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Gas turbine and gas turbine combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F23R-003/10
  • F23R-003/16
  • F23R-003/54
출원번호 US-0762598 (2001-02-09)
우선권정보 JP-0162520 (1999-06-09)
국제출원번호 PCT/JP00/03716 (2000-06-08)
국제공개번호 WO00/75573 (2000-12-14)
발명자 / 주소
  • Kawata, Yutaka
  • Mandai, Shigemi
  • Tsukuda, Yoshiaki
  • Akita, Eiji
  • Arimura, Hisato
출원인 / 주소
  • Mitsubishi Heavy Industries, Ltd.
대리인 / 주소
    Wenderoth, Lind & Ponack, L.L.P.
인용정보 피인용 횟수 : 40  인용 특허 : 7

초록

A gas turbine combustor has homogenous air inflow by elimination of turbulence from the air, reducing combustion instability. A combustor 3 has, at its center, a pilot nozzle 8 and eight main nozzles 7 around the pilot nozzle 8. The air flows in around the individual nozzles 7 and 8 to the leading e

대표청구항

A gas turbine combustor has homogenous air inflow by elimination of turbulence from the air, reducing combustion instability. A combustor 3 has, at its center, a pilot nozzle 8 and eight main nozzles 7 around the pilot nozzle 8. The air flows in around the individual nozzles 7 and 8 to the leading e

이 특허에 인용된 특허 (7)

  1. Stokes Mitchell O., Annular premix section for dry low-NO.sub.x combustors.
  2. Wuchter Gerhard (Wolfschlugen DEX), Combustion chamber for gas turbines.
  3. Lane Christopher D. (Bristol GB2) Rowe Rodney A. (Bristol GB2), Fuel combustion in ducted flow.
  4. Mandai Shigemi,JPX ; Ota Masataka,JPX ; Tanimura Satoshi,JPX ; Haruta Hideki,JPX, Gas turbine combustor.
  5. Tsukahara Satoshi,JPX ; Yoshida Shohei,JPX ; Yamagishi Masahiko,JPX ; Iwai Kazumi,JPX ; Koizumi Hiromi,JPX ; Yoshinaga Yoichi,JPX, Gas turbine combustor.
  6. Ito Kazuyuki (Hitachinaka JPX) Murakami Tadayoshi (Hitachi JPX) Kobayashi Nariyoshi (Hitachinaka JPX) Azuhata Shigeru (Hitachi JPX) Moritomo Yoshikazu (Hitachi JPX), Gas turbine combustor and gas turbine.
  7. Urushidani Haruo (Hitachi JPX) Kirikami Seiichi (Hitachi JPX) Sato Isao (Hitachi JPX) Shimizu Nobuo (Hitachi JPX) Arai Osamu (Hitachi JPX) Shimura Akira (Hitachi JPX) Kuroda Michio (Hitachi JPX) Koga, Gas turbine combustor and methodd of operating the same.

이 특허를 인용한 특허 (40)

