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Thrust reverser with variable nozzle

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0694808 (1996-08-09)
발명자 / 주소
  • Butler Lawrence (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 83  인용 특허 : 0

초록

A thrust reverser is provided for both modulating and reversing bypass flow discharged from a fan through a bypass duct of a turbofan gas turbine engine. The reverser includes an aft cowl joined to a forward cowl and having an aft end surrounding a core engine to define a discharge fan nozzle of min

대표청구항

A thrust reverser for modulating and reversing bypass flow discharged from a fan through a bypass duct defined between a core engine and a fan nacelle comprising: an aft cowl of said nacelle joined to a forward cowl thereof and having an aft end defining with a core cowl surrounding said core engine

이 특허를 인용한 특허 (83)

  1. Jones, Teddy L.; Wallen, Gregory T.; Gibbons, Kevin; Villano, William E., Actuation system.
  2. Ramlaoui, Jihad I.; Pinto, Geoffrey; Shetzer, Daniel; Amkraut, Daniel M.; Hawksworth, Andrew Robert; Harvey, John; Evans, Alan K.; Chandarana, Vikram; Moorhouse, Roger, Actuation system for a translating variable area fan nozzle.
  3. Ramlaoui, Jihad I.; Pinto, Geoffrey; Shetzer, Daniel; Amkraut, Daniel M.; Hawksworth, Andrew Robert; Harvey, John; Evans, Alan K.; Chandarana, Vikram; Moorhouse, Roger, Actuation system for a translating variable area fan nozzle.
  4. Zsurka, Mark, Aerodynamic track fairing for a gas turbine engine fan nacelle.
  5. Beardsley, Peter K; Knight, Glenn A, Aeroengine thrust reverser.
  6. Baker, Von David, Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle.
  7. Hatrick, Michael John; Bennett, Joel David; McEvoy, Finbarr; Campbell, Hugh Keith; Beattie, William Edwin, Aircraft propulsive power unit.
  8. Thornock, Russel L.; Sangwin, Michael L.; Hsiao, Entsung, Aircraft systems including cascade thrust reversers.
  9. Tsou, Chi-Ling Michael; Holdren, Carl Francis; Bailey, William Andrew; Lenahan, Dean Thomas, Baffle seal for gas turbine engine thrust reverser.
  10. Tsou, Chi-Ling Michael; Holdren, Carl Francis; Bailey, William Andrew; Lenahan, Dean Thomas, Baffle seal for gas turbine engine thrust reverser.
  11. Lair, Jean-Pierre; Peters, Frederick Henry, Bifold door thrust reverser.
  12. Lair, Jean-Pierre, Confluent exhaust nozzle.
  13. Lair, Jean-Pierre, Confluent variable exhaust nozzle.
  14. Jannetta, Thomas J.; Peters, Frederick H., Converging nozzle thrust reverser.
  15. James, Norman J., Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle.
  16. Marshall, Richard M., Dual function cascade integrated variable area fan nozzle and thrust reverser.
  17. Marshall, Richard M., Dual function cascade integrated variable area fan nozzle and thrust reverser.
  18. Suciu, Gabriel L.; Merry, Brian D.; Penda, Allan R.; Dye, Christopher M.; Bhatt, Jay, Fan case thrust reverser.
  19. Rosenkrans, William E.; Morris, Robert J., Flutter sensing system for a gas turbine engine.
  20. Chanez, Philippe Gerard; Zeggai, Kamel, Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl.
  21. Malecki, Robert E., Gas turbine engine thrust reverser system.
  22. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  23. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  24. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  25. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  26. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  27. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  28. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  29. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  30. Kohlenberg, Gregory A.; Zamora, Sean P.; Schwarz, Frederick M., Gas turbine engine with fan variable area nozzle for low fan pressure ratio.
  31. Kohlenberg, Gregory A.; Zamora, Sean P.; Schwarz, Frederick M., Gas turbine engine with fan variable area nozzle for low fan pressure ratio.
  32. Kohlenberg, Gregory A.; Zamora, Sean P.; Schwarz, Frederick M., Gas turbine engine with fan variable area nozzle to reduce fan instability.
  33. Smith, Peter G.; Ochs, Stuart S.; Schwarz, Frederick M., Gas turbine engine with low fan pressure ratio.
  34. Do, Logan H.; Krystowski, Edward A., Gas turbine engine with variable area fan nozzle.
  35. Stern, Alfred M., Gas turbine engine with variable area fan nozzle bladder system.
  36. Ramlaoui, Jihad I.; Roberts, Stephen Michael; Forsey, David, Guide system for nacelle assembly.
