이 특허를 인용한 특허 (24)

1. Siewert, Piotr; Lachner, Rudolf, Combustion chamber and method for damping pulsations.

   상세보기
2. Peter Senior BE; Sebastian Maidhof IT, Combustor arrangement.

   상세보기
3. Flohr,Peter; Schuermans,Bruno; Toqan,Majed, Combustor for a gas turbine.

   상세보기
4. Nichols, Richard Lee; Norman, Bruce G.; Elward, Kevin Michael; Pavri, Roointon Erach; Rush, Benjamin; Boettner, Robert Edward; VanDevelde, John P., Control of gas turbine combustion temperature by compressor bleed air.

   상세보기
5. Hawie, Eduardo David; Davenport, Nigel Caldwell; Zhou, Jian-Ming, Fluid manifold for gas turbine engine and method for delivering fuel to a combustor using same.

   상세보기
6. Patel, Nayan Vinodbhai; Mancini, Alfred Albert; Thomsen, Duane Douglas, Fuel supply system for a gas turbine engine.

   상세보기
7. Komatsu Yasutaka,JPX ; Urushidani Haruo,JPX ; Azuhata Shigeru,JPX ; Iizuka Nobuyuki,JPX ; Watanabe Yasuyuki,JPX ; Arai Hiroyuki,JPX ; Kobayashi Nariyoshi,JPX ; Ohtsuka Masaya,JPX ; Ito Kazuyuki,JPX, Gas turbine combustor and operation method thereof for a diffussion burner and surrounding premixing burners separated b.

   상세보기
8. Danis, Allen Michael; Mueller, Mark Anthony; Held, Timothy James; Marakovits, Steven, Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities.

   상세보기
9. Corsmeier, Donald Michael; Noe, Mark Eugene; Radwanski, Michael Todd; Roghe, Oliver; Subit, Jessica Licardi; Xie, Ming, Gas turbine engine combustor with CMC heat shield and methods therefor.

   상세보기
10. Corsmeier, Donald Michael; Noe, Mark Eugene; Radwanski, Michael Todd; Roghe, Oliver; Subit, Jessica Licardi; Xie, Ming, Gas turbine engine combustor with CMC heat shield and methods therefor.

    상세보기
11. Von Der Bank, Ralf Sebastian, Lean premix burner for a gas turbine and operating method for a lean premix burner.

    상세보기
12. Widener, Stanley Kevin, Low-cost dual-fuel combustor and related method.

    상세보기
13. 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.

    상세보기
14. Cerny,Jan; Jhalani,Anurag, Method for operating a gas turbine combustion chamber including a plurality of burners arranged in groups.

    상세보기
15. Stalder, Marcel; Rebhan, Dieter; Kueenzi, Thomas; Knoepfel, Hans Peter, Method for running up a gas turbine plant.

    상세보기
16. Kawai, Ryo; Murata, Hidetaro; Saito, Takeo; Kizuka, Nobuaki; Nanataki, Kenji, Method for starting premixed combustion in combustor for two-shaft gas turbine.

    상세보기
17. Hermann Jakob,DEX ; Hantschk Carl-Christian,DEX ; Zangl Peter,DEX ; Vortmeyer Dieter,DEX ; Orthmann Armin,DEX, Method for the active damping of combustion oscillation and combustion apparatus.

    상세보기
18. Stuttaford,Peter; Margarit Bel,Nuria; Chen,Yan; Oumejjoud,Khalid; Jennings,Stephen, Method of operating a combustion system for increased turndown capability.

    상세보기
19. Gerhard Muller DE; Frank Reiss DE; Pirmin Schiessel CH; Stefan Tschirren CH, Method of operating a gas-turbine chamber with gaseous fuel.

    상세보기
20. Chen, Alexander G.; Kendrick, Donald W., Multi-point staging strategy for low emission and stable combustion.

    상세보기
21. Chen,Alexander G.; Kendrick,Donald W., Multi-point staging strategy for low emission and stable combustion.

    상세보기
22. Chen,Alexander G.; Kendrick,Donald W., Multi-point staging strategy for low emission and stable combustion.

    상세보기
23. Flohr, Peter; Motz, Christian Joerg; Toqan, Majed; Zajadatz, Martin, Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement.

    상세보기
24. Johnson, Thomas Edward; Mordaunt, Christopher, Universal multi-nozzle combustion system and method.

    상세보기
더보기