36. Moser, Matthew A.; Finn, Michael R.; Liu, Benjamin M., Optimized flap positioning for go-around operations.
  37. Dennison, William D.; May, Carl A., Removable horizontal stabilizer for helicopter.
  38. Lawrence, James Randolph, Rolling vortex wing slat system and method of use.
  39. Eisenberg, Drew, Secondary airfoil mounted on stall fence on wind turbine blade.
  40. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  41. Wollaston, Timothy David; Ribeiro, James Michael, Slat assembly.
  42. Havar, Tamas; Meyer, Oliver; Roth, York C.; Seack, Oliver, Slats with a flexible trailing edge.
  43. Chan, Andre S.; Hendriks, Ferdinand; Takemori, Keiichi, System and apparatus for mass-balanced spoiler in disk storage devices.
  44. Lorkowski, Thomas; Grohmann, Boris, System for reducing aerodynamic noise at a supplementary wing of an aircraft.
  45. Lorkowski, Thomas; Grohmann, Boris, System for reducing aerodynamic noise at a supplementary wing of an aircraft.
  46. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  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.
  48. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  49. Wayne T. Bliesner, Tailored wing assembly for an aircraft moveable slat system.
  50. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  51. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Good, Mark S.; Jones, Sarah A., Variable camber flap system and method.
  52. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  53. Hinkleman Michael J., Wing leading edge flap and method therefor.
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