  37. Roberts, Stephen Michael, Guide system for nacelle assembly.
  38. Lair,Jean Pierre; Wolters,Gregory Thomas, Induction coupled variable nozzle.
  39. Sundstrom, Dale B.; Gibbons, Kevin; Jones, Teddy L., Integrated electric variable area fan nozzle thrust reversal actuation system.
  40. Martens,Steven; Saddoughi,Seyed Gholamali; Early,Kevin Sean, Method and apparatus for noise attenuation for gas turbine engines using at least one synthetic jet actuator for injecting air.
  41. Howe, Mark E., Method of varying a fan duct nozzle throat area of a gas turbine engine.
  42. Parham, Dean L., Method of varying a fan duct throat area.
  43. Caruel, Pierre; Segat, Peter, Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle.
  44. Vauchel, Guy Bernard, Nacelle for aircraft engine having a nozzle with a variable section.
  45. Bulin, Guillaume; Oberle, Patrick; Surply, Thierry, Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle.
  46. Lair,Jean Pierre, Nested latch thrust reverser.
  47. Lair, Jean-Pierre, Pivoting door thrust reverser for a turbofan gas turbine engine.
  48. Howe, Mark E., Pivoting fan nozzle nacelle.
  49. Lair, Jean-Pierre, Rotary adjustable exhaust nozzle.
  50. Tsou, Chi-Ling Michael; Holdren, Carl Francis; Bailey, William Andrew; Lenahan, Dean Thomas, Sealing arrangements for gas turbine engine thrust reverser.
  51. Lair, Jean-Pierre, Self stowing thrust reverser.
  52. Lair,Jean Pierre, Spider actuated thrust reverser.
  53. Biset, Charles M., System and apparatus for a thrust reverser.
  54. Kopecek, Joseph Thomas; Walker, Peter William, System and method for operating a thrust reverser for a turbofan propulsion system.
  55. Lair, Jean-Pierre, Thrust reverser.
  56. Murphy, Michael Joseph, Thrust reverser assembly with shaped drag links.
  57. Aten, Michael Ray; Crawford, Sara Christine, Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion.
  58. Aten, Michael Ray; Crawford, Sara Christine, Thrust reverser cascade assembly with flow deflection shelf.
  59. West, Randall R.; Schaefer, Henry A., Thrust reverser configuration for a short fan duct.
  60. Gallet, Francois, Thrust reverser device for compact jet pipe.
  61. Lair, Jean-Pierre, Thrust reverser door.
  62. Lair, Jean-Pierre, Thrust reverser door.
  63. Lair, Jean-Pierre, Thrust reverser for a turbofan gas turbine engine.
  64. Lair, Jean-Pierre, Thrust reverser nozzle for a turbofan gas turbine engine.
  65. Caruel, Pierre; Segat, Peter, Thrust reverser with retractable cascade vanes.
  66. Harrison, Geoffrey E.; Sternberger, Joe E.; Lallement, Michael K.; Strunk, John T.; Byrd, William S.; Jundt, Darrell C., Thrust reversers including locking assemblies for inhibiting deflection.
  67. Sternberger, Joe E., Thrust reversers including support members for inhibiting deflection.
  68. Stern, Alfred M., Thrust reversing variable area nozzle.
  69. Stern, Alfred M., Thrust reversing variable area nozzle.
  70. Lair, Jean-Pierre, Toggle interlocked thrust reverser.
  71. Cloft, Thomas G.; Gukeisen, Robert L., Translatable cascade thrust reverser.
  72. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  73. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  74. Wang, Shunshen Richard, Translating variable area fan nozzle with split beavertail fairings.
  75. Kemper, Paul D.; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine nozzle assembly and method of operating same.
  76. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D., Variable area fan nozzle bearing track.
  77. Grabowski, Zbigniew M.; Morris, Robert J.; Carmichael, Ray W., Variable area fan nozzle fan flutter management system.
  78. Chakkera, Kevin K.; Vaughan, Ron, Variable area fan nozzle systems with improved drive couplings.
  79. Frank, Joel Hudson; James, Norman John; Wang, Shunshen Richard; McKleny, Bryant Lynoel; Baer, David A.; Jones, Tony; Harvey, John H.; Bacon, Peter W.; Hubberstey, Mark; Wharton, Brett J.; Davies, Neil C.; Roberts, Stephen Michael; Wylie, Steven Andrew, Variable area fan nozzle with bypass flow.
  80. Binks, Alan; Layland, Michael J.; James, Norman J., Variable area fan nozzle with one or more integrated blocker doors.
  81. Weiner, Richard Alan, Variable area nozzle for gas turbine engine.
  82. Lair,Jean Pierre, Variable cam exhaust nozzle.
  83. Lair,Jean Pierre, Ventilated confluent exhaust nozzle.
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