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Deicing of a geared gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
  • F02G-003/00
출원번호 US-0046708 (1987-05-07)
발명자 / 주소
  • Perry Derick A. (Derby)
출원인 / 주소
  • Rolls-Royce Plc (London GBX 03)
인용정보 피인용 횟수 : 71  인용 특허 : 3

초록

A geared turbofan gas turbine engine has a fan rotor carrying a plurality of fan blades driven by a gas generator via a gear assembly. A fan casing which has an exterior surface is positioned coaxially with and encloses the fan rotor. A lubricant supply is provided to lubricate and cool the gear ass

대표청구항

A geared gas turbine engine comprising a gas generator, at least one rotor carrying a plurality of blades, a gear assembly, a surface to be deiced, the at least one rotor being driven by the gas generator via the gear assembly, a lubricant supply to lubricate and cool the gear assembly, a heat excha

이 특허에 인용된 특허 (3)

  1. Hurley John F. (Huntington CT), Air pump for turbofan fuel control system.
  2. Harper John Everett (Phoenix AZ) Kell Louis H. (Phoenix AZ), Fuel system pneumatic purge apparatus and method.
  3. Shah Anil D. (Seattle WA), Integrated thermal anti-icing and environmental control system.

이 특허를 인용한 특허 (71)

  1. Stretton,Richard G; Beardsley,Peter, Aeroengine intake having a heat exchanger within an annular closed chamber.
  2. Todorovic, Predrag, Air ejector nozzle tube for an oil heat exchanger of an aircraft engine.
  3. Cheong, Chee Yuen, Air recovery system for precooler heat-exchanger.
  4. Todorovic, Predrag, Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device.
  5. Warnet, Stephane, Aircraft turbine engine comprising an air intake housing with a variable aerodynamic profile.
  6. DiBenedetto, Enzo; Coffin, James B.; Davis, Todd A., Apparatus and method for providing damper liquid in a gas turbine.
  7. DiBenedetto, Enzo; Coffin, James B.; Davis, Todd A., Apparatus and method for providing damper liquid in a gas turbine engine.
  8. Ullyott, Richard, Compact compound engine package.
  9. Laurant, Franck; Bellet, Francois; Joret, Jean-Philippe, Composite panel having a built-in duct.
  10. Suciu, Gabriel L.; Glahn, Jorn A.; Dye, Christopher M., Compression system for turbomachine heat exchanger.
  11. Twerdochlib,Michael, Compressor airfoil surface wetting and icing detection system.
  12. Caruel, Pierre; Hurlin, Hervé, De-icing and conditioning device for an aircraft.
  13. Jain, Ashok K.; Winter, Michael, Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the ice.
  14. Belmonte, Olivier; Bart, Jacques René, Device for de-icing a turbomachine separator.
  15. Alain Porte FR; Stephane Viala FR, Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit.
  16. Bonnaud,Cyril, Drain particularly for engine support strut.
  17. Weiner, Richard Alan, Dual function air diverter and variable area fan nozzle.
  18. Blackwelder, Mark J.; Alt, John Timothy; Gagne, Steven; Vetters, Daniel Kent, Electrical power generation apparatus for contra-rotating open-rotor aircraft propulsion system.
  19. Bolender, Lars; Wagnon, Sébastien, Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system.
  20. Sheridan, William G., Fan drive planetary gear system integrated carrier and torque frame.
  21. Xu, JinQuan, Fluid system with gravity controlled valve.
  22. Zhang, Hua; Byrd, Douglas Scott; Hu, Iris Ziqin; Erickson, Dean Matthew, Fuel conditioning system.
  23. Appukuttan, Ajith; Keeler, Benjamin; Vanacore, Paolo, Gas turbine engine anti-icing system.
  24. Ackermann, William K.; Stripinis, Philip S., Gas turbine engine buffer system providing zoned ventilation.
  25. Ackerman Steven C. ; Berry Brian S. ; Pedotto Vincent A., Gas turbine engine commanded oil flow valve with failsafe.
  26. Coffinberry, George Albert, Gas turbine engine fan bleed heat exchanger system.
  27. Pero, Edward B., Gas turbine engine fan variable area nozzle with swivable insert system.
  28. Storage, Michael Ralph; McQueen, Dennis Alan; Foster, Roger Earl, Gas turbine engine heat exchangers and methods of assembling the same.
  29. Dooley, Kevin Allan, Gas turbine engine including apparatus to transfer power between multiple shafts.
  30. Dooley, Kevin Allen, Gas turbine engine including apparatus to transfer power between multiple shafts.
