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특허 상세정보

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Method of varying a fan duct nozzle throat area of a gas turbine engine

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B63H-011/00    F02K-003/02    F02K-001/00    B63H-011/10    A63F-013/30    G07F-017/32    H04M-001/725    H04M-001/02   
미국특허분류(USC) 060/204; 060/226.1; 060/771; 239/265.19
출원번호 US-0360658 (2012-01-27)
등록번호 US-8959889 (2015-02-24)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 2  인용 특허 : 80
초록

A method of varying a fan duct nozzle throat area of a gas turbine engine includes pivoting a fan nozzle outwardly relative to a longitudinal axis of the gas turbine engine. The fan nozzle is configured to move axially non-contemporaneously with the pivoting of the fan nozzle.

대표
청구항
▼

1. A method of varying a fan duct nozzle throat area of a gas turbine engine having a longitudinal axis and a fan nozzle capable of pivoting and moving axially independent of the pivoting of the fan nozzle, comprising the steps of: pivoting the fan nozzle outwardly about a pivot axis oriented transversely relative to the longitudinal axis; andvarying the fan duct nozzle throat area when pivoting the fan nozzle about the pivot axis. 2. The method of claim 1 further comprising the step of: pivoting the fan nozzle outwardly and inwardly between stowed and d...

이 특허에 인용된 특허 (80)

