| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 04/23/2008 | CN101166935A Process and device for regulating the course of a gas turbine combustion chamber |
| 04/22/2008 | US7360363 Premixing nozzle, combustor, and gas turbine |
| 04/22/2008 | CA2433402C Combustor for gas turbine |
| 04/17/2008 | WO2008017551A3 Combustion chamber of a combustion plant |
| 04/17/2008 | US20080090005 Heat treatment ot a ceramic protectvie coating (oxides of barium, strontium, aluminum and silicon) to form an outer surface region of stoichiometric crystalline phases and crystalline phase free of nonstoichiometric silica; nonporous; heat, corrosion, oxidation chemical resistance; gas turbine engines |
| 04/17/2008 | DE102007049299A1 Verfahren und Systeme zur Analyse von Verbrennungsdynamiken in der Zeitdomäne Methods and systems for the analysis of combustion dynamics in the time domain |
| 04/16/2008 | EP1912022A2 Gas turbine combustor and method for supplying fuel to the same |
| 04/16/2008 | EP1910018A1 A method and a device for production of a set of holes |
| 04/16/2008 | CN101162483A Methods and systems for analysis of combustion dynamics in the time domain |
| 04/15/2008 | US7356994 Alignment and positioning system for installing a fuel injector in a gas turbine engine |
| 04/15/2008 | CA2394694C Pilot nozzle of gas turbine combustor |
| 04/10/2008 | WO2008040118A1 Multi-channel fuel manifold |
| 04/10/2008 | DE112006001317T5 Gasturbinen-Brennkammer A gas turbine combustor |
| 04/10/2008 | CA2665353A1 Multi-channel fuel manifold |
| 04/09/2008 | EP1909032A2 Method and apparatus for reducing gas turbine engine emissions |
| 04/09/2008 | EP1909031A1 Fuel injector for the combustion chamber of a gas turbine engine |
| 04/09/2008 | EP1909030A2 Methods and apparatus to facilitate decreasing combustor acoustics |
| 04/09/2008 | EP1714081B1 Premixing burner arrangement for operating a burner chamber and method for operating a burner chamber |
| 04/09/2008 | EP1529181B1 Gas turbine combustion chamber |
| 04/09/2008 | CN101158479A Liquid fuel enhancement for natural gas swirl stabilized nozzle and method |
| 04/09/2008 | CN101158478A Combustion system for gas turbines comprises combustion chamber, into which air is fed through inlet, fuel being fed into air stream through pair of inlets at angle to it, so that streams cross |
| 04/09/2008 | CN101158477A Methods and apparatus for assembling turbine engines |
| 04/09/2008 | CN101158476A Method and apparatus for reducing gas turbine engine emissions |
| 04/09/2008 | CN100380046C Gasifying combined power generating apparatus |
| 04/09/2008 | CN100379947C Structure for connecting or space sealing members with different thermal expansion coefficients |
| 04/06/2008 | CA2605952A1 Fuel injector for a gas turbine engine combustion chamber |
| 04/03/2008 | WO2008037554A2 Improvements in or relating to gas turbine engines |
| 04/03/2008 | DE102007046251A1 Combustion system for gas turbines comprises combustion chamber, into which air is fed through inlet, fuel being fed into air stream through pair of inlets at angle to it, so that streams cross |
| 04/03/2008 | DE102006045946A1 Combustion chamber for aircraft and ground gas turbine engines comprises an outer housing, a flame tube, fuel nozzles, an ignition plug and an expandable ionization chamber containing electrodes |
| 04/03/2008 | DE102006045943A1 New form of nozzle for aircraft engine combustion chambers for reduced emissions has turbulence guides in fuel channel and attached fitting with cross-piece mounted within it that provides turbulent flow of liquid within nozzle |
| 04/02/2008 | EP1905951A2 Structual members in a pedestal array |
| 04/02/2008 | EP1904717A2 Hot gas-conducting housing element, protective shaft jacket, and gas turbine system |
| 04/02/2008 | CN101153558A Premixing device, gas turbines comprising the premixing device, and methods of use |
| 04/01/2008 | US7350360 Annular combustor for a gas turbine |
| 04/01/2008 | US7350357 Nozzle |
| 04/01/2008 | CA2284363C Thermal barrier coating systems and materials |
| 03/29/2008 | CA2603567A1 Methods and apparatus to facilitate decreasing combustor acoustics |
| 03/27/2008 | WO2008034227A1 Internal fuel manifold having temperature reduction feature |
| 03/27/2008 | US20080072603 Annular turbomachine combustion chamber |
| 03/27/2008 | DE102007045053A1 Mischlochanordnung und Verfahren zur Verbesserung der Homogenität eines Brennstoff-Luft-Gemisches in einer Brennkammer Mixing hole arrangement and method for improving the homogeneity of a fuel-air mixture in a combustion chamber |
| 03/27/2008 | DE102006042124A1 Gasturbinenbrennkammer A gas turbine combustor |
| 03/26/2008 | EP1903283A1 Annular combustion chamber of a turbomachine |
| 03/26/2008 | CA2604278A1 Method of manufacturing a heat shield for a fuel manifold |
| 03/26/2008 | CA2604272A1 Heat shield for fuel manifold |
| 03/22/2008 | CA2603595A1 Heat shield with stress relieving feature |
| 03/22/2008 | CA2602938A1 Annular combustion chamber for a turbine engine |
