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Method and system of controlling a jet engine for avoiding engine surge 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G01M-015/00
출원번호 US-0621326 (1975-10-10)
발명자 / 주소
  • Haloff
  • Gary J.
출원인 / 주소
  • The United States of America as represented by the Secretary of t, he Air, Force
대리인 / 주소
    Rusz, Joseph E.Siegel, Julian L.
인용정보 피인용 횟수 : 87  인용 특허 : 0

초록

A jet engine is controlled by placing time variant total pressure probes at the entry plane and the discharge plane of a jet engine fan. The pressure values at the probes are converted into electrical signals, filtered, and then fed to meters where the root-mean-square (RMS) values of the electrical

대표청구항

대표청구항이 없습니다.

이 특허를 인용한 특허 (87)

  1. Munsell, Peter M.; Stripinis, Philip S., Compressed air bleed supply for buffer system.
  2. Gallagher, Edward J.; Monzon, Byron R., Efficient, low pressure ratio propulsor for gas turbine engines.
  3. Gallagher, Edward J.; Monzon, Byron R., Efficient, low pressure ratio propulsor for gas turbine engines.
  4. Gallagher, Edward J.; Monzon, Byron R.; Bugaj, Shari L., Efficient, low pressure ratio propulsor for gas turbine engines.
  5. Gallagher, Edward J.; Monzon, Byron R.; Bugaj, Shari L., Efficient, low pressure ratio propulsor for gas turbine engines.
  6. Callahan, David J.; Mazzawy, Robert S.; Stryker, Howard Y.; Kelly, James B., Engine surge prevention system.
  7. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Epicyclic gear train.
  8. Otto, John R.; Baker, Stephanie M., Fan drive gear system manifold radial tube filters.
  9. McCune, Michael E.; Husband, Jason, Flexible support structure for a geared architecture gas turbine engine.
  10. McCune, Michael E.; Husband, Jason, Flexible support structure for a geared architecture gas turbine engine.
  11. McCune, Michael E.; Husband, Jason, Flexible support structure for a geared architecture gas turbine engine.
  12. Gallagher, Edward J.; Brilliant, Lisa I.; Straccia, Joseph C.; Balamucki, Stanley J.; Stephens, Mark A.; Hudon, Kate, Gas turbine engine airfoil.
  13. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  14. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  15. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  16. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  17. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  18. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  19. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  20. Baltas, Constantine, Gas turbine engine bifurcation located fan variable area nozzle.
  21. Suciu, Gabriel L.; Epstein, Alan H.; Lord, Wesley K.; McCune, Michael E.; Merry, Brian D., Gas turbine engine driving multiple fans.
  22. Munsell, Peter M.; Stripinis, Philip S., Gas turbine engine forward bearing compartment architecture.
  23. Munsell, Peter M.; Stripinis, Philip S., Gas turbine engine forward bearing compartment architecture.
  24. Munsell, Peter M.; Stripinis, Philip S., Gas turbine engine forward bearing compartment architecture.
  25. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Gas turbine engine gear train.
  26. Coffin, James B.; Pescosolido, Alessio, Gas turbine engine geared architecture axial retention arrangement.
  27. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L., Gas turbine engine shaft bearing configuration.
  28. Blackwell, Geoffrey T.; McVey, William J.; Tempelman, William G., Gas turbine engine variable area fan nozzle control.
  29. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  30. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  31. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  32. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  33. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  34. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  35. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  36. Kohlenberg, Gregory A.; Zamora, Sean P.; Schwarz, Frederick M., Gas turbine engine with fan variable area nozzle for low fan pressure ratio.
  37. Kohlenberg, Gregory A.; Zamora, Sean P.; Schwarz, Frederick M., Gas turbine engine with fan variable area nozzle to reduce fan instability.
  38. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Gas turbine engine with geared architecture.
  39. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Gas turbine engine with geared architecture.
  40. Suciu, Gabriel L.; Schwarz, Frederick M.; Ackermann, William K.; Kupratis, Daniel Bernard, Gas turbine engine with high speed low pressure turbine section.
