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특허 상세정보

Gas turbine group with reheat combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/14   
미국특허분류(USC) 60/3917 ; 60/39182
출원번호 US-0525040 (1995-09-08)
우선권정보 CH-0001079 (1993-04-08)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 35  인용 특허 : 3
초록

In a gas turbine group which consists essentially of a compressor (2), a first combustion chamber (3), a first turbine (4), a second combustion chamber (5) and a second turbine (6), the first combustion chamber (3) is configured as an annular combustion chamber. This annular combustion chamber (3) is operated by a number of premixing burners (11) which are distributed at the periphery. The first turbine (4) is designed in such a way that its exhaust gases have a temperature level which is above the self-ignition temperature of the fuel (13) used in the s...

대표
청구항

A gas turbine group, comprising: at least one compressor unit; a first combustion chamber for generating working gas, the first combustion chamber connected to receive compressed air from the compressor unit, the first combustion chamber being an annular combustion chamber having a plurality of premixing burners; a first turbine connected to received working gas from the first combustion chamber; a second turbine; a second combustion chamber connected to receive exhausted working gas from the first turbine and deliver working gas to the second turbine, t...

이 특허를 인용한 특허 피인용횟수: 35

  1. Bunker, Ronald Scott. Aerodynamic pylon fuel injector system for combustors. USP2014078763400.
  2. Helgeson Norman Lewis. Annular after reactor for use with a jet engine test cell. USP2001056237395.
  3. Norman Lewis Helgeson. Annular after reactor with sound attenuator for use in a jet engine test cell and test stand. USP2002126497137.
  4. Zebec, Igor; Schweizer, Raphael; Stedul, Josip; Schmitt, Tobias; Szücs, Frigyes. Apparatus and method for the forming of turbine vane cover plates. USP2015089097116.
  5. Dobbeling, Klaus. Burner for heat generator. USP2004036702574.
  6. Rauch, Marc; Hoenig, Felix. Carrier ring. USP20180710012094.
  7. Carroni, Richard; Flohr, Peter. Combustion method and burner for carrying out the method. USP2005056896509.
  8. Keller Jakob J.,CHX. Combustor for a gas turbine. USP2001086272864.
  9. Payling, Stephen R.; Coleman, Robert P.; Brown, Curtis L.. Control systems and methods for water injection in a turbine engine. USP2003046553753.
  10. Gilchrist, III, George Martin; Simpson, Stanley Frank; Karim, Hasan. Exhaust gas recirculation system, turbomachine system having the exhaust gas recirculation system and exhaust gas recirculation control method. USP2016039297306.
  11. Paschereit Christian Oliver,CHX ; Polifke Wolfgang,CHX ; Sattelmayer Thomas,CHX. Gas turbine combustion chamber with two stages and enhanced acoustic properties. USP2000046050078.
  12. Genin, Franklin Marie; Aluri, Naresh; Cerny, Jan; Eroglu, Adnan; Pasqualotto, Ennio. Gas turbine combustion system. USP2017119810152.
  13. Ebacher, Jon V.; Nin, Carol Noëlle. Gas turbine engine and reheat system. USP2015038984859.
  14. Hines William R.. Gas turbine engine with water injection. USP2000016012279.
  15. Stryapunin, Sergey Aleksandrovich; McMahan, Kevin Weston; Myers, Geoffrey David. Gas turbine system having premixed injector vanes. USP2015089097184.
  16. Olmes, Sven; Reiter, Wilhelm; Zierer, Thomas. Gas turbine with heat exchanger for cooling compressed air and preheating a fuel. USP2010107810332.
  17. Lockwood, Jr.,Hanford N.. High compression gas turbine with superheat enhancement. USP2007087254951.
  18. Attia Magdy S.. High temperature compression and reheat gas turbine cycle and related method. USP2000066079197.
  19. Davis, Jr., Lewis Berkley; Foster, Gregory Thomas; Graham, Kaitlin Marie; Venkataraman, Krishnakumar; Widener, Stanley Kevin. Injecting apparatus with reheat combustor and turbomachine. USP20181010094569.
  20. Widener, Stanley Kevin; Davis, Jr., Lewis Berkley; Foster, Gregory Thomas; Graham, Kaitlin Marie; Venkataraman, Krishnakumar. Injection systems for fuel and gas. USP20181010107498.
  21. Davis, Jr., Lewis Berkley; Foster, Gregory Thomas; Graham, Kaitlin Marie; Venkataraman, Krishnakumar; Widener, Stanley Kevin. Injector apparatus and reheat combustor. USP20181010094570.
  22. Davis, Jr., Lewis Berkley; Foster, Gregory Thomas; Graham, Kaitlin Marie; Venkataraman, Krishnakumar; Widener, Stanley Kevin. Injector apparatus with reheat combustor and turbomachine. USP20181010094571.
  23. Benz, Eribert; Flohr, Peter; Hellat, Jaan; Webb, Graham. Method for operating a gas turbine and a gas turbine for implementing the method. USP2009087574855.
  24. Benz, Eribert; Flohr, Peter; Wirsum, Manfred. Method for operating a gas turbine and a gas turbine for implementing the method. USP2009097584598.
  25. Benz, Eribert; Wirsum, Manfred. Method for operating a gas turbine and a gas turbine for implementing the method. USP2009047513118.
  26. Benz, Eribert; Wirsum, Manfred. Method for operating a gas turbine as well as a gas turbine for implementing the method. USP2009097584599.
  27. Frutschi, Hans Ulrich. Method for operating an internal combustion engine. USP2005016845738.
  28. Krakowitzer Wilhelm,CHX. Method for starting gas turbine in combined cycle power station. USP1998045737912.
  29. Fortuna, Douglas Marti; Kelsey, Mark Patrick; Rasmussen, Neil Sidney; Groeschen, James Anthony. Methods and apparatus for injecting water into gas turbine engines. USP2003076598801.
  30. Stephen R. Payling ; Robert P. Coleman ; Curtis L. Brown. Methods and apparatus for water injection in a turbine engine. USP2002106470668.
  31. Mark Stephen Rocklin ; Nicholas Damlis ; Curtis Lee Brown ; Robert Paul Coleman ; James William Stegmaier. Methods for operating gas turbine engines. USP2002116484508.
  32. Carroni, Richard. Mixer assembly. USP2010087780151.
  33. Stephen R. Payling ; Robert P. Coleman ; Curtis L. Brown. Nozzles for water injection in a turbine engine. USP2002106467252.
  34. Hein, Olaf; Minne, Michael. Temperature measuring device, gas turbine having a temperature measuring device and method for directly determining the temperature in a combustion chamber. USP2013108555651.
  35. Evulet, Andrei Tristan; Ledezma, Gustavo Adolfo; Bourassa, Corey. Trapped vortex combustor and method of operating thereof. USP2013068464538.