  31. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L., Gas turbine engine shaft bearing configuration.
  32. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L., Gas turbine engine shaft bearing configuration.
  33. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L., Gas turbine engine shaft bearing configuration.
  34. Ullyott, Richard; Mitrovic, Lazar; Dubreuil, Jean; Kenny, Stephen Christopher; Bouchard, Guy; Medvedev, Ilya B.; Morgan, Keith; Karanjia, Darius Jehangir; Youssef, Nashed Azer, Gas turbine engine with transmission and method of adjusting rotational speed.
  35. Todorovic, Predrag; Poenick, Sascha, Gas-turbine engine with oil cooler in the engine cowling.
  36. Parnin, Francis; DiBenedetto, Enzo, Gravity operated valve.
  37. Venkataramani, Kattalaicheri Srinivasan; Moniz, Thomas Ory; Stephenson, Justin P.; Bailey, William Andrew, Heat pipe-based cooling apparatus and method for turbine engine.
  38. Roby, Benjamin; Monttinen, Jarmo, Heated booster splitter plenum.
  39. Roby, Benjamin; Monttinen, Jarmo, Heated booster splitter plenum.
  40. Thompson,Robert G., Inlet muff anti-icing system for an auxiliary power unit.
  41. Ullyott,Richard, Integral cooling system for rotary engine.
  42. Romani Giuseppe,CAX, Integrated fan / low pressure compressor rotor for gas turbine engine.
  43. Roberge, Gary D., Integrated heat exchangers for low fan pressure ratio geared turbofan.
  44. Merry, Brian D.; Suciu, Gabriel L.; Brilliant, Lisa I.; Rose, Becky E.; Dong, Yuan; Balamucki, Stanley J., LPC flowpath shape with gas turbine engine shaft bearing configuration.
  45. Schilling, Jan Christopher, Method and apparatus for operating gas turbine engines.
  46. Kumar, Hemanth Gudibande Sathyakumar; Mondal, Bhaskar Nanda; Moniz, Thomas Ory, Method and system for metallic low pressure fan case heating.
  47. Venkataramani,Kattalaicheri Srinivasan; Butler,Lawrence; Lee,Ching Pang, Methods and apparatus for operating gas turbine engines.
  48. Griffiths, James Alan; Smith, Mitchell Donald; Bartos, James William, Methods and apparatus for supplying cooling air to turbine engines.
  49. Caruel, Pierre, Nacelle equipped with an oil-cooling circuit comprising an intermediate heat exchanger.
  50. Baptist,Praba Kharan; Bharath,Keppel Nyron, Nacelle inlet lip anti-icing with engine oil.
  51. Zysman, Steven H., Nacelle scoop inlet.
  52. DiBenedetto, Enzo; Parnin, Francis; James, Denman H.; Peters, Robert E., Oil bypass channel deaerator for a geared turbofan engine.
  53. DiBenedetto, Enzo, Oil capture and bypass system.
  54. Parnes Marvin J. (Norwalk CT) Vogel Herman (Newtown CT), Oil cooler for fan jet engines.
  55. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  56. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  57. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  58. Dionne,Luc, Passive cooling system for auxiliary power unit installation.
  59. Larkin,Michael J.; Eiler,Donald C., Supplemental oil cooler airflow for gas turbine engine.
  60. Smith, Alan W., System and method to manage transients for rapid power demand changes.
  61. Ritland,Paul David, System for heating an air intake of turbine engine.
  62. Mackin, Steve; Fisher, Robert Earl, Systems and methods for preventing ice formation on portions of an aircraft.
  63. Bintz, Matthew E.; Gendrich, Charles P.; DiTomasso, John C.; Murphy, Andrew J., Thermal management system for a gas turbine engine with an integral oil tank and heat exchanger in the nacelle.
  64. Wolford, Robert Lee, Thermal system for a working member of a power plant.
  65. NguyenLoc, Fred; Quach, San, Turbine engine transmission gutter.
  66. NguyenLoc, Fred; Quach, San, Turbine engine transmission gutter.
  67. Olver, Bryan; Ciampa, Alessandro; Marrano, Roberto; Trepanier, Richard; Lamarre, Sylvain; Bernard, Martin; Germain, Patrick, Turbofan bypass duct air cooled fluid cooler installation.
  68. Wadia, Aspi R.; Holm, Raymond G., Turbofan engine internal anti-ice device.
  69. Norris, James W.; Twelves, Jr., Wendell V., Vapor cooling of detonation engines.
  70. Grabowski, Zbigniew M.; Morris, Robert J.; Carmichael, Ray W., Variable area fan nozzle fan flutter management system.
  71. Parnin, Francis, Windmill and zero gravity lubrication system for a gas turbine engine.
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