  1. Fernz James A. (Wichita KS). Actuation system for a blocker door in a jet engine nacelle. USP1990034909442.
  2. Lair Jean-Pierre. Adjustable fairing for thrust reversers. USP1998035730392.
  3. Rudolph Peter K. C.. Aircraft chute ejector nozzle. USP1999065908159.
  4. Rudolph Peter K. C.. Aircraft scoop ejector nozzle. USP1998105826794.
  5. Szupkay Imre A.. Aircraft thrust reverser system with linearly translating inner and outer doors. USP1998085794434.
  6. Sternberger, Joe; Lallement, Michael K.. Apparatus and method for mounting a cascade support ring to a thrust reverser. USP2004116824101.
  7. Sternberger, Joe; Lallement, Michael K.. Apparatus and method for mounting a cascade support ring to a thrust reverser. USP2005076915984.
  8. Dorris ; III John ; Smith David Michael ; Parekh David Espineli ; Kibens Valdis. Apparatus and methods for active flow control of a nozzle exhaust plume. USP2001106308898.
  9. Vieth Gary L. (Bellevue WA). Apparatus for influencing the flow of air through a passageway. USP1992035097662.
  10. Hapke Donald William (Issaquah WA). Articulated nozzle for upper surface blown aircraft. USP1977064030687.
  11. Hardy Brant B. ; Sternberger Joe E. ; Hills Gregory S. ; Kraft Kurt R.. Automatic restow system for aircraft thrust reverser. USP2001096286784.
  12. Sternberger, Joe E.. Bi-fold thrust reverser door assembly. USP2004076764045.
  13. Luttgeharm Clint A. (Wichita KS) Todd Marty J. (Wichita KS) Welch John M. (Wichita KS). Cascade assembly for use in a thrust-reversing mechanism. USP1996045507143.
  14. Lair, Jean-Pierre. Confluent variable exhaust nozzle. USP2004066751944.
  15. Harner Kermit I. (Windsor CT) Schneider Roy W. (Ellington CT). Control system for variable pitch fan propulsor with reverse pitch. USP1976023936226.
  16. Chamay Anthony Joseph (Marblehead MA) Smith James (Topsfield MA) Hull ; Jr. Thomas Neil (Marblehead MA). Cowling arrangement for a turbofan engine. USP1976113988889.
  17. Madden William M. (Palm Springs FL). Exhaust nozzle coupled with reverser exhaust door. USP1987094690329.
  18. Roach Thomas A. (Palm Beach Gardens FL) Starke Roy R. (Lake Park FL). Exhaust nozzle with reverser exhaust door mechanism. USP1992035092525.
  19. Shine Paul R. (Bellevue WA). Flexible fire seal for overlapping cowl side edges. USP1992105156360.
  20. Birch, Nigel T; Webster, John R. Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators. USP2004116813877.
  21. Woodward Clifford S. (Bristol GB2). Gas turbine engine power plant. USP1982054327548.
  22. Vermilye Michael L. (Redmond WA). Hinge system for thrust reverser cowl. USP1987104697763.
  23. Vermilye Michael L. (Redmond WA). Hybrid thrust reverser cascade basket and method. USP1989084852805.
  24. Lair,Jean Pierre; Wolters,Gregory Thomas. Induction coupled variable nozzle. USP2006107127880.
  25. Linderman ; Duane L. ; Hom ; Felix. Integrated divergent exhaust nozzle thrust reverser. USP1978064093122.
  26. Moorehead James R. (Bellevue WA). Integrated power plant installation system. USP1984034437627.
  27. Klees Garry W. (Mercer Island WA) Wright Charles P. (Seattle WA). Internally ventilated noise suppressor with large plug nozzle. USP1985024501393.
  28. Lair Jean-Pierre (Plaisance FRX) Fage Etienne (Ramatuelle TX FRX) Finch Thomas E. (San Antonio TX). Jet engine having a planar exit opening. USP1992035097661.
  29. Fage Etienne (Ramatuelle FRX) Lair Jean-Pierre (Plaisance FRX). Jet engine provided with a thrust reverser. USP1994055310117.
  30. Fage Etienne (Ramatuelle FRX) Lair Jean-Pierre (Plaisance FRX). Jet engine provided with a thrust reverser. USP1990104966327.
  31. Fage Etienne (Ramatuelle FRX) Lair Jean-Pierre (Plaisance FRX). Jet engine provided with a thrust reverser. USP1993035192023.
  32. James Varnell L. (Auburn WA). Jet engine thrust reverser. USP1977054026105.
  33. Stachowiak Claude R. (Renton WA). Jet engine thrust reverser. USP1977064030290.
  34. Rudolph Peter K. C. (Seattle WA). Jet thrust reverser. USP1980014183478.
  35. Grabowski, Zbigniew M.; Winter, Michael. Managing spool bearing load using variable area flow nozzle. USP2011057950237.
  36. Repp Timothy O. (Renton WA). Mechanical lock for jet engine thrust reverser. USP1995095448884.
  37. Paulson Allen E. (P.O. Box 2206 Savannah GA 31402). Method and apparatus for quieting a turbojet engine. USP1993045203164.
  38. Klees Garry W. (Mercer Island WA). Mixed exhaust flow supersonic jet engine and method. USP1993065216878.
  39. Robinson Michael R. ; Ouellette Richard P.. Multi axis thrust vectoring for turbo fan engines. USP1998015706649.
  40. Klees Garry W. (Mercer Island WA) Lidstone Gary L. (Federal Way WA) Sloan Mark L. (Renton WA). Nozzle system and method for supersonic jet engine. USP1993065222359.
  41. MacLean Malcolm K. (Mason OH) Daniels Mark E. (Hamilton OH). Nozzle with thrust vectoring in the yaw direction. USP1990124978071.
