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Dual fuel nozzle 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-001/00
출원번호 US-0470592 (1999-12-22)
우선권정보 JP-0367255 (1998-12-24)
발명자 / 주소
  • Shigemi Mandai JP
  • Masataka Ohta JP
  • Kazuya Kobayashi JP
  • Koichi Nishida JP
출원인 / 주소
  • Mitsubishi Heavy Industries, Ltd. JP
대리인 / 주소
    Christie, Parker & Hale, LLP
인용정보 피인용 횟수 : 49  인용 특허 : 6

초록

A dual fuel nozzle is provided with two different size injection holes. The first injection holes have larger diameters and are used only for injecting gaseous fuel into a combustion chamber. On the other hand, the second injection nozzles have smaller diameters and are used for injecting either gas

대표청구항

1. A method for operating a dual fuel nozzle to inject gaseous fuel and/or liquid fuel into a combustion chamber, the fuel nozzle being provided with a first injection hole and a second injection hole for injecting fuel therefrom, the second injection hole having a diameter smaller than the first in

이 특허에 인용된 특허 (6)

  1. Becker Bernard (Mlheim DEX), Burner configuration, particularly for gas turbines, for the low-pollutant combustion of coal gas and other fuels.
  2. Cohen Mitchell ; Kuwata Masayoshi ; Steber Charles E. ; Mick Warren J., Center burner in a multi-burner combustor.
  3. Leonard Gary L. (Cincinnati OH), Flashback resistant fuel staged premixed combustor.
  4. Beaudoin Ronald J. (Schenectady NY), Fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation.
  5. Donlan John P. (Oviedo FL), Gas turbine dual fuel nozzle assembly with steam injection capability.
  6. Hoffeins Hans (Viernheim DEX) Kalbfuss Richard (Mannheim DEX) Ipek Bora (Weinheim DEX), Multifuel burner.

이 특허를 인용한 특허 (49)

