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특허 상세정보

Turbine engine having improved thrust bearing load control

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/08   
미국특허분류(USC) 60/726 ; 415/106
출원번호 US-0771906 (1996-12-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Astle
인용정보 피인용 횟수 : 34  인용 특허 : 15
초록

A modified turbine engine design in which control of the forward load on a thrust bearing is improved, while reducing or eliminating the need for the use of a balance piston is disclosed. The turbine engine has a longitudinal axis and comprises, a compressor for pressurizing gases in the engine. The impeller has an impeller rear face and a tip. The engine further comprises a shaft mounted to a thrust bearing for rotation about the axis. The impeller is fixed to the shaft for rotation therewith. A cavity fixed within the engine casing is defined at least ...

대표
청구항

[ I claim:] [1.] A turbine engine within an engine casing, said turbine engine hating a longitudinal axis, said turbine engine comprising:a compressor comprising an impeller, said impeller having an impeller rear face and an impeller tip, said compressor for pressurizing gases in said turbine engine;a shaft mounted to a thrust bearing for rotation about said axis, said impeller fixed to said shaft for rotation therewith;a combustion section in flow communication with pressurized gases from said compressor;a cavity fixed within said engine casing and defi...

이 특허에 인용된 특허 (15)

  1. Campbell David A. (Borrowash GB2) Morley Frederick W. W. (Castle Donington GB2). Air cooled turbine for a gas turbine engine. USP1982094348157.
  2. Neal Peter F. (Derby GB2). Air cooling systems for gas turbine engines. USP1987044657482.
  3. Speak Trevor H. (Gloucester GB2) Kernon John D. (Bristol GB2) Roberts Derek A. (Bristol GB2). Air sealing for turbomachines. USP1984014425079.
  4. Mize Christopher D. (Palm Beach Gardens FL) Pirsig William W. (Manchester CT) Vercellone Peter T. (North Haven CT). Anti-contamination thrust balancing system for gas turbine engines. USP1995045402636.
  5. Cantor Eugene (Glastonbury CT) Farrand Thomas A. (Glastonbury CT). Anti-rotation feature for a turbine rotor faceplate. USP1987104701105.
  6. Laurello Vincent P. (Guilford CT). Gas turbine engine having bleed apparatus with dynamic pressure recovery. USP1980124236869.
  7. Hennecke Dietmar (Rossdorf DEX) Pfaff Klaus (Munich DEX) Grigo Dietrich (Munich DEX). Gas turbine propulsion unit with devices for branching off compressor air for cooling of hot parts. USP1988084761947.
  8. Kelch George W. (Palm Beach Gardens FL). Method and apparatus for assessing thrust loads on engine bearings. USP1990034907943.
  9. Radtke Leland J. (North Palm Beach FL). Radial inflow blade cooling system. USP1976113990812.
  10. Brown Wayne M. (North Granby CT) Neal William F. (South Windsor CT) Schwarz Frederick M. (Glastonbury CT). Rotor thrust balancing. USP1987104697981.
  11. Coplin John F. (Duffield GB2) Hadaway Edward S. (Duffield GB2). Turbine. USP1984014428713.
  12. Adamson Arthur P. (Cincinnati OH). Turbine cooling air modulation apparatus. USP1981104296599.
  13. Hovan Edward J. (Manchester CT) Stephens Guilford E. (Manchester CT) Peele Samuel C. (Glastonbury CT). Turbine cooling for gas turbine engine. USP1989044820116.
  14. Cameron Daniel G. (West Chester OH) Albrecht Richard W. (Fairfield OH) Kutney ; Jr. John T. (Cincinnati OH). Turbine disk forward seal assembly. USP1994015275534.
  15. Charier Gilles A. (La Grande Paroisse FRX) Guyonnet Xavier ; J. M. A. (St Fargeau Ponthierry FRX) Picard Jean-Louis (Vaux le Penil FRX). Turbo-engine provided with a device for blowing air onto a rotor element. USP1995085440874.