  41. Suciu, Gabriel L.; Schwarz, Frederick M.; Ackermann, William K.; Kupratis, Daniel Bernard, Gas turbine engine with high speed low pressure turbine section.
  42. Schwarz, Frederick M.; Suciu, Gabriel L.; Ackermann, William K.; Kupratis, Daniel Bernard, Gas turbine engine with high speed low pressure turbine section and bearing support features.
  43. Schwarz, Frederick M.; Suciu, Gabriel L.; Ackermann, William K.; Kupratis, Daniel Bernard; McCune, Michael E., Gas turbine engine with high speed low pressure turbine section and bearing support features.
  44. Gilson, Jonathan; Cicon, Dennis; Atassi, Oliver V., Gas turbine engine with noise attenuating variable area fan nozzle.
  45. Coffin, James B.; McCune, Michael E.; Sheridan, William G., Gear carrier flex mount lubrication.
  46. Sheridan, William G., Gear system architecture for gas turbine engine.
  47. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
  48. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
  49. Sheridan, William G.; McCune, Michael E., Geared gas turbine engine with reduced oil tank size.
  50. Schwarz, Frederick M.; Kupratis, Daniel Bernard, Geared turbofan engine with a high ratio of thrust to turbine volume.
  51. Schwarz, Frederick M.; Hasel, Karl L., Geared turbofan engine with high compressor exit temperature.
  52. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  53. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  54. Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  55. Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  56. Schwarz, Frederick M.; Suciu, Gabriel L., Geared turbofan with a gearbox upstream of a fan drive turbine.
  57. Sanchez, Paul K.; Tu, John S.; Parekh, Kalpendu J.; Daniels, William A., Internal manifold for turning mid-turbine frame flow distribution.
  58. Topol, David A.; Morin, Bruce L.; Korte, Detlef, Low noise compressor and turbine for geared turbofan engine.
  59. Topol, David A.; Morin, Bruce L.; Korte, Detlef, Low noise compressor and turbine for geared turbofan engine.
  60. Topol, David A.; Morin, Bruce L., Low noise compressor rotor for geared turbofan engine.
  61. Topol, David A.; Morin, Bruce L., Low noise compressor rotor for geared turbofan engine.
  62. Kerr Walter B. (West Palm Beach FL), Method and apparatus for controlling a gas turbine engine.
  63. Hurwitz, Wayne; Levasseur, Glenn, Method and device to avoid turbo instability in a gas turbine engine.
  64. Sheridan, William G.; Hasel, Karl L., Method for setting a gear ratio of a fan drive gear system of a gas turbine engine.
  65. DaCunha, Nelson; Christophel, Jesse R., Method of assembling gas turbine engine section.
  66. Muldoon, Marc J.; Reinhardt, Gregory E., Mid-turbine frame buffer system.
  67. Schwarz, Frederick M.; Sheridan, William G., Monitoring system for non-ferrous metal particles.
  68. Sheridan, William G.; McCune, Michael E., Oil baffle for gas turbine fan drive gear system.
  69. Sheridan, William G., Oil loss protection for a fan drive gear system.
  70. Hurwitz, Wayne; McVey, William J., Operational line management of low pressure compressor in a turbofan engine.
  71. Hedrick Geoffrey S. M. (Malvern PA), Pressure transducer cross-check system.
  72. McCune, Michael E.; Portlock, Lawrence E., Ring gear mounting arrangement with oil scavenge scheme.
  73. McCune, Michael E.; Portlock, Lawrence E., Ring gear mounting arrangement with oil scavenge scheme.
  74. McCune, Michael E.; Portlock, Lawrence E., Ring gear mounting arrangement with oil scavenge scheme.
  75. Roberge, Gary D.; Berryann, Andrew P.; Carr, Scott A., Start system for gas turbine engines.
  76. Zeeban Joe P. (Renton WA) Johnson Paul E. (Bellingham WA), System for measuring aircraft engine thrust.
  77. Sabnis, Jayant, Thrust efficient turbofan engine.
  78. Sabnis, Jayant, Thrust efficient turbofan engine.
  79. Sabnis, Jayant, Thrust efficient turbofan engine.
  80. Sabnis, Jayant, Thrust efficient turbofan engine.
  81. Sabnis, Jayant, Thrust efficient turbofan engine.
  82. Snyder, Daniel A.; Lana, Kyle Charles; Sandoval, Jonathan Perry; Virkler, Scott Daniel; Taraskevich, Jaimie; Otero, Edwin, Turbine blade damper seal.
  83. Otto, John R., Turbine gear assembly support having symmetrical removal features.
  84. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph Brent; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  85. Atassi, Oliver V.; Petrenko, Oleg, Variable area fan nozzle with wall thickness distribution.
  86. Atassi, Oliver V.; Petrenko, Oleg, Variable area fan nozzle with wall thickness distribution.
  87. Weiner, Richard Alan, Variable area nozzle for gas turbine engine.
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