| 03/21/2008 | CA2603130A1 Combustion transition duct providing stage 1 tangential turning for turbine engines |
| 03/20/2008 | WO2008033542A2 Gas turbine fuel injector with a removable pilot assembly |
| 03/20/2008 | DE102006041955A1 Verfahren zur Steuerung der Verbrennung in einer Brennkammer und Brennkammervorrichtung Method for controlling the combustion in a combustion chamber and combustion chamber device |
| 03/19/2008 | EP1899649A1 Ceramic component comprising a surface which is resistant to hot gas, and method for the production thereof |
| 03/19/2008 | EP1899648A2 Molding compound for producing a refractory lining |
| 03/19/2008 | EP1899582A1 Turbine thermal shield and guide vane for a gas turbine |
| 03/19/2008 | EP1730441B1 Device and method for stabilizing the flame in a burner |
| 03/18/2008 | US7343745 Gas turbine combustor and operating method thereof |
| 03/13/2008 | WO2008028621A1 Gas turbine combustion chamber |
| 03/13/2008 | CA2662720A1 Gas turbine combustion chamber |
| 03/12/2008 | EP1898155A1 Annular combustion chamber of a turbomachine |
| 03/12/2008 | EP1896775A1 Gas turbine combustion transition duct providing tangential turning of the flow |
| 03/12/2008 | CN100374242C Process for drilling holes in a metallic workpiece having a thermal barrier coating |
| 03/12/2008 | CA2599786A1 Combustor with enhanced cooling access |
| 03/11/2008 | US7341797 Environmental barrier coating for silicon-containing substrates and process therefor |
| 03/11/2008 | US7340881 Gas turbine combustor |
| 03/11/2008 | US7340880 Compressed air bypass valve and gas turbine |
| 03/06/2008 | WO2008025525A1 Method of controlling the combustion in a combustion chamber and combustion chamber device |
| 03/06/2008 | US20080053103 Combustor heat shield and method of cooling |
| 03/06/2008 | DE102007042059A1 Einspritzanordnung für eine Brennkammer Injection assembly for a combustion chamber |
| 03/06/2008 | DE102006040760A1 Lean-burning gas turbine combustion chamber wall, has Inflow holes formed perpendicularly over chamber wall, and damping openings formed by shingle, where shingle is spaced apart from chamber wall by using side part |
| 03/05/2008 | EP1895236A2 Method and apparatus for cooling gas turbine engine combustors |
| 03/05/2008 | EP1893917A2 Attachment device for removable components in hot gas paths in a turbine engine |
| 03/05/2008 | CN101137868A Premix burner for producing an ignitable fuel/air mixture |
| 03/05/2008 | CN101135462A Method and apparatus for cooling gas turbine engine combustors |
| 03/04/2008 | US7338244 Attachment device for turbine combustor liner |
| 03/04/2008 | US7337614 Engine fueling method |
| 03/04/2008 | CA2178874C Annular combustion chamber with wall having multiple perforations |
| 02/29/2008 | CA2599816A1 Improved fuel injection system and method of assembly |
| 02/29/2008 | CA2598333A1 Welded gas turbine engine parts with different thicknesses and method |
| 02/28/2008 | CA2598543A1 Annular combustion chamber of a turbomachine |
| 02/27/2008 | EP1892472A1 Combustion system particularly for a gas turbine |
| 02/27/2008 | EP1892469A1 Swirler passage and burner for a gas turbine engine |
| 02/27/2008 | EP1344002B1 Burner with progressive fuel injection |
| 02/27/2008 | CN201028592Y Nitrogen gas blowing and isolating system of gas turbine medium and low-calorie fuels supply system |
| 02/27/2008 | CN201028591Y Medium and low-calorie fuels supply system of gas turbine |
| 02/26/2008 | US7335429 Gas turbine engine protuberances coated with a cooling coating and a protective coating; improved heat exchange and oxidation and corrosion resistances |
| 02/26/2008 | US7334412 Cooling air and injected liquid system for gas turbine blades |
| 02/26/2008 | US7334410 Swirler |
| 02/26/2008 | US7334407 Method of suppressing coke in endothermic fuel processing |
| 02/22/2008 | CA2597272A1 Optimized internal manifold heat shield attachment |
| 02/21/2008 | WO2008019997A1 Swirler passage and burner for a gas turbine engine |
| 02/21/2008 | WO2008019969A1 Combustion system, particularly for a gas turbine |
| 02/21/2008 | US20080041059 Radially staged RQL combustor with tangential fuel premixers |
| 02/20/2008 | EP1890083A1 Fuel injector for a gas turbine engine |
| 02/20/2008 | EP1360439B1 A method and a device for supplying fuel to a combustion chamber |
| 02/20/2008 | CN201025371Y A flame canister with corset structure |
| 02/20/2008 | CN101126353A 燃气轮机系统和燃气轮机控制方法 Gas turbine and gas turbine system control method |
| 02/20/2008 | CN100370177C Combustion chamber for firing one kind of combustable liquid mixed fuel |
| 02/19/2008 | US7331182 Combustion chamber for a gas turbine |
| 02/19/2008 | CA2361962C Gas turbine combustor with cooling water injection |
| 02/14/2008 | WO2008017550A1 Combustion chamber of a combustion installation |
| 02/14/2008 | DE19809364B4 Dynamisch entkoppelter Brenner mit geringen NOx-Emissionen Dynamically decoupled burner with low NOx emissions |
| 02/13/2008 | EP1886001A1 Method, device and system for efficient energy transformation |