  1. Bland, Robert J.; Battaglioli, John; Gulati, Anil; Ramier, Stephen, Air flow conditioner for a combustor can of a gas turbine engine.
  2. Stewart, Jason Thurman; Berry, Jonathan Dwight; Hughes, Michael John, Apparatus for conditioning airflow through a nozzle.
  3. Böttcher, Andreas; Krieger, Tobias; Vogtmann, Daniel; Wörz, Ulrich, Burner assembly including a fuel distribution ring with a slot and recess.
  4. Lorenz, Edmund; Niederl, Franz; Gabl, Helmuth, Combustion turbine in which combustion is intermittent.
  5. Takiguchi, Satoshi; Yuasa, Atsushi; Tanimura, Satoshi, Combustor.
  6. Tanimura, Satoshi; Kurihara, Kenta; Saitoh, Toshihiko; Rodriguez, Jose, Combustor.
  7. Tanimura, Satoshi; Kurihara, Kenta; Saitoh, Toshihiko; Rodriguez, Jose, Combustor.
  8. Tanimura, Satoshi; Kurihara, Kenta; Saitoh, Toshihiko; Rodriguez, Jose, Combustor.
  9. Tanimura, Satoshi; Kurihara, Kenta; Saitoh, Toshihiko; Rodriguez, Jose; Terada, Yoshitaka; Kamiya, Tadashi, Combustor.
  10. Mulherin, Jason; Intile, John Charles, Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement.
  11. Hirasaki, Takeo, Combustor of a gas turbine having a nozzle pipe stand.
  12. Propheter-Hinckley, Tracy A.; Santoro, Stephanie, Drill to flow mini core.
  13. Propheter-Hinckley, Tracy A; Santoro, Stephanie, Drill to flow mini core.
  14. Stuttaford, Peter John; Rizkalla, Hany, Flamesheet combustor contoured liner.
  15. Stuttaford, Peter John; Jorgensen, Stephen; Hui, Timothy; Chen, Yan; Rizkalla, Hany; Oumejjoud, Khalid, Flamesheet combustor dome.
  16. McMasters, Marie Ann; Benjamin, Michael A.; Mancini, Alfred, Fuel distributor.
  17. Tanaka,Katsunori; Yoshida,Katsuya, Fuel injection nozzle for gas turbine combustor, gas turbine combustor, and gas turbine.
  18. McMasters, Marie Ann; Benjamin, Michael A.; Mancini, Alfred; Lohmueller, Steven Joseph, Fuel nozzle.
  19. McMasters, Marie Ann; Lohmueller, Steven Joseph; Boehm, Randall Charles, Fuel nozzle.
  20. Mook, Joshua Tyler; Bellardi, Jason Joseph; Tu, Ting-Yu, Fuel nozzle with flexible support structures.
  21. Nakamura, Sosuke; Arase, Kenichi; Motoyama, Norihiko, Gas turbine and method of forming combustor insertion hole of gas turbine.
  22. Doerr,Thomas; Lazik,Waldemar, Gas turbine combustion chamber with defined fuel input for the improvement of the homogeneity of the fuel-air mixture.
  23. Moriwaki, Atsushi; Ohta, Masataka; Saitoh, Keijiro; Tanimura, Satoshi; Akamatsu, Shinji; Nagai, Norihiko, Gas turbine combustor.
  24. Saitoh, Toshihiko; Ohta, Masataka; Akamatsu, Shinji; Nose, Masakazu, Gas turbine combustor having multiple independently operable burners and staging method thereof.
  25. Wada, Yasuhiro; Sasao, Toshifumi; Saito, Takeo, Gas turbine combustor with annular flow sleeves for dividing airflow upstream of premixing passages.
  26. Hase, Matthias; Huth, Michael; Angel, Robert; Ehlert, Drew; Marshall, James; Shteyman, Yevgeniy, Gas-turbine burner.
  27. Angel, Robert; Ehlert, Drew; Hase, Matthias; Huth, Michael; Marshall, James; Shteyman, Yevgeniy, Gas-turbine burner having inflow guide means.
  28. Rackwitz, Leif; Bagchi, Imon-Kalyan; Doerr, Thomas, Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneity.
  29. Fox, Timothy A.; Schilp, Reinhard, Interface ring for gas turbine fuel nozzle assemblies.
  30. Hadley, Mark Allan, Method and apparatus for generating combustion products within a gas turbine engine.
  31. McMasters, Marie Ann; Benjamin, Michael A.; Mancini, Alfred, Method of manufacturing a unitary conduit for transporting fluids.
  32. Kastrup, David Allen; McMasters, Marie Ann, Mixer for a combustor.
  33. Stewart, Jason Thurman; Keener, Christopher Paul; Ostebee, Heath Michael, System and method for sealing a fuel nozzle.
  34. Keener, Christopher Paul; Stewart, Jason Thurman, System having a multi-tube fuel nozzle.
  35. Stewart, Jason Thurman; Keener, Christopher Paul; Ostebee, Heath Michael, System having a multi-tube fuel nozzle with a fuel nozzle housing.
  36. Keener, Christopher Paul; Stewart, Jason Thurman; Ostebee, Heath Michael, System having a multi-tube fuel nozzle with an aft plate assembly.
  37. Stewart, Jason Thurman; Keener, Christopher Paul; Ostebee, Heath Michael, System having a multi-tube fuel nozzle with an inlet flow conditioner.
  38. Stuttaford, Peter John; Jorgensen, Stephen; Rizkalla, Hany, Thermally free liner retention mechanism.
  39. Berry, Jonathan Dwight; Stewart, Jason Thurman, Turbine air flow conditioner.
  40. Stewart, Jason Thurman, Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber.
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