  42. Klees Garry W. (Mercer Island WA). Plug-type exhaust nozzle having a variable centerbody and translating shroud. USP1989024802629.
  43. Smith Michael A. (Tacoma WA). Strut supported inlet. USP1984074458863.
  44. Culbertson Christopher C.. Supersonic engine, multi-port thrust reversing system. USP1999115987880.
  45. Klees Garry W. (Mercer Island WA). Supersonic jet engine installation and method with sound suppressing nozzle. USP1995115463866.
  46. Harris Alfred W. (Bellevue WA). Target type thrust reverser. USP1980084216923.
  47. Vermilye Michael L. (Redmond WA). Thrust reverser blocker door assembly. USP1986014564160.
  48. Sargisson Donald Farley (Cincinnati OH). Thrust reverser for a gas turbofan engine. USP1977064030291.
  49. Johnston Everett A. (Mason OH) Ryan Edward W. (Mason OH). Thrust reverser for a long duct fan engine. USP1981074278220.
  50. Rohra Alois (Mnchen DEX) Tracksdorf Peter (Grbenzell DEX). Thrust reverser for a propfan engine. USP1994095343696.
  51. Jurich Umberto (Kirkland WA). Thrust reverser for high bypass jet engines. USP1989024807434.
  52. Lair Jean-Pierre (8023 Vantage ; Suite 1450 San Antonio TX 78230). Thrust reverser integrating a variable exhaust area nozzle. USP1993015181676.
  53. Jackson John (Renton WA) Gucker Mark J. (Kirkland WA) Smith Mark H. (Birmingham AL). Thrust reverser synchronization shaft lock. USP1997035609020.
  54. Parham,Dean. Thrust reverser utilizing integrated structural bypass duct. USP2006107124981.
  55. Butler Lawrence (Cincinnati OH). Thrust reverser with variable nozzle. USP1997085655360.
  56. Harrison Geoffrey E. (Kirkland WA) Brown Robert B. (Renton WA). Thrust reversing system and method. USP1992045103634.
  57. Brown Robert B. (Renton WA). Thrust reversing system for high bypass fan engines. USP1990054922711.
  58. Brown Robert B. (Renton WA). Thrust reversing system for high bypass fan engines. USP1992095142862.
  59. Lair, Jean-Pierre. Thrust vectoring and variable exhaust area for jet engine nozzle. USP2005096938408.
  60. Thornock Russel L. (Seattle WA). Translating jet engine nozzle plug. USP1986064592508.
  61. Valleroy Laurent Georges,FRX. Turbo fan engine thrust reverser. USP1998035725182.
  62. Szuminski Gary F. (Marietta GA) Tape Robert F. (Marietta GA). Turbo machine nozzle with thrust reverser. USP1985074529130.
  63. Dhoore Louis G. (Seattle WA) Schultz William H. (Bellevue WA). Turbofan engine having variable geometry fan duct. USP1979054155221.
  64. Durand Lionel F. G. J. (Fontaine la Mallet FRX) Lor Xavier R. Y. (Le Havre FRX). Turbojet engine having a thrust reverser door and variable exhaust cross-section. USP1989094865256.
  65. Charier Gilles Alain,FRX ; Andre Guyonnet Xavier Jean-Michel,FRX ; Rollin Gilles Louis,FRX. Turbojet engine thrust reverser and exhaust nozzle. USP2001096289670.
  66. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser having movable rear baffle pivattally connected by forward and rear linkrods which are. USP1999115974783.
  67. Nightingale Douglas J. (Rolls-Royce Inc. ; 1895 Phoenix Blvd. Atlanta GA 30349). Turbomachine ejector nozzle. USP1984084463903.
  68. Szuminski Gary F. (Marietta GA) Nightingale Douglas J. (Atlanta GA) Tape Robert F. (Marietta GA). Turbomachine ejector nozzle and thrust reverser. USP1985034502638.
  69. Nightingale Douglas J. (Atlanta GA). Turbomachine ejector nozzle with thrust reverser. USP1985034502637.
  70. Thayer Edward B. (Jupiter FL) McLafferty George H. (North Palm Beach FL). Two dimensional gas turbine engine exhaust nozzle. USP1988064753392.
  71. Johnston Everett A. (Mason OH). Variable area exhaust nozzle. USP1979014132068.
  72. Duesler Paul W. ; Loffredo Constantino V. ; Prosser ; Jr. Harold T. ; Jones Christopher W.. Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems. USP1998075778659.
  73. Lair, Jean-Pierre. Variable area thrust reverser nozzle. USP2004026688099.
  74. Cariola Roy E. ; Aten Michael R.. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser. USP1998095806302.
  75. James Varnell L. (Kent WA). Variable geometry convergent divergent exhaust nozzle. USP1980044196856.
  76. Konarski Mieczyslaw (Lawrenceburg IN). Variable geometry exhaust nozzle. USP1983034375276.
  77. Loffredo Constantino V. ; Szyszko Charles J.. Variable geometry exhaust nozzle for a turbine engine. USP1998115833140.
  78. Carletti Ollivier (Vaux le Penil FRX). Variable geometry jet engine exhaust nozzle. USP1995085437412.
  79. Nightingale Douglas J. (Atlanta GA). Variable geometry nozzle with thrust reverser for a turbomachine. USP1984084463902.
  80. Adamson ; Arthur P.. Variable thrust nozzle for quiet turbofan engine and method of operating same. USP1978014068469.

이 특허를 인용한 특허 피인용횟수: 2

  1. Bahadoran, Iman; Cox, Jared. Sealing system for variable area fan nozzle. USP2018019856742.
  2. Kelford, Bryce Tyler; Holt, Bryan S.. Vibration damping drag link fitting for a thrust reverser. USP20180710024270.

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