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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Aircraft thrust vectoring system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/78   
미국특허분류(USC) 239/01 ; 239/265.23
출원번호 US-0433675 (1995-05-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Woodard, Emhardt, Naughton, Moriarty & McNett
인용정보 피인용 횟수 : 63  인용 특허 : 11
초록
▼

A thrust vectoring system comprising a working fluid source mounted to an aircraft, and a vectoring nozzle connected to the working fluid source which has an extendable conduit defining a passage from an inlet to an outlet. The passage is adjustable so that the direction of the working fluid exiting the outlet is different than the working fluid entering the inlet when the conduit of the vectoring nozzle is extended. This conduit provides a way to change the direction of working fluid exiting the nozzle and correspondingly change the thrust vector of the...

대표
청구항
▼

[ What is claimed is:] [65.] A combination, comprising:an aircraft;a working fluid source mounted to said aircraft;an extendable conduit defining a passage from an inlet to an outlet, said inlet being connected to said working fluid source, said conduit being adjustably extendable to controllably vary direction of working fluid exiting said outlet, said passage being generally straight when said conduit is unextended; andat least three guide vanes mounted across said outlet, said vanes being selectively pivotable to controllably direct working fluid exit...

이 특허에 인용된 특허 (11)

  1. Madden William M. (Palm Springs FL). Area two-dimensional converging/diverging nozzle. USP1986054587806.
  2. Thayer Edward B. (Jupiter FL) Stevens Herman L. (West Palm Beach FL). Control vent for diverting exhaust nozzle. USP1989024805401.
  3. Nash Dudley O. (Forest Park OH) Beavers Robert G. (Mason OH) Burge Joseph C. (Cincinnati OH) Castells Onofre T. M. (Sharonville OH) Parker Alan I. (Cincinnati OH). Flight maneuverable nozzle for gas turbine engines. USP1977014000610.
  4. Ohmori Takashi (Hitachi JPX) Sato Isao (Hitachi JPX) Ishibashi Yoji (Hitachi JPX) Minakawa Yoshimitsu (Hitachi JPX) Kuroda Michio (Hitachi JPX) Tamura Zensuke (Hitachi JPX). Premixing swirling burner. USP1986054587809.
  5. Bevilaqua Paul M. (Santa Clarita CA) Shumpert Paul K. (Valencia CA). Propulsion system for a vertical and short takeoff and landing aircraft. USP1993055209428.
  6. Musgrove Robert G. (Arlington TX). Tandem fan series flow VSTOL propulsion system. USP1984104474345.
  7. Brown Robert B. (Renton WA). Thrust reversing system for high bypass fan engines. USP1990054922711.
  8. Brown Robert B. (Renton WA). Thrust reversing system for high bypass fan engines. USP1992095142862.
  9. Scrace Harold A. (Bristol GB2). Vectorable exhaust nozzle for gas turbine engines. USP1987044660767.
  10. Wooten ; Jr. William H. (Evendale OH) Speir Donald W. (Cincinnati OH). Vectorable nozzle. USP1981074280660.
  11. Herrick Paul W. (Jupiter FL) Thayer Edward B. (Jupiter FL) Stewart Jim D. (Jupiter FL). Yaw and pitch convergent-divergent thrust vectoring nozzle. USP1989064836451.