이 특허를 인용한 특허 피인용횟수: 34

  1. Friedl,Winfried Hagen. Arrangement for bearing relief in a gas turbine. USP2007017156613.
  2. Hart, Katherine; Held, Timothy James. Automated mass management control. USP2018019863282.
  3. Fish,Jason Araan; L챕gar챕,Pierre Yves; Hawie,Eduardo David. Bearing chamber pressurization system. USP2007107287384.
  4. Held, Timothy James; Vermeersch, Michael Louis; Xie, Tao. Carbon dioxide refrigeration cycle. USP2015069062898.
  5. Virkler, Scott D.. Component lock for a gas turbine engine. USP2014098840375.
  6. Faulder, Leslie John. Compressor aft hub sealing system. USP2017069677423.
  7. Held, Timothy James; Vermeersch, Michael; Xie, Tao. Driven starter pump and start sequence. USP2016089410449.
  8. Schwarz, Frederick M.; Glahn, Jorn A.. Fan drive thrust balance. USP20181010107131.
  9. Oxman, Ilia; Michelassi, Vittorio. Fan-cooled electrical machine with axial thrust compensation. USP20190210218245.
  10. Arase, Kenichi; Katou, Eigo; Takeuchi, Masato. Gas turbine and method of opening chamber of gas turbine. USP2015079080464.
  11. Held, Timothy J.; Miller, Jason D.. Heat engine and heat to electricity systems and methods for working fluid fill system. USP2015038966901.
  12. Held, Timothy James; Hostler, Stephen; Miller, Jason D.; Vermeersch, Michael; Xie, Tao. Heat engine and heat to electricity systems and methods with working fluid mass management control. USP2016109458738.
  13. Held, Timothy James. Heat engine cycles for high ambient conditions. USP2014108857186.
  14. Kacludis, Alexander Steven; Hostler, Stephen R.; Zakem, Steve B.. Heat engine system with a supercritical working fluid and processes thereof. USP2015089118226.
  15. Held, Timothy James. Heat engines with cascade cycles. USP2014108869531.
  16. Gurin, Michael H.. Heat pump with integral solar collector. USP2016049316404.
  17. Legare, Pierre-Yves; Herborth, Jason Todd; Arthur, Glen Owen. Impeller baffle with air cavity deswirlers. USP2010037682131.
  18. Legare, Pierre-Yves. Impeller rear cavity thrust adjustor. USP2010087775758.
  19. Alecu, Daniel T.; Watson, John. Load distribution system for gas turbine engine. USP2012058182201.
  20. Ganelin Boris. Method and device for reducing axial thrust in rotary machines and a centrifugal pump using same. USP2000106129507.
  21. Vermeersch, Michael Louis; Bowan, Brett A.; Khairnar, Swapnil. Methods for reducing wear on components of a heat engine system at startup. USP2017059638065.
  22. Virkler, Scott D.; Arnold, Jason. Multi-function heat shield for a gas turbine engine. USP2014038662845.
  23. Held, Timothy James; Vermeersch, Michael Louis; Xie, Tao; Miller, Jason. Parallel cycle heat engines. USP2016039284855.
  24. Bowan, Brett A.. Process for controlling a power turbine throttle valve during a supercritical carbon dioxide rankine cycle. USP2017099752460.
  25. Tanimura, Kazuhiko. Sealing apparatus with multistage brush seal. USP2014048707711.
  26. Xie, Tao; Vermeersch, Michael; Held, Timothy. Supercritical carbon dioxide power cycle for waste heat recovery. USP2016059341084.
  27. Vermeersch, Michael Louis. Supercritical working fluid circuit with a turbo pump and a start pump in series configuration. USP2015079091278.
  28. Held, Timothy James. System and method for managing thermal issues in gas turbine engines. USP2015049014791.
  29. Held, Timothy James. System and method for managing thermal issues in one or more industrial processes. USP2016099441504.
  30. Pal, Dipankar; Garcia-Crespo, Andres Jose. System and method for modifying rotor thrust. USP2013058434994.
  31. Held, Timothy J.; Hostler, Stephen; Miller, Jason D.; Hume, Brian F.. Thermal energy conversion device. USP2015089115605.
  32. Liu Xiaoliu,CAX. Turbine engine having improved high pressure turbine cooling. USP2001056227801.
  33. Liu, Xiaoliu. Turbine engine having turbine cooled with diverted compressor intermediate pressure air. USP2003116647730.
  34. Liu Xiaoliu,CAX. Turbine engine with cooled P3 air to impeller rear cavity. USP2000036035627.