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Gas turbine combustor 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/26
  • F02C-003/22
출원번호 US-0391312 (1989-08-09)
우선권정보 JP-0202789 (1988-08-16); JP-0033811 (1989-02-15)
발명자 / 주소
  • Yamanaka Susumu (Kawasaki) Furuya Tomiaki (Yokohama) Hayata Terunobu (Kawasaki) Koezuka Junji (Yokohama) Tanemura Katsuhei (Ichikawa) Ohkoshi Akio (Abiko) Hara Yukiyoshi (Ageo) Tominaga Hitoshi (Yoko
출원인 / 주소
  • Kabushiki Kaisha Toshiba (Kawasaki JPX 03) The Tokyo Electric Power Co., Inc. (Tokyo JPX 03)
인용정보 피인용 횟수 : 53  인용 특허 : 5

초록

A gas turbine combustor includes a main body with a combustion portion into which mixture of fuel and air is supplied. The gas mixture is burned through a catalytic reaction at a catalyst body arranged in the main body. The gas mixture passed through the catalyst body is introduced into a gas phase

대표청구항

A gas turbine combustor comprising: a main body having a combustion chamber formed therein; gas supply means for supplying a gas mixture of fuel and gas including oxide to the combustion chamber; igniting means for igniting the gas mixture; catalyst means arranged in the main body on the downstream

이 특허에 인용된 특허 (5)

  1. Roffe Gerald A. (3 Markwood La. East Northport NY 11731) Trucco Horacio A. (13 Saddler Ct. Huntington Station NY 11746), Apparatus for the premixed gas phase combustion of liquid fuels.
  2. Flanagan Paul (Princeton NJ), Combustion method and apparatus.
  3. Beebe Kenneth W. (Galway NY), Multiple venturi tube gas fuel injector for catalytic combustor.
  4. Furuya Tomiaki (Yokohama JPX) Yamanaka Susumu (Yokohama JPX) Hayata Terunobu (Kawasaki JPX) Koezuka Junji (Yokohama JPX), Nitrogen oxides decreasing combustion method.
  5. DeCorso Serafino M. (Media PA) Pillsbury Paul W. (Wallingford PA), Wide range catalytic combustor.

이 특허를 인용한 특허 (53)

