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Gas turbine combustor and combustion method therefor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-003/14
  • F23R-003/32
출원번호 US-0563191 (1990-08-06)
우선권정보 JP-0050060 (1987-03-05)
발명자 / 주소
  • Kuroda Michio (Hitachi JPX) Kirikami Seiichi (Hitachi JPX) Hisano Katsukuni (Hitachi JPX) Iizuka Nobuyuki (Hitachi JPX) Urushidani Haruo (Hitachi JPX) Sato Isao (Hitachi JPX) Ishibashi Yoji (Hitachi
출원인 / 주소
  • Hitachi, Ltd. (Tokyo JPX 03)
인용정보 피인용 횟수 : 55  인용 특허 : 0

초록

A gas turbine combustor comprising a head combustion chamber and a rear combustion chamber connected to a downstream side of the head combustion chamber, a first stage burner for premixing first stage fuel and air and supplying the resultant fuel and air premixture into the head combustion chamber t

대표청구항

A multistage combustion type gas turbine combustor comprising a head combustion chamber means disposed at a head of said combustor for effecting first stage premix combustion of fuel premixed with combustion air, a first stage burner disposed at an upstream side of said head combustion chamber means

이 특허를 인용한 특허 (55)

  1. Schilp, Reinhard, Air regulation for film cooling and emission control of combustion gas structure.
  2. Ziminsky, Willy Steve; Wolfe, Christopher Edward; Meshkov, Sergey Anatolievich; Oskin, Sergey Adolfovich, Apparatus and method for a combustor.
  3. Rohs, Ulrich, Axial piston engine and method for operating an axial piston engine.
  4. Karlsson, Andreas; Milosavljevic, Vladimir, Burner.
  5. Berenbrink, Peter, Burner configuration with primary and secondary pilot burners.
  6. Evulet, Andrei Tristan; Varatharajan, Balachandar; Kraemer, Gilbert Otto; ElKady, Ahmed Mostafa; Lacy, Benjamin Paul, Coanda injection system for axially staged low emission combustors.
  7. Dobbeling Klaus (Nussbaumen CHX) Knopfel Hans P. (Besenburen CHX) Sattelmayer Thomas (Mandach CHX), Combustion process for atmospheric combustion systems.
  8. Fox, Timothy A.; Wiebe, David J.; Ritland, David M.; Glessner, John Carl, Combustor apparatus in a gas turbine engine.
  9. Alkabie Hisham S,GBX, Combustor for gas- or liquid-fueled turbine.
  10. Bland, Robert; Battaglioli, John, Combustor nozzle.
  11. Melton, Patrick Benedict; Stoia, Lucas John; DiCintio, Richard Martin; Willis, Christopher Paul, Combustor support assembly for mounting a combustion module of a gas turbine.
  12. 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.
  13. Hughes, Michael John; Berry, Jonathan Dwight; Stewart, Jason Thurman; Valeev, Almaz; Wu, Chunyang, Combustor with a lean pre-nozzle fuel injection system.
  14. Melton, Patrick Benedict; Stoia, Lucas John; DiCintio, Richard Martin, Continuous combustion liner for a combustor of a gas turbine.
  15. Mowill R. Jan,NLX, Convectively cooled, single stage, fully premixed controllable fuel/air combustor.
  16. Mowill R. Jan (c/o OPRA B.V. Opaalstraat 60-P.O. Box 838 7550 AV Hengelo NLX), Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission.
  17. Melton, Patrick Benedict; Stoia, Lucas John; DiCintio, Richard Martin, Flow sleeve assembly for a combustion module of a gas turbine combustor.
  18. DiCintio, Richard Martin; Melton, Patrick Benedict; Stoia, Lucas John; Willis, Christopher Paul; Pentecost, Ronnie Ray, Flow sleeve for a combustion module of a gas turbine.
  19. Rohrssen, Robert Joseph; Cihlar, David William; Melton, Patrick Benedict; Stoia, Lucas John, Fuel delivery system with moveably attached fuel tube.
  20. Rawlins Doug C. (Murrieta CA) Smith Kenneth O. (San Diego CA), Fuel injection nozzle.
  21. Wiebe, David J.; Fox, Timothy A., Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine.
