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Lockable free wing aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/38
출원번호 US-0795329 (1991-11-20)
발명자 / 주소
  • Schmittle Hugh (605 Carolyn Rd. Glen Burnie MD 21061)
인용정보 피인용 횟수 : 37  인용 특허 : 0

초록

The aircraft includes a free wing freely pivotally supported about a spanwise axis for flight in a free wing mode and lockable in selected predetermined, fixed angles of incidence with respect to a fuselage for flight in a fixed wing mode. The predetermined angle of incidence in the fixed wing fligh

대표청구항

An aircraft comprising: a fuselage; a wing having an aerodynamic center and connected to said fuselage for free pivotal movement about a spanwise axis forwardly of said aerodynamic center thereby establishing a free wing mode of aircraft operation; and means for selectively locking said wing at a su

이 특허를 인용한 특허 (37)

  1. Rutan Elbert L. ; Chevallier Christophe, Active feedback loop to control body pitch in STOL/VTOL free wing aircraft.
  2. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  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. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  8. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  9. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  10. 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.
  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.; 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.
  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. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  15. Parks, Robert, Ducted spinner for engine cooling.
  16. Zha, Gecheng, Fluid systems that include a co-flow jet.
  17. Zha, Gecheng, Fluid systems that include a co-flow jet.
  18. Parks,Robert, Inbound transition control for a tail-sitting vertical take off and landing aircraft.
  19. Panatov Gennady Sergeevich,RUX ; Kravtsov Valentin Nikolaevich,RUX ; Konoplev Vladimir Nikolaevich,RUX, Lightamphibian.
  20. Bernhard Kreppold DE, Method, selector switch and selector device for securely sensing a selector switch position.
  21. Xi, Fengfeng; Finistauri, Allan Daniel; Moosavian, Amin, Morphing wing for an aircraft.
  22. 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.
  23. Reichert, Todd, Rotor-blown wing with passively tilting fuselage.
  24. Schmittle Hugh, STOL/VTOL free wing aircraft with improved shock dampening and absorbing means.
  25. Volk John Alan, Selectively rotatable and torsionally flexible aerodynamic control apparatus.
  26. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  27. Margaritoff Michael, Six seater twin engine aircraft.
  28. Parks,Robert, System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft.
  29. Parks,Robert; Led��,Jean Charles; Drela,Mark, System and method for controlling engine RPM of a ducted fan aircraft.
  30. Muren, Petter, System for controlling flight direction.
  31. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  32. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  33. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  34. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  35. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  36. Golshany, Sina Sam; Erickson, Todd W.; Tretow, Paul R.; Huntly, David M., Vibration dampening for horizontal stabilizers.
  37. Parks, Robert; Ledé, Jean-Charles, Vibration isolation engine mount system and method for ducted fans.
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