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특허 상세정보

Gas turbine combustor and gas turbine generating apparatus

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/50   
미국특허분류(USC) 60/3923 ; 60/3927 ; 60/747
출원번호 US-0010576 (1993-01-28)
우선권정보 JP-0013685 (1992-01-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 25  인용 특허 : 0
초록

A gas turbine combustor is capable of reducing NOx over a whole load range of a gas turbine. The combustor comprises two burner systems. It is possible to independently control a flow rate of combustion air supplied to a burner of the respective systems and a flow rate of bypass air jetted from through a bypass air port. The air supplied to the burners is mixed with fuel in a mixing chamber and then ejected into a combustion chamber so as to form a flame. The amount of bypass air is controlled in accordance with an operation load, a humidity of air and a...

대표
청구항

A gas turbine combustor comprising: a combustion chamber; pilot burner means of a premixed flame burner type disposed in said combustion chamber, said premixed flame burner means being constructed such that fuel and air are premixed prior to combustion; main burner means of a premixed flame burner type disposed so as to surround said pilot burner means, said main burner means being constructed such that fuel and air are premixed prior to combustion; bypass air port means; means for supplying fuel to said pilot burner means and said main burner means; fir...

이 특허를 인용한 특허 피인용횟수: 25

  1. Mowill,R. Jan. Apparatus and method for gas turbine engine fuel/air premixer exit velocity control. USP2007017162874.
  2. Chandler, Christopher. Automated tuning of gas turbine combustion systems. USP2013058437941.
  3. Chandler, Christopher. Automated tuning of gas turbine combustion systems. USP2016029267443.
  4. Chandler, Christopher. Automated tuning of gas turbine combustion systems. USP2016059328670.
  5. Chandler, Christopher. Automated tuning of gas turbine combustion systems. USP20190410260428.
  6. Chandler, Christopher. Automated tuning of multiple fuel gas turbine combustion systems. USP2016059354618.
  7. Wasif, Samer P.; Meisl, Juergen; Janus, Bertram; Koch, Andreas. Can annular combustion arrangement with flow tripping device. USP2016039297532.
  8. Mittricker, Franklin F.; O'Dea, Dennis M.; Deckman, Harry W.; Rasmussen, Chad C.; Noble, David R.; Seitzman, Jerry M.; Lieuwen, Timothy C.; Dhanuka, Sulabh K.; Huntington, Richard. Combustor systems and combustion burners for combusting a fuel. USP2016059353940.
  9. Zuo, Baifang. Fuel/air premixing system for turbine engine. USP2015018925323.
  10. Brunhuber, Christian; Hirschfelder, Oliver; Lenk, Uwe; Menapace, Wolfgang; Vortmeyer, Nicolas. Gas power plant. USP2016059341114.
  11. Inoue, Kei; Saito, Keijiro; Matsumura, Yoshikazu; Nakamura, Sosuke. Gas turbine combustor. USP2017109791149.
  12. Inoue, Kei; Saito, Keijiro; Matsumura, Yoshikazu; Nakamura, Sosuke. Gas turbine combustor. USP2017049612013.
  13. Inoue, Kei; Saito, Keijiro; Matsumura, Yoshikazu; Nakamura, Sosuke. Gas turbine combustor. USP2014088794004.
  14. Mandai Shigemi,JPX ; Kawabata Hitoshi,JPX ; Nishida Koichi,JPX. Gas turbine combustor having multiple burner groups and independently operable pilot fuel injection systems. USP1999055901555.
  15. Saitoh, Toshihiko; Ohta, Masataka; Akamatsu, Shinji; Nose, Masakazu. Gas turbine combustor having multiple independently operable burners and staging method thereof. USP2010097797942.
  16. Inoue, Hiroshi; Koganezawa, Tomomi; Kobayashi, Nariyoshi; Ohtsuka, Masaya; Ito, Kazuyuki; Takehara, Isao. Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low NOx combustion. USP2004076761033.
  17. Inoue, Hiroshi; Koganezawa, Tomomi; Kobayashi, Nariyoshi; Ohtsuka, Masaya; Ito, Kazuyuki; Takehara, Isao. Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low nox combustion. USP2005036871503.
  18. Ryan, William R.. Gas turbine pilot burner and method. USP2003126666029.
  19. Chandler, Christopher. Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications. USP2017069671797.
  20. Amos David J. ; Stokes Mitchell O.. Pilot cones for dry low-NO.sub.x combustors. USP2000096122916.
  21. Duesing, Michael; Freitag, Ewald. Sequential combustion arrangement with dilution gas. USP20181210151487.
  22. Lee,Byeong Jun; Kim,Jin Hyun. Simultaneous combustion with premixed and non-premixed fuels and fuel injector for such combustion. USP2006087093444.
  23. Ito Kazuyuki,JPX ; Murakami Tadayoshi,JPX ; Kawaike Kazuhiko,JPX ; Azuhata Shigeru,JPX ; Kuroda Michio,JPX. Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer. USP2000026026644.
  24. Miyake,Yoshiaki; Nakae,Tomoyoshi. System and method for controlling combustion in gas turbine with annular combustor. USP2006047024862.
  25. McMahan, Kevin Weston; Johnson, Thomas Edward; Widener, Stanley Kevin. Systems and methods for reintroducing gas turbine combustion bypass flow. USP2012108281601.