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Gas turbine engine catalytic and primary combustor arrangement having selective air flow control 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/228
  • F23R-003/26
  • F23R-003/40
출원번호 US-0181516 (1994-01-14)
발명자 / 주소
  • Cowell Luke H. (San Diego CA) Roberts Peter B. (Encinitas CA)
출원인 / 주소
  • Solar Turbines Incorporated (San Diego CA 02)
인용정보 피인용 횟수 : 55  인용 특허 : 0

초록 ▼

In the operation of gas turbine engines, it is an ever increasing goal to reduce the amount of harmful elements contained within the emissions of the engine. In particular, it is of primary importance to reduce the amounts of nitrogen oxides contained within the emissions. The use of a catalytic com

대표청구항 ▼

A combustor arrangement positioned within a flow of compressed air that is directed between a compressor and a turbine portion of a gas turbine engine, comprising: a housing having a first and second end portion and a first and second air passageway positioned between the end portions; a catalytic c

이 특허를 인용한 특허 (55)

  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.
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  2. Joshi, Ajay; Yee, David, Catalyst module overheating detection and methods of response.
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  3. Hellat,Jaan, Catalytic burner.
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  4. Willis Jeffrey W. (Los Angeles CA) Belmont James E. (Canoga Park CA), Catalytic combustion system.
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  5. Bland,Robert; Bandaru,Ramarao V.; Battaglioli,John, Catalytic combustion system and method.
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  6. Lipinski John J. ; Brine Philip J. ; Buch Rajesh D. ; Lester George R., Catalytic combustor for gas turbines.
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  7. Laster,Walter Ray; Bandaru,Ramarao V., Catalytic combustor having fuel flow control responsive to measured combustion parameters.
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  8. 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.
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  9. Kendrick, Donald W., Combustion cavity layouts for fuel staging in trapped vortex combustors.
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  10. Butler Philip D,GBX, Combustion chamber and a method of operation thereof.
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  11. Sattelmayer Thomas (Mandach CHX), Combustion chamber for gas turbine engine.
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  12. Willis Jeffrey D.,GBX ; Melville James,GBX, Combustion chamber with separate, valved air mixing passages for separate combustion zones.
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  13. Berry, Jonathan Dwight; Ostebee, Heath Michael, Combustor leaf seal arrangement.
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  14. Toronto, David Kaylor; Kim, Kwanwoo; Khan, Abdul Rafey; Flamand, Luis, Combustor with fuel staggering for flame holding mitigation.
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  15. Toronto, David Kaylor; Kim, Kwanwoo; Khan, Abdul Rafey; Flamand, Luis, Combustor with fuel staggering for flame holding mitigation.
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  16. Edelman, Edward C., Command and control system for controlling operational sequencing of multiple turbogenerators using a selected control mode.
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  17. Yee,David K.; Velasco,Marco A.; Nickolas,Sarento G.; Dalla Betta,Ralph A., Control strategy for flexible catalytic combustion system.
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  18. Laster, Walter R.; Bandaru, Ramarao V., Controlled pilot oxidizer for a gas turbine combustor.
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  19. Yee, David K.; Corr, II, Robert Anthony; Nickolas, Sarento George, Design and control strategy for catalytic combustion system with a wide operating range.
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  21. Peter Stuttaford CA; Stephen Oliver Oikawa CA; David Edwin Cowburn CA, Diffusion mixer.
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  22. Etemad Shahrokh ; Smith Lance L. ; Karim Hasan Ul ; Jackson Gregory Scott ; Pfefferle William C., Dry, low NO.sub.x catalytic pilot.
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  23. Yee,David K.; Reppen,Dag, Dynamic control system and method for multi-combustor catalytic gas turbine engine.
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  24. Chen, Daih-Yeou, Electric motor assisted airblast injector.
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  25. Stuttaford, Peter John; Rizkalla, Hany, Flamesheet combustor contoured liner.
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  26. Stuttaford, Peter John; Jorgensen, Stephen; Hui, Timothy; Chen, Yan; Rizkalla, Hany; Oumejjoud, Khalid, Flamesheet combustor dome.
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  28. Darling Douglas Dean ; Ryan William Richard, Gas pilot with radially displaced, high momentum fuel outlet, and method thereof.
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  30. Willis Jeffrey D,GBX, Gas turbine engine combustion chamber having premixed homogeneous combustion followed by catalytic combustion and a method of operation thereof.
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  31. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D., Gas turbine engine having a multi-stage multi-plane combustion system.
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  32. Piper, James Scott; Wang, Hongyu, Gas turbine fuel injector with a removable pilot assembly.
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  34. Oikawa, Stephen Oliver; Tang, Wei, Gas-liquid premixer.
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  35. Stephen Lan-Sun Hung ; Jeffery Alan Lovett ; Kenneth Winston Beebe ; Martin Bernard Cutrone ; Sanjay Marc Correa, Hybrid catalytic combustor.
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  37. Ul Karim, Md. Hasan; Lyle, Kent; Smith, Lance L.; Etemad, Shahrokh; Pfefferle, William C, Main burner, method and apparatus.
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  40. Dalla Betta, Ralph A.; Velasco, Marco A.; Yee, David K.; Nickolas, Sarento G., Method of thermal NOx reduction in catalytic combustion systems.
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  44. Cornwell, Michael; Milosavljevic, Vladimir Dusan, Pilot combustor for stabilizing combustion in gas turbine engines.
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  47. Stuttaford, Peter; Kojovic, Aleksandar, Swirled diffusion dump combustor.
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  48. Guillermo Pont ; James Brian Dickey ; Ed Edelman ; Mark G. Gilbreth ; Jeffrey W. Willis, System and method for modular control of a multi-fuel low emissions turbogenerator.
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  49. Borchert, Bradford David; Trout, Jesse Edwin; Simmons, Scott Robert; Valeev, Almaz; Slobodyanskiy, Ilya Aleksandrovich; Sidko, Igor Petrovich; Ginesin, Leonid Yul'evich, Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation.
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  50. Stuttaford, Peter John; Jorgensen, Stephen; Rizkalla, Hany, Thermally free liner retention mechanism.
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  54. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P., Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel.
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