이 특허를 인용한 특허 (44)

1. Wang, Shanwu; Han, Fei; Mueller, Mark Anthony, Acoustic damping device for use in gas turbine engine.

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2. Portillo Bilbao, Juan Enrique; Rajaram, Rajesh; You, Danning; Spence, Kevin M., Acoustic damping system for a combustor of a gas turbine engine.

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3. Liu, Zheji, Acoustic liner and a fluid pressurizing device and method utilizing same.

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4. Kim, Kwanwoo; Han, Fei; Jain, Praveen; Narra, Venkat; Bethke, Sven Georg, Acoustic resonator located at flow sleeve of gas turbine combustor.

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5. Wasif,Samer P.; Johnson,Clifford E., Acoustic resonator with impingement cooling tubes.

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6. Slobodyanskiy, Ilya; Lipinski, John; Srinivasan, Shiva; Tretyakov, Dmitry, Acoustically stiffened gas turbine combustor supply.

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7. Alkabie,Hisham, Aerodynamic trip for a combustion system.

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8. Genin, Franklin Marie; Aluri, Naresh; Bothien, Mirko Ruben, Annular helmholtz damper.

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9. Dobbeling Klaus,CHX ; Paschereit Christian,CHX ; Polifke Wolfgang,CHX, Arrangement for damping combustion-chamber oscillations.

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10. Flohr,Patrick; Krebs,Werner; Schulze,G��nther, Burner, method for operating a burner and gas turbine.

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11. Huth, Michael; Tiemann, Peter; Oltmanns, legal representative, Iris, Combustion chamber.

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12. Jakob Keller CH; Georg Keller CH; Vera Keller CH, Combustion chamber for a gas turbine.

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13. Macquisten, Michael A; Moran, Anthony J; Whiteman, Michael; Carrotte, Jonathan F; Barker, Ashley G, Combustion chamber for a gas turbine engine.

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14. Macquisten,Michael A; Moran,Anthony J; Whiteman,Michael; Carrotte,Jonathan F; Barker,Ashley G; Goodwin,Martin S, Combustion chamber for a gas turbine engine.

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15. Schnell, Alexander; Noiray, Nicolas; Reinert, Felix; Lauffer, Diane; Schuermans, Bruno, Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators.

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16. Huber, Andreas; Noiray, Nicolas; Benz, Urs; Reinert, Felix; Lauffer, Diane, Combustion device with a layered wall structure for a gas turbine.

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17. Johnson, Thomas Edward; Brown, James Thomas, Combustion turbine engine and methods of assembly.

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18. Bobba, Mohan Krishna; Kim, Kwanwoo; Melton, Patrick Benedict; Antoniono, Carolyn Ashley, Combustor resonator with non-uniform resonator passages.

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19. Marcel Stalder CH; Franz Joos DE, Damping device for reducing the vibration amplitude of acoustic waves for a burner.

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20. Liu, Zheji, Double layer acoustic liner and a fluid pressurizing device and method utilizing same.

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21. Han, Fei; Dinc, Osman Saim; Mohammed-Fakir, Abdul-Azeez; Kim, Sung Jin, Dynamically uncoupled can combustor.

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22. Lovett Jeffery Allan ; Goebel Steven George, Dynamically uncoupled low NOx combustor having multiple premixers with axial staging.

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23. Lovett Jeffery Allan ; Goebel Steven George, Dynamically uncoupled low nox combustor with axial fuel staging in premixers.

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24. Kudernatsch, Gunter, Exhaust gas system with helmholtz resonator.

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25. Gambacorta, Domenico; Johnson, Clifford E., Forward-section resonator for high frequency dynamic damping.

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26. Liu, Zheji, Gas compression apparatus and method with noise attenuation.

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27. Flohr,Patrick; Krebs,Werner; Prade,Bernd, Gas turbine.

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28. Ono, Masaki; Nishimura, Masaharu; Ohnishi, Keizo; Ikeda, Kazufumi; Tanaka, Katsunori, Gas turbine combustion device.

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29. Genin, Franklin Marie; Aluri, Naresh; Cerny, Jan; Eroglu, Adnan; Pasqualotto, Ennio, Gas turbine combustion system.

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30. Ohnishi, Keizo; Ikeda, Kazufumi; Ono, Masaki; Nishimura, Masaharu; Tanaka, Katsunori, Gas turbine combustor having an acoustic energy absorbing wall.

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31. Johnson, Thomas Edward; Ziminsky, Willy Steve; York, William David; Stevenson, Christian Xavier, Injector with integrated resonator.

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32. Hoffmann Stefan,DEX ; Berenbrink Peter,DEX ; Judith Hans,DEX, Method and device for burning fuel with air.

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33. Carrea,Elisabetta; Jansohn,Peter, Method for combustion of a fuel.

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34. Sattinger, Stanley S., Method of suppressing combustion instabilities using a resonator adopting counter-bored holes.

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35. Liu, Zheji, Multi-degree of freedom resonator array.

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36. Sattinger,Stanley S., Resonator adopting counter-bored holes and method of suppressing combustion instabilities.

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37. Davis, Jr., Lewis Berkley; Han, Fei; Srinivasan, Shiva; Singh, Kapil Kumar; Kim, Kwanwoo; Narra, Venkateswarlu, Resonator assembly for mitigating dynamics in gas turbines.

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38. Johnson, Clifford E.; Wasif, Samer P., Resonator device at junction of combustor and combustion chamber.

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39. Tobik,Steven E.; Sattinger,Stanley S.; Ohri,Rajeev; Koenig,Michael H., Resonator performance by local reduction of component thickness.

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40. Antoniono, Carolyn Ashley; Byrne, William Lawrence; Fadde, Elizabeth Angelyn, System and method for a turbine combustor.

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41. Kim, Kwanwoo; Narra, Venkateswarlu; Jain, Praveen Kumar Babulal; Bethke, Sven Georg, System for damping oscillations in a turbine combustor.

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42. Boardman, Gregory Allen; Chila, Ronald James; Hadley, Mark Allan; McConnaughhay, Johnie Franklin; Crothers, Sarah Lori, Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor having multiple premix times.

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43. Bagnall, Adam MacGregor; Lockwood, Clive, Temperature controlling apparatus.

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44. Park, Roger James, Turbine engine fuel injector with helmholtz resonators.

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