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특허 상세정보

Aeroelastic control flap

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/04   
미국특허분류(USC) 244/90R ; 244/214 ; 244/75R
출원번호 US-0453507 (1983-02-28)
발명자 / 주소
  • Borzachillo Angelo (San Marcos CA)
출원인 / 주소
  • Northrop Corporation (Hawthorne CA 02)
인용정보 피인용 횟수 : 47  인용 특허 : 0
초록

Auxiliary aeroelastic control flaps arranged on the leading edge of an aircraft\s wings at or near the wing tips and ahead of the ailerons for actuation under control of the pilot. The aeroelastic control flaps operate with the ailerons to induce supplementary aerodynamic force to augment the effectiveness of lateral and directional control during high stress manuevers at high dynamic pressures, but do not rely on wing sensors such as accelerometers coupled with a computer for automatic operation.

대표
청구항

A fighter airplane having a fuselage and wings supported and extending from the fuselage, said wings having leading and trailing edges, said fighter airplane designed for high dynamic pressure producing flight maneuvers, the improvement comprising, in combination, outboard ailerons mounted at the trailing edges of the wings at or near the wing tips for movement up or down with respect to the wing under the control of the pilot, control means operable by the pilot to move said ailerons, outboard aeroelastic control flaps mounted on the leading edge of the...

이 특허를 인용한 특허 (47)

  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. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  3. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  4. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  5. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  6. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  8. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  9. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  10. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  11. 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.
  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.; 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.
  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. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  16. Arata,Allen A.; Graham,David H., Aircraft with articulated leading edge of fuselage and wings.
  17. Arata,Allen A., Aircraft with extendable leading edge of fuselage and wings.
  18. Clark,Walter Dennis, Aircraft with forward opening inlay spoilers for yaw control.
  19. Arata,Allen A., Aircraft with rotatable leading edge of fuselage and wings.
  20. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  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. Volk, John A., Control system for alleviating a gust load on an aircraft wing.
  24. Appa Kari, Extendible leading edge flap.
  25. McCormick, Patrick J.; Huynh, Neal V.; Overton, Timothy G.; Marx, Alan, Hydraulic system and method for an aircraft flight control system.
  26. Bowcutt, Kevin G., Hypersonic waverider variable leading edge flaps.
  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. Moser, Matthew A.; Finn, Michael R.; Park, Duk; Konings, Christopher A., Leading edge system and method for approach noise reduction.
  31. 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.
  32. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  33. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  34. 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.
  35. Becker, Juergen, Process for designing flight controllers.
  36. 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.
  37. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  38. Clark, Walter D., System and method for controlling an aircraft.
  39. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Murphy, Robert M.; Thoreen, Adam, System and method for optimizing performance of an aircraft.
  40. Moser, Matthew A.; Leopold, David D.; Finn, Michael R., System and method for reducing the stopping distance of an aircraft.
  41. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  42. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  43. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  44. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  45. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  46. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Good, Mark S.; Jones, Sarah A., Variable camber flap system and method.
  47. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.