  22. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  23. Paschereit Christian Oliver,CHX ; Polifke Wolfgang,CHX ; Sattelmayer Thomas,CHX, Gas turbine combustion chamber with two stages and enhanced acoustic properties.
  24. Tsukahara Satoshi,JPX ; Yoshida Shohei,JPX ; Yamagishi Masahiko,JPX ; Iwai Kazumi,JPX ; Koizumi Hiromi,JPX ; Yoshinaga Yoichi,JPX, Gas turbine combustor.
  25. 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.
  26. 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.
  27. Mowill, R. Jan, Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities.
  28. Maeda Fukuo,JPX ; Iwai Yasunori,JPX ; Sato Yuzo,JPX, Gas turbine multi-stage combustion system.
  29. Fukuo Maeda JP; Yasunori Iwai JP; Yuzo Sato JP, Gas turbine staged control method.
  30. DiCintio, Richard Martin; Chen, Wei, Hot gas path duct for a combustor of a gas turbine.
  31. Oskam, Gareth W., Lean direct fuel injector.
  32. Frank J. Zupanc ; Rudolph Dudebout ; John J. Lipinski ; Ram Srinivasan, Low cost, low emissions natural gas combustor.
  33. Sjunnesson Anders,SEX ; Johansson Patrik,SEX ; Andersson Alf,SEX ; Lundgren Sonny,SEX ; Gabrielsson Rolf,SEX, Low-emission combustion chamber for gas turbine engines.
  34. Ul Karim, Md. Hasan; Lyle, Kent; Smith, Lance L.; Etemad, Shahrokh; Pfefferle, William C, Main burner, method and apparatus.
  35. Oskam, Gareth W., Method of operating a gas turbine engine.
  36. Myers, Geoffrey David; Snider, David August; Motter, Eric; Tegel, Daniel R.; Harper, James; Watts, Stephen R.; Citeno, Joseph, Methods and systems for operating gas turbine engines.
  37. Van Blaricom, Terry Michael, Open-cycle internal combustion engine.
  38. Van Blaricom, Terry Michael, Open-cycle internal combustion engine.
  39. Joshi Mahendra L. ; Fournier ; Jr. Donald J. ; Tester Marvin E., Oxygen-fuel boost reformer process and apparatus.
  40. Mowill R. Jan,NLX, Premixer with dilution air bypass valve assembly.
  41. Beebe Kenneth W., Premixing dry low NOx emissions combustor with lean direct injection of gas fuel.
  42. Beebe Kenneth W., Premixing dry low nox emissions combustor with lean direct injection of gas fule.
  43. Toon, Ian J.; O'Dell, Stephen J.; Currin, John H.; Willis, Jeffrey D., Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection.
  44. Mowill R. Jan (OPRA B.V. Opaalstraat 60 ; P.O. Box 838 7550 AV Hengelo NLX), Star combustor with dilution ports in can portions.
  45. Stoia, Lucas John; DiCintio, Richard Martin; Poschel, William Michael; Melton, Patrick Benedict, Support frame and method for assembly of a combustion module of a gas turbine.
  46. Stuttaford, Peter; Kojovic, Aleksandar, Swirled diffusion dump combustor.
  47. Antoniono, Carolyn Ashley; Byrne, William Lawrence; Fadde, Elizabeth Angelyn, System and method for a turbine combustor.
  48. Huntington, Richard A.; Dhanuka, Sulabh K.; Slobodyanskiy, Ilya Aleksandrovich, System and method for diffusion combustion with oxidant-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system.
  49. DiCintio, Richard Martin; Melton, Patrick Benedict; Stoia, Lucas John; Willis, Christopher Paul, System for providing fuel to a combustor.
  50. Borkowicz Richard J. (Westminster MD) Davis ; Jr. L. Berkley (Schenectady NY) Kuwata Masayoshi (Ballston Lake NY), Tertiary fuel, injection system for use in a dry low NOx combustion system.
  51. Haynes, Joel Meier, Turbine containing system and an injector therefor.
  52. Ritland, David M., Turbine engine flow sleeve.
  53. Callas, James J.; White, David J., Turbine engine having folded annular jet combustor.
  54. Hallit, Raymond I., Variable firing rate fuel burner.
  55. Grienche Guy,FRX ; Schott Gerard,FRX ; Le Gal Jean-Herve,FRX ; Martin Gerard,FRX ; Laborde Patrice,FRX ; Spagna Raphael,FRX, Variable-throat gas-turbine combustion chamber.
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