이 특허를 인용한 특허 (53)

1. Bes,Martine; Hernandez,Didier; Lepretre,Gilles; Trahot,Denis, Annular combustion chamber for a turbomachine with an improved inner fastening flange.

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2. Farmer, Gilbert; Devane, Shaun M.; Vandike, John L., Annular one-piece corrugated liner for combustor of a gas turbine engine.

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3. Bulman, David Edward; Darkins, Jr., Toby George; Schroder, Mark Stewart; Lipinski, John Joseph, Bolting configuration for joining ceramic combustor liner to metal mounting attachments.

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4. Gerendas,Miklos; Ebel,Michael, Combustion chamber of gas turbine with starter film cooling.

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5. Fitzpatrick, Erich Robert; Stieg, Michael Alan; Kenoyer, Kimberly Lynne Christman, Combustion liner for use in a combustor assembly and method of manufacturing.

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6. Stastny,Honza; Sze,Robert, Combustor exit duct.

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7. Stastny, Honza; Verhiel, Jeffrey Richard; Sampath, Parthasarathy, Combustor for gas turbine engine.

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8. Stastny, Honza; Verhiel, Jeffrey; Sampath, Parthasarathy, Combustor for gas turbine engine.

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9. Patel, Bhawan Bhai; Sampath, Parthasarathy; Fish, Jason Araan, Combustor liner V-band design.

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10. Tariq Kay Harris ; Michael Burke Briski, Combustor liner having preferentially angled cooling holes.

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11. Patel,Bhawan Bhal; Sampath,Parthasarathy; Fish,Jason Araan, Combustor liner v-band design.

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12. Hawie, Eduardo; Sze, Robert, Combustor with chamfered dome.

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13. Alkabie, Hisham, Combustor with improved cooling holes arrangement.

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14. Jorgensen, Stephen W.; Leahy, Jr., James H., Effusion cooled transition duct.

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15. Anderson,Morris G.; Kawamura,Hiroshi; Flamand,Luis M., Effusion momentum control.

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16. Howell Stephen J. ; Waslo Jennifer, Film cooled combustor liner and method of making the same.

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17. Harjit Singh Hura ; Paul Edward Sabla ; James Neil Cooper ; Beverly Stephenson Duncan ; Hukam Chand Mongia ; Steven Joseph Lohmueller, Fuel nozzle assembly for reduced exhaust emissions.

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

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19. Farmer, Gilbert; Brown, Daniel D.; Rutherford, Myron E.; Vise, Steven C.; Martini, Jeffrey M., Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form.

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20. Cunha, Frank J.; Erbas-Sen, Nurhak, Gas turbine engine combustor liner assembly with convergent hyperbolic profile.

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21. Snyder, Timothy S.; McKinney, Randal G.; Hoke, James B., Gas turbine engine combustor with tailored temperature profile.

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22. Quach, San; King, Christopher; Slavens, Thomas N., Gas turbine engine component with increased cooling capacity.

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23. Dierberger, James A., Gas turbine engine component with upstream-directed cooling film holes.

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24. Markarian, Lorin; Patel, Bhawan B., Gas turbine floating collar arrangement.

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25. Tschuor, Remigi; Schneider, Lothar; Markovic, Alen; Hähnle, Harmut, Gas turbine with welded combustor liners.

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26. Gerendas, Miklos; Sadig, Sermed, Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall.

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27. Pacheco Tougas,Monica; Coughlan, III,Joseph D.; Hoke,James B.; Goetschius,Alan J., Heat shield panels for use in a combustor for a gas turbine engine.

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28. Hawie, Eduardo; Ozem, Hayley, Heat shield sealing for gas turbine engine combustor.

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29. Keller, Dougas A.; Gonzalez, Malberto F.; Morrison, Jay A., Hybrid ceramic structure with internal cooling arrangements.

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30. Kutter, Ella Christine; Al-Roub, Marwan; Leen, Thomas Anthony; Brown, Daniel Dale; Young, Craig Douglas; Farmer, Gilbert; Ehteshami, Mohammad, Hybrid film cooled combustor liner.

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31. Vincent C. Martling ; Brian R. Mack ; Robert J. Kraft ; Mark A. Minnich, Low NOx combustion liner with cooling air plenum recesses.

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32. Christopher K. Nelson ; David B. Patterson ; Eugene F. Pridgett, Method of making a combustion chamber liner.

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33. Lee, Ching-Pang; Guentert, Joseph M.; Lu, Wenfeng; Iles, Mitchell E., Methods and apparatus for assembling turbine engines.

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34. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.

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35. Young, Craig Douglas; Sabla, Paul Edward; Vise, Steven Clayton, Methods and apparatus for cooling gas turbine engine combustors.

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36. Reback,Scott Mitchell; Sebeika,Stephen Thomas, Methods and apparatus for injecting cleaning fluids into combustors.

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37. Caldwell, James M.; Emilianowicz, Edward J.; Loveless, Gary Scott, Methods for replacing a portion of a combustor dome assembly.

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38. Emilianowicz, Edward John, Methods for replacing a portion of a combustor liner.

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39. Farmer, Gilbert; Patterson, David Bruce; Stiverson, Steven Allen; Caldwell, James Michael; Emilianowicz, Edward John; Martini, Jeffrey Michael, Methods for replacing combustor liner panels.

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40. Moertle,George E.; Emilianowicz,Edward John; Pelletier,Scott Howard, Methods for replacing combustor liners.

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41. Emilianowicz, Edward John, Methods for replacing nuggeted combustor liner panels.

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42. Budnick, Matthew, Mount with deflectable tabs.

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43. Patterson David B. ; Duncan Beverly S. ; Rettig Mark G. ; Thompson James E. ; Wiehe Glenn E., Multi-hole film cooled combuster liner.

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44. Miller, Jonathan L.; Artiles, Antonio F., Multi-stage inter shaft ring seal.

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45. Moertle,George Eric; Mills,Bruce Ernest; Holmes,James Patrick; Lind,David Albin; Harris,Tariz Kay, Multihole patch for combustor liner of a gas turbine engine.

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46. Bastnagel, Philip Michael; Petty, Jack Dwayne, Relief slot for combustion liner.

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47. Schreiber, Karl; Gerendas, Miklos, Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber.

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48. Hu, Tin-Cheung John; Lao, Si-Man Amy; Sreekanth, Sri; Papple, Michael, Single skin combustor with heat transfer enhancement.

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49. Dierberger, James A., Structures with adaptive cooling.

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50. Toqan, Majed; Gregory, Brent Allan; Yamane, Ryan Sadao; Regele, Jonathan David, Tangential combustor with vaneless turbine for use on gas turbine engines.

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51. McMasters,Marie Ann, Thick coated combustor liner.

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52. Burns Craig P. ; Duncan Beverly S. ; Thompson James E. ; Wiehe Glenn E., Transitional multihole combustion liner.

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53. Hall Kenneth B., Turbine blade cooling.

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