이 특허를 인용한 특허 피인용횟수: 63

  1. Goelet, John. Airship having a cargo compartment. USP2017119828082.
  2. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian. Annular turbine ring rotor. USP2014038672630.
  3. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian. Annular turbine ring rotor. USP2012048152469.
  4. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian. Axial compressor for tip turbine engine. USP2010127845157.
  5. Nordeen, Craig A.; Suciu, Gabriel L.. Balanced turbine rotor fan blade for a tip turbine engine. USP2014088807936.
  6. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian. Cantilevered tip turbine engine. USP2011108033094.
  7. Suciu, Gabriel L.; Nordeen, Craig A.; Kramer, Stephen. Combustor for turbine engine. USP2011098024931.
  8. Merry, Brian; Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Counter-rotating compressor case and assembly method for tip turbine engine. USP2011118061968.
  9. Suciu, Gabriel; Merry, Brian; McCune, Michael E.. Counter-rotating gearbox for tip turbine engine. USP2015028950171.
  10. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Diffuser aspiration for a tip turbine engine. USP2013068468795.
  11. Suciu, Gabriel L.; Roberge, Gary D.. Ejector cooling of outer case for tip turbine engine. USP2011077980054.
  12. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian. Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine. USP2011027887296.
  13. Otto, Paul Robert. Flight control system using thrust devices. USP2013028376268.
  14. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  15. Lemelson Jerome H. ; Pedersen Robert D. ; Blake Tracy D.. Fuzzy logic based emergency flight control with thrust vectoring. USP2001076259976.
  16. Lemelson, Jerome H.; Lemelson, Dorothy; Pedersen, Robert D.; Blake, Tracy D.. Fuzzy logic based emergency flight control with thrust vectoring capability. USP2003126662086.
  17. Migliaro, Jr., Edward F.. Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle. USP2013028365515.
  18. Nordeen, Craig A.; Norris, James W.. Individual inlet guide vane control for tip turbine engine. USP2015038967945.
  19. Suciu, Gabriel L.; Portlock, Lawrence E.; Merry, Brian. Inflatable bleed valve for a turbine engine. USP2011077976272.
  20. Dierksmeier, Douglas David. Lift fan flow path device. USP2012128336806.
  21. Pesyna, Kenneth M.; Henkle, Jeffrey P.. Mechanism for a vectoring exhaust nozzle. USP2010117836681.
  22. Pesyna, Kenneth M.; Henkle, Jeffrey P.. Mechanism for a vectoring exhaust nozzle. USP2012088245495.
  23. Cousino, Sr., Dennis James. Method and apparatus for boosting gas turbine engine performance. USP2013128616005.
  24. Stephan, Volker. Method for the control of aero gas turbine engines. USP2004036712314.
  25. Elsberg Laura Linda ; Pozniak Jennifer Elizabeth. Method of making prefastened disposable absorbent articles. USP2000026022432.
  26. Suciu, Gabriel L.; Merry, Brian. Modular tip turbine engine. USP2009127631480.
  27. Baker, Von David; Vittal, Baily Ramachandra. Nozzle with an adjustable throat. USP2010097793504.
  28. Baker, Von David; Vittal, Baily Ramachandra. Nozzle with an adjustable throat. USP2014078769959.
  29. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian. Particle separator for tip turbine engine. USP2015049003759.
  30. Norris, James W.; Nordeen, Craig A.. Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method. USP2014028641367.
  31. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Regenerative turbine blade and vane cooling for a tip turbine engine. USP2009107607286.
  32. Roberts, Steven D.; Damgaard, Jocelyn Charis. Retainer for suspended thermal protection elements in a gas turbine engine. USP2013118572986.
  33. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian. Seal assembly for a fan rotor of a tip turbine engine. USP2011027883315.
  34. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian. Seal assembly for a fan-turbine rotor of a tip turbine engine. USP2011027883314.
  35. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian. Stacked annular components for turbine engines. USP2012018087885.
  36. Merry, Brian; Webb, Scot Adams; McCune, Michael. Starter generator system for a tip turbine engine. USP2011017874163.
  37. Sokhey, Jagdish; Kornegay, Brian. Techniques to reduce infrared detection of a gas turbine engine. USP2014078776527.
  38. Klingels, Hermann; Klaen, Stephan; Scherer, Christian; Vogel, Uwe. Thrust deflecting device and aircraft engine. USP2017059664141.
  39. Fujisawa, Fuminori; Tani, Hiroyuki; Hyuga, Daisuke. Thrust vectoring apparatus and flying object having thrust vectoring apparatus. USP2017059663222.
  40. David Levi Sutterfield ; Von David Baker ; Jagdish Singh Sokhey. Thrust vectoring mechanism. USP2002056382559.
  41. Ulanoski Michael S. ; Sokhey Jagdish S.. Thrust vectoring system. USP2000086105901.
  42. Ulanoski Michael S. ; Sokhey Jagdish S. ; Vittal Baily R. ; Baker Von D.. Thrust vectoring techniques. USP2001116318668.
  43. Norris, James W.; Nordeen, Craig A.. Tip turbine engine and operating method with reverse core airflow. USP2012018096753.
  44. Suciu, Gabriel L.; Norris, James W.; Merry, Brian. Tip turbine engine composite tailcone. USP2017129845727.
  45. Suciu, Gabriel L.; Merry, Brian; Portlock, Lawrence. Tip turbine engine comprising a nonrotable compartment. USP2014068757959.
  46. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Tip turbine engine comprising turbine blade clusters and method of assembly. USP2011017874802.
  47. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor. USP2011027878762.
  48. Suciu, Gabriel L.; Norris, James W.; Merry, Brian. Tip turbine engine integral case, vane, mount and mixer. USP2013028365511.
  49. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian. Tip turbine engine integral fan, combustor, and turbine case. USP2011108033092.
  50. Suciu, Gabriel L.; Merry, Brian. Tip turbine engine support structure. USP2011077976273.
  51. Suciu, Gabriel L.; Merry, Brian. Tip turbine engine with a heat exchanger. USP2009127631485.
  52. Norris, James W.; Nordeen, Craig A.; Roberge, Gary. Tip turbine engine with multiple fan and turbine stages. USP2012018104257.
  53. Norris, James W.; Nordeen, Craig A.. Tip turbine engine with reverse core airflow. USP2017019541092.
  54. Suciu, Gabriel L.; Norris, James W.; Merry, Brian. Tip turbine single plane mount. USP2015089109537.
  55. Roberge, Gary D.. Turbine blow down starter for turbine engine. USP2011027882695.
  56. Suciu, Gabriel L.; Pagluica, Gino J.; Duong, Loc Quang; Portlock, Lawrence E.. Turbine engine with differential gear driven fan and compressor. USP2013108561383.
  57. Windisch, D. Anthony. VTOL propulsion for aircraft. USP2015028960592.
  58. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J.. Variable fan inlet guide vane assembly for gas turbine engine. USP2011027882694.
  59. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J.. Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method. USP2012108276362.
  60. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J.. Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method. USP2015049003768.
  61. Roberge, Gary D.. Vectoring transition duct for turbine engine. USP2010127854112.
  62. Dickau, John Eugene. Vertical takeoff and landing aircraft propulsion systems. USP2005076918244.
  63. Devine, Michael Thomas. Vertical/short take-off and landing aircraft. USP2003056561456.

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