  1. Mendoza, Robert Eleazar; Morrison, Paul Elliot; Leon, Marco Ezra; Bognuda, Tiziano Marco; Ito, Satoshi; Turner, legal representative, Shari, Active combustion control for a turbine engine.
  2. Parsania, Nishant Govindbhai; Myers, Geoffrey D.; Boardman, Gregory Allen, Axial flow fuel nozzle with a stepped center body.
  3. Kendrick, Donald W., Combustion cavity layouts for fuel staging in trapped vortex combustors.
  4. Khan, Abdul Rafey; Stevenson, Christian Xavier; Zuo, Baifang, Dual fuel combustor nozzle for a turbomachine.
  5. Gerhold, Bruce W., Dual fuel power generation system.
  6. Gerhold, Bruce W., Dual fuel power generation system.
  7. Khan, Abdul Rafey; Ziminsky, Willy Steve, Fuel flexible combustor systems and methods.
  8. Toon, Ian J; Eadon, Gary; Graham, Andrew C; Salt, Allan J, Fuel injection.
  9. Toon,Ian J; Eadon,Gary; Graham,Andrew C; Salt,Allan J, Fuel injection.
  10. Cavanagh,Mark S.; Urven, Jr.,Roger L.; Lawrence,Keith E., Fuel injector nozzle for an internal combustion engine.
  11. Cavanagh,Mark S.; Urven, Jr.,Roger L.; Lawrence,Keith E., Fuel injector nozzle for an internal combustion engine.
  12. Cavanagh,Mark S.; Urven, Jr.,Roger L.; Lawrence,Keith E., Fuel injector nozzle for an internal combustion engine.
  13. Gillis, Edward R.; Coldren, Dana R.; Ellenbecker, Charles D., Fuel injector with directly controlled dual concentric check and engine using same.
  14. Lueck, Rudolf; Giugno, Dominik; Otterbach, Christian, Fuel supply system for a gas-turbine engine.
  15. Bonzani, Federico; Pollarolo, Giacomo, Gas turbine burner.
  16. Popovic, Predrag; Baruah, Abinash; Kraemer, Gilbert Otto; Ross, William Thomas, Gas turbine combustor having a fuel nozzle for flame anchoring.
  17. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with a removable pilot assembly.
  18. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with removable pilot liquid tube.
  19. Rebhan, Dieter; Stalder, Marcel, Gas turbine system for injecting a mixture of high value hydrocarbons plural distinct fuels into the gas turbine combustion chamber.
  20. Payne, David C., Hydrocabon cracking furnace with steam addition to lower mono-nitrogen oxide emissions.
  21. von Schweinitz, Horst Graf; Munko, Andreas, Industrial burner and method for operating an industrial burner.
  22. Kendrick, Donald W., Inlet premixer for combustion apparatus.
  23. Barton, Jesse Ellis; Berry, Jonathan Dwight; Hadley, Mark Allan; Nelson, Glenn David; Rohrssen, Robert Joseph; Vanselow, John Drake, Method and apparatus for introducing diluent flow into a combustor.
  24. Barton, Jesse Ellis; Berry, Jonathan Dwight; Hadley, Mark Allan; Melton, Patrick Benedict, Method and apparatus of introducing diluent flow into a combustor.
  25. Rebhan,Dieter; Stalder,Marcel, Method for operating a gas turbine and gas turbine system for carrying out the method.
  26. Cerny,Jan; Jhalani,Anurag, Method for operating a gas turbine combustion chamber including a plurality of burners arranged in groups.
  27. Deuker, Eberhard; Kostlin, Berthold; Meisl, Jurgen; Nehlsen, Dennis; Schildmacher, Kai-Uwe, Method for running up a stationary gas turbine.
  28. Bothien, Mirko Ruben; Zajadatz, Martin; Pennell, Douglas Anthony, Method for switching over a combustion device between a first fuel and a second fuel.
  29. Kendrick, Donald W., Method of fuel staging in combustion apparatus.
  30. Durbin, Mark D.; Danis, Allen Michael; Held, Timothy James; Durstock, Daniel; Cooper, James N.; Fortuna, Douglas Marti, Methods and apparatus for injecting fluids into a turbine engine.
  31. Durbin, Mark; Danis, Allen M.; Held, Timothy J.; Cooper, James N.; Fortuna, Douglas Marti; Durstock, Daniel, Methods and apparatus for injecting fluids into a turbine engine.
  32. Fortuna,Douglas Marti; Held,Timothy James; Kastrup,David Allen, Methods and apparatus for reducing gas turbine engine emissions.
  33. Durbin, Mark David; Mongia, Hukam Chand, Multiple injector combustor.
  34. Mao, Chien-Pei; Short, John Earl; Thomson, Neal A., Multiplex injector.
  35. Oskooei, Saeid, Nozzle design to reduce fretting.
  36. Oskooei, Saeid, Nozzle design to reduce fretting.
  37. Oskooei, Saeid; Hope, Nicholas, Nozzle repair to reduce fretting.
  38. Ohta, Masataka; Aoyama, Kuniaki; Inada, Mitsuru; Mandai, Shigemi; Tanimura, Satoshi; Tanaka, Katsunori; Nishida, Koichi, Pilot nozzle of gas turbine combustor.
  39. Van Liere, Jacobus, Power generating system comprising a combustion unit that includes an explosion atomizing unit for combusting a liquid fuel.
  40. Prabhu, Edan D., Processing fuel and water.
  41. 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.
  42. Thompson, Brett Matthew, System for fuel and diluent control.
  43. Zhang, Hua; Hu, Tailai; Todeti, Sudhakar; Selfridge, Kenneth Eugene, System for turbine combustor fuel mixing.
  44. Zhang, Hua; Hu, Tailai; Todeti, Sudhakar; Selfridge, Kenneth Eugene, System for turbine combustor fuel mixing.
  45. Cowan, Curtis C., Turbine engine combustor.
  46. Cowan, Curtis C., Turbine engine fuel injector.
  47. Cowan, Curtis C., Turbine engine fuel injector.
  48. Wasif, Samer P., Utilizing a diluent to lower combustion instabilities in a gas turbine engine.
  49. Kendrick, Donald W., Vortex premixer for combustion apparatus.
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