  1. Farhangi,Shahram; Sprouse,Kenneth M; Matthews,David R, Apparatus for mixing fluids.
  2. Collmer, Andreas; Kouril, Axel; Grotstollen, Uwe; Bendix, Lars; Roppelt, Oliver; Heim, Marcus, Bottom assembly unit for a combustion chamber assembly unit of a vaporizing burner.
  3. Pfister, Wolfgang; Blaschke, Walter; Hermann, Valerij, Bottom assembly unit for a combustion chamber assembly unit of a vaporizing burner.
  4. Lacy, Benjamin Paul; Ziminsky, Willy Steve; Johnson, Thomas Edward; Zuo, Baifang; York, William David; Uhm, Jong Ho, Bundled multi-tube nozzle for a turbomachine.
  5. Von Arx,Alan V.; Horn,Mark D., Cascade ignition of catalytic combustors.
  6. Hellat,Jaan, Catalytic burner.
  7. Willis Jeffrey W. (Los Angeles CA) Belmont James E. (Canoga Park CA), Catalytic combustion system.
  8. Sprouse,Kenneth M; Farhangi,Shahram; Moriarty,Michael P; Matthews,David R, Catalytic combustor and method for substantially eliminating various emissions.
  9. Lipinski John J. ; Brine Philip J. ; Buch Rajesh D. ; Lester George R., Catalytic combustor for gas turbines.
  10. Laster,Walter Ray; Bandaru,Ramarao V., Catalytic combustor having fuel flow control responsive to measured combustion parameters.
  11. Beebe Kenneth W. ; Hung Stephen L. ; Cutrone Martin B., Catalytic combustor with lean direct injection of gas fuel for low emissions combustion and methods of operation.
  12. Bruck,Gerald J.; Laster,Walter R., Concentric catalytic combustor.
  13. Yee,David K.; Velasco,Marco A.; Nickolas,Sarento G.; Dalla Betta,Ralph A., Control strategy for flexible catalytic combustion system.
  14. Hamrin, Douglas; Lampe, Steve, Controls for multi-combustor turbine.
  15. Lovett Jeffery Allan ; Goebel Steven George, Dynamically uncoupled low nox combustor with axial fuel staging in premixers.
  16. Prabhu, Edan, Fuel oxidation in a gas turbine system.
  17. Beebe, Kenneth W.; Davis, L. Berkly; Iasillo, Robert J., Fuel trim method for a multiple chamber gas turbine combustion system.
  18. Oskam, Gareth W., Gas turbine and fuel injector for the same.
  19. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D., Gas turbine engine having a multi-stage multi-plane combustion system.
  20. Maslov, Boris A., Gradual oxidation and autoignition temperature controls.
  21. Maslov, Boris A., Gradual oxidation and autoignition temperature controls.
  22. Maslov, Boris A., Gradual oxidation and multiple flow paths.
  23. Armstrong, Jeffrey, Gradual oxidation below flameout temperature.
  24. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas, Gradual oxidation with adiabatic temperature above flameout temperature.
  25. Maslov, Boris A.; Armstrong, Jeffrey, Gradual oxidation with flue gas.
  26. Watts, Jim, Gradual oxidation with gradual oxidizer warmer.
  27. Hamrin, Douglas; Armstrong, Jeffrey, Gradual oxidation with heat control.
  28. Lampe, Steve; Hamrin, Douglas, Gradual oxidation with heat control.
  29. Lampe, Steve; Hamrin, Douglas, Gradual oxidation with heat control.
  30. Lampe, Steve; Hamrin, Douglas, Gradual oxidation with heat control.
  31. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas, Gradual oxidation with heat transfer.
  32. Armstrong, Jeffrey; Maslov, Boris A., Gradual oxidation with heat transfer.
  33. Hamrin, Douglas; Martin, Richard; Armstrong, Jeffrey, Gradual oxidation with heat transfer.
  34. Sisco, James Charles; Kerrebrock, Jack; Hollman, Jeremy Scott, High altitude combustion system.
  35. Stephen Lan-Sun Hung ; Jeffery Alan Lovett ; Kenneth Winston Beebe ; Martin Bernard Cutrone ; Sanjay Marc Correa, Hybrid catalytic combustor.
  36. Martin, Richard; Armstrong, Jeffrey; Hamrin, Douglas, Hybrid gradual oxidation.
  37. Davis, Jr., Lewis Berkley; Ziminsky, Willy Steve; McMahan, Kevin Weston; Chila, Ronald James; Meshkov, Sergey Anatolievich, Integrated combustor and stage 1 nozzle in a gas turbine and method.
  38. Oskam, Gareth W., Lean direct fuel injector.
  39. Davis, Jr., Lewis Berkley; Johnson, Thomas Edward; Stewart, Jason Thurman, Method and apparatus for delivery of a fuel and combustion air mixture to a gas turbine engine using fuel distribution grooves in a manifold disk with discrete air passages.
  40. Farhangi,Shahram, Method and apparatus for injecting a fuel into a combustor assembly.
  41. Oskam, Gareth W., Method of operating a gas turbine engine.
  42. Hamrin, Douglas; Lampe, Steve, Multi-combustor turbine.
  43. Chen,Alexander G.; Kendrick,Donald W., Multi-point staging strategy for low emission and stable combustion.
  44. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr., Multi-stage multi-plane combustion system for a gas turbine engine.
  45. Sprouse,Kenneth M.; Farhangi,Shahram; Horn,Mark D.; Matthews,David R., Non-swirl dry low NOx (DLN) combustor.
  46. Prabhu, Edan, Oxidizing fuel in multiple operating modes.
  47. Ziminsky, Willy Steve; Johnson, Thomas Edward; Lacy, Benjamin Paul; York, William David; Uhm, Jong Ho; Zuo, Baifang, Premixed direct injection nozzle for highly reactive fuels.
  48. Wolflick John R. ; Beer Gary L. ; Payne Richard L., Process for converting gas to liquids.
  49. Armstrong, Jeffrey; Martin, Richard; Hamrin, Douglas, Staged gradual oxidation.
  50. Agee Mark A. ; Weick Larry J., System and method for converting light hydrocarbons to heavier hydrocarbons with separation of water into oxygen and hydrogen.
  51. O'Beck, John T.; Tendick, Rex C., System and method for treatment of water and disposal of contaminants produced by converting lighter hydrocarbons into heavier hydrocarbon.
  52. Agee Mark A. ; Weick Larry J., System for converting light hydrocarbons to heavier hydrocarbons with separation of water into oxygen and hydrogen.
  53. Stoia, Lucas John; Melton, Patrick Benedict; Johnson, Thomas Edward; Stevenson, Christian Xavier; Vanselow, John Drake; Westmoreland, James Harold, Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same.
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