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Variable camber airfoil

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/48
출원번호 US-0455837 (1974-03-28)
발명자 / 주소
  • Cole James B. (Mercer Island WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 55  인용 특허 : 0

초록

A variable camber apparatus for the leading and/or trailing edge of an airfoil that is operable for lift variation at high airspeeds of a jet aircraft such as for maneuvering of fighter aircraft. The cambering apparatus comprises an upper surface flexible skin panel which is supported along its inne

대표청구항

A variable camber airfoil comprising: an aerodynamically continuous upper surface of the airfoil connected at its inner-end to fixed structure of the airfoil; a rib member fixedly hinged at its inner-end to fixed structure of the airfoil for rotation in a chordwise plane and having its free-end exte

이 특허를 인용한 특허 (55)

  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. Breidenbach, Thomas Scott, Aerodynamic drag reducing apparatus.
  3. Breidenbach, Thomas Scott, Aerodynamic drag reducing apparatus.
  4. Breidenbach, Thomas Scott, Aerodynamic drag reducing apparatus.
  5. Breidenbach, Thomas Scott, Aerodynamic drag reducing apparatus.
  6. Breidenbach, Thomas Scott, Aerodynamic drag reducing apparatus.
  7. Smith, Andrew F.; Niemiec, Jared A.; Hinricher, Court S.; Polidori, Michael W.; Grossmann, Jeffrey J., Aerodynamic structures secured to the underbody of cargo bodies.
  8. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  9. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  10. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  11. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  12. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  13. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  14. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  15. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  16. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  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.
  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.
  19. 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.
  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.
  21. 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.
  22. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  23. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  24. Rawdon, Blaine K.; Harber, Benjamin A.; Harrison, Neal A., Dual-rib morphing leading edge.
  25. Umlauft, Sebastian; Wenzel, Henryk, Fastening arrangement for fastening a component on a fuselage.
  26. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  27. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  28. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  29. Beyer, Kevin W.; Sakurai, Seiya, Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods.
  30. 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.
  31. 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.
  32. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  33. Grip, Robert E.; Brown, John J.; Harrison, Neal A.; Rawdon, Blaine K.; Vassberg, John C., Morphing airfoil leading edge.
  34. Gordon, Jason; Borgstrom, Carl; Fisher, Noah; Fuhrmeister, Cory; Madigan, Nathan; Parkins, Carly, Morphing wing leading edge.
  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. Smith, Andrew F.; Horrell, Charles M.; Grossmann, Jeffrey J., Rear-mounted aerodynamic structure for truck cargo bodies.
  37. Smith, Andrew F.; Horrell, Charles M.; Grossmann, Jeffrey J.; Feldman, Jonathan R.; Bruccoleri, Alexander R., Rear-mounted aerodynamic structure for truck cargo bodies.
  38. Smith, Andrew F.; Grossmann, Jeffrey J.; Hinricher, Court S.; Cholnoky, Robert R.; Duncanson, Austin A., Rear-mounted aerodynamic structures for cargo bodies.
  39. Smith, Andrew F.; Niemiec, Jared A.; Grossmann, Jeffrey J.; Cholnoky, Robert R.; Polidori, Michael W.; Dickinson, Barrie J., Rear-mounted retractable aerodynamic structure for cargo bodies.
  40. Smith, Andrew F.; Pagliarella, Riccardo M.; Hinricher, Court S.; Grossmann, Jeffrey J.; Niemiec, Jared A.; Polidori, Michael W., Retractable aerodynamic structures for cargo bodies and methods of controlling positioning of the same.
  41. 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.
  42. Grip, Robert Erik; Rawdon, Blaine Knight, Segmented aircraft wing having solar arrays.
  43. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  44. Arata Allen A., Single surface independent aircraft control.
  45. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  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. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  48. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  49. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  50. Seiya Sakurai ; Stephen John Fox, Variable camber leading edge for an airfoil.
  51. McKinney Maurice E. (Bellevue WA) Rudolph Peter K. C. (Seattle WA), Variable camber leading edge mechanism with Krueger flap.
  52. Zapel ; Edwin J., Variable camber trailing edge for airfoil.
  53. Cole, James B., Variable-camber airfoil.
  54. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  55. Lewis George E. (Renton WA) Thomasson Robert E. (Seattle WA) Nelson David W. (Redmond WA), Wing lift/drag optimizing system.
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