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Split fan work gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/04
출원번호 US-0587135 (1975-06-16)
발명자 / 주소
  • Simmons John Robert (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Lynn MA 02)
인용정보 피인용 횟수 : 50  인용 특허 : 0

초록

One or more of the aft stages of the fan section of a gas turbine engine are rotated by the high pressure turbine of a gas generator and the remainder of the fan stages are rotated by a low pressure turbine downstream of the gas generator. This arrangement divides the fan work between the low and hi

대표청구항

In a gas turbine engine having a compressor, combustor, high pressure turbine supplying rotational energy to the compressor and low pressure turbine in serial flow relation, all being circumscribed by an inner engine casing and an outer nacelle spaced apart from the inner engine casing to define a b

이 특허를 인용한 특허 (50)

  1. Ress, Jr., Robert A.; Stratton, Steve; Starr, Matthew J., Adaptive fan system for a variable cycle turbofan engine.
  2. Kupratis, Daniel Bernard, Adaptive fan with cold turbine.
  3. Rupp, George D.; Troia, Trajaen J., Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching.
  4. Orlando, Robert Joseph; Moniz, Thomas Ory; Baughman, John Lewis, Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans.
  5. Orlando, Robert Joseph; Moniz, Thomas Ory, Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines.
  6. Orlando, Robert Joseph; Moniz, Thomas Ory, Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines.
  7. Johnson, James Edward, Apparatus and method for assembling gas turbine engines.
  8. Johnson James E. (Hamilton OH) Castells Onofre T. M. (Fairfield OH) Rundell Dan J. (Madeira OH), Auxiliary lift propulsion system with oversized front fan.
  9. Neitzel Robert E. (Marblehead MA), Convertible aircraft engine.
  10. Orlando, Robert Joseph; Moniz, Thomas Ory, Counter rotating fan aircraft gas turbine engine with aft booster.
  11. Newton Arnold C,GBX, Ducted fan gas turbine engine with variable area fan duct nozzle.
  12. Oliver Richard C. (8504 W. 125 N. West Lafayette IN 47906), Electronic sound generating system for a stringed musical instrument.
  13. Fitzpatrick, Erich R., Exhaust fan systems.
  14. Orlando, Robert Joseph; Moniz, Thomas Ory, Gas turbine assembly and methods of assembling same.
  15. Bradbrook, Stephen John; Davis, Brian; Wilson, Richard James, Gas turbine engine.
  16. Bradbrook, Stephen John; Davis, Brian; Wilson, Richard James, Gas turbine engine.
  17. Paul Marius A. (1100 E. Orangethorpe Ave. ; Ste. 140 Anaheim CA 92801), Gas turbine engine.
  18. Kupratis, Daniel B., Gas turbine engine with intercooling turbine section.
  19. Kupratis, Daniel B., Gas turbines with multiple gas flow paths.
  20. Kupratis, Daniel B., Gas turbines with multiple gas flow paths.
  21. Kupratis, Daniel B., Gas turbines with multiple gas flow paths.
  22. Lugg, Richard H.; Youngren, Harold, Hybrid jet/electric VTOL aircraft.
  23. Wagenknecht Conrad D. (West Chester OH) Faust Guy K. (West Chester OH), Individual bypass injector valves for a double bypass variable cycle turbofan engine.
  24. Ruthemeyer, Michael Anthony, Integrated variable geometry flow restrictor and heat exchanger.
  25. McVey, William J., Managing low pressure turbine maximum speed in a turbofan engine.
  26. Simmons John R. (Montgomery OH), Means for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine.
  27. Simmons John R. (Montgomery OH), Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas.
  28. Simmons John R. (Montgomery OH), Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine.
  29. Wilson,Kenneth J.; Jaul,Warrent K.; Fitzpatrick,Shannon L.; Burman,Robert G., Method for using variable supersonic Mach number air heater utilizing supersonic combustion.
  30. Christophel, Jesse R., Method of assembling gas turbine engine section.
  31. DaCunha, Nelson; Christophel, Jesse R., Method of assembling gas turbine engine section.
  32. Giffin, Rollin George; Powell, Brandon Flowers; Harrington, Mark; Johnson, James Edward, Method of operating adaptive core engines.
  33. Stern, Alfred M., Method of using an afterburner to reduce high velocity jet engine noise.
  34. Griffin, III,Rollin George; Morrow,William James, Methods and apparatus for assembling a gas turbine engine.
  35. Dawson, David Lynn; Lariviere, Erin Lee; Petersen, Brian Joseph; Ellerhorst, Robert Jerome, Multi-nozzle flow diverter for jet engine.
  36. Paul Marius A. (1100 E. Orangethorpe Ave. ; Ste. 140 Anaheim CA 92801), Multiple propulsion with quatro vectorial direction system.
  37. Christians, Joseph T., Pre-turbine engine case variable area mixing plane.
  38. Giffin ; III Rollin G. ; Johnson James E. ; Crall David W. ; Salvage John W. ; Szucs Peter N., Turbofan engine with a core driven supercharged bypass duct.
  39. Bartos James W., Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and a.
  40. Ruberte Sanchez, Jose E., Turbomachine bypass flow diverting assembly and method.
  41. Sankrithi, Mithra M. K. V.; Seidel, Gerhard E.; Prichard, Alan K.; Moore, Matthew, Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan.
  42. Kenworth ; Ivan E. ; Woltmann ; Ivan E., Variable area bypass injector system.
  43. Murphy, Michael J., Variable area fan nozzle.
  44. Schirle Steven M. (Boynton Beach FL) Baghdadi Samy (Palm Beach Gardens FL) Khalid Syed J. (Palm Beach Gardens FL) Perkins Gary M. (Palm Beach Gardens FL), Variable cycle engine with enhanced stability.
  45. Heathco, Craig, Variable cycle gas turbine engine.
  46. Hubbard, Adrian Alexander, Variable mode jet engine--compact.
  47. Wilson, Kenneth J.; Jaul, Warren K.; Burman, Robert G.; Fitzpatrick, Shannon L., Variable supersonic mach number air heater utilizing supersonic combustion.
  48. Baughman, John Lewis; Orlando, Robert Joseph; Moniz, Thomas Ory, Variable torque split aircraft gas turbine engine counter rotating low pressure turbines.
  49. Birch Stanley F. (Bellevue Federal Way WA) Lawler John A. (Federal Way WA) Paynter Gerald C. (Seattle WA), Vortex generators for internal mixing in a turbofan engine.
  50. Birch Stanley F. (Bellevue WA) Lawler John A. (Seattle WA) Paynter Gerald C. (Seattle WA), Vortex generators for internal mixing in a turbofan engine.
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