Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
10/2008
10/30/2008WO2008128325A1 Improved start flow measurement
10/30/2008CA2683942A1 Improved start flow measurement
10/29/2008EP1985927A2 Methods and systems to facilitate reducing NOx emissions in combustion systems
10/29/2008EP1985926A2 Combustion equipment and combustion method
10/29/2008EP1985925A2 Methods and systems to facilitate operating within flame-holding margin
10/29/2008EP1985924A1 Swirler
10/29/2008EP1985923A2 Methods and systems to facilitate reducing flashback/flame holding in combustion systems
10/29/2008EP1985920A2 Combustor and a fuel suppy method for the combustor
10/29/2008EP1985822A2 Start fuel flow measurement
10/29/2008EP1984674A1 Gas turbine burner and method of mixing fuel and air in a swirling area of a gas turbine burner
10/29/2008CN101297156A Burner arrangement for a combustion chamber, associated combustion chamber and method for combusting fuel
10/29/2008CN101294715A Combustion equipment and burner combustion method
10/29/2008CN101294714A Combustor and a fuel supply method for the combustor
10/28/2008US7442239 Fuel-conditioning skid
10/28/2008US7441409 Combustor liner v-band design
10/23/2008WO2008127437A2 Quench jet arrangement for annular rich-quench-lean gas turbine combustors
10/23/2008US20080256956 Methods and systems to facilitate reducing combustor pressure drops
10/23/2008DE102007018061A1 Gasturbinenbrennkammerwand Gas turbine combustion chamber wall
10/23/2008CA2667430A1 Method and apparatus for isolating inactive fuel passages
10/22/2008EP1983266A2 Methods and systems to facilitate reducing combustor pressure drops
10/22/2008EP1983265A2 Gas turbine reaction chamber wall
10/19/2008CA2625330A1 Combustor liner with improved heat shield retention
10/15/2008EP1980790A2 Electro-dynamic swirler, combustion apparatus and methods using the same
10/15/2008CN101285592A Integral fuel jet axial swirler pre-mixing preevaporated low pollution combustion-chamber
10/15/2008CN101285591A Integral fuel jet radial swirler pre-mixing preevaporated low pollution combustion-chamber
10/15/2008CN101285590A Electro-dynamic swirler, combustion apparatus and methods using the same
10/14/2008US7434404 Method for operating a gas turbine combustion chamber including a plurality of burners arranged in groups
10/14/2008US7434401 Fuel/air premixer for gas turbine combustor
10/14/2008CA2335355C Igniter with porous sleeve
10/09/2008WO2008119737A1 Combustion pre-chamber
10/09/2008US20080245072 Damping of Vibration of a Combustion Chamber By Resonators
10/09/2008DE102008016931A1 System zur Reduktion der Brennkammerdynamik System to reduce the combustion chamber dynamics
10/08/2008EP1978308A2 Combustors and combustion systems for gas turbine engines
10/08/2008EP1978307A2 Combustor of a gas turbine engine
10/08/2008EP1978306A2 Hooded air/fuel swirler for a gas turbine engine
10/08/2008EP1978305A1 Shielding for the bottom of a combustion chamber
10/08/2008EP1423645B1 Damping arrangement for reducing combustion chamber pulsations in a gas turbine system
10/08/2008CN100424416C Cooling structure of gas turbine tail pipe
10/07/2008US7430869 System for catalytic combustion
10/07/2008CA2614624C Pilot nozzle of gas turbine combustor
10/07/2008CA2335349C Fuel injector for gas turbine engine
10/07/2008CA2332359C Gas turbine fuel injector
10/02/2008WO2008116906A1 Eccentric chamfer at inlet of branches in a flow channel
10/02/2008WO2008078024A3 Composite material part with a silicon-containing ceramic matrix protected against corrosion
10/02/2008US20080236165 Dual-injector fuel injector system
10/01/2008EP1975514A2 A location ring arrangement
10/01/2008EP1975513A2 A premix burner for a gas turbine, in particular a microturbine
10/01/2008EP1975512A2 Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
10/01/2008EP1975506A1 Combustion pre-chamber
10/01/2008EP1975372A1 Eccentric chamfer at inlet of branches in a flow channel
10/01/2008CN101278153A Turbine engine having acoustically tuned fuel nozzle
10/01/2008CN101278152A Fuel nozzle having swirler-integrated radial fuel jet
10/01/2008CN101277783A A method and a device for production of a set of holes
10/01/2008CN101275751A Radial swirler turning zone liquid and mist injection premixing and prevapourising low pollution burning chamber
10/01/2008CN101275750A Radial swirler turning zone direct injection premixing and prevapourising low pollution burning chamber
10/01/2008CN100422645C Multiport dome baffle
09/2008
09/30/2008US7428817 Premix burner with a swirl generator delimiting a conical swirl space and having sensor monitoring
09/30/2008CA2627881A1 Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
09/30/2008CA2625531A1 Combustor floating collar with louver
09/26/2008CA2626952A1 Combustors and combustion systems for gas turbine engines
09/25/2008US20080230997 Combustion chamber for a gas turbine
09/25/2008US20080229752 Fuel lance
09/25/2008US20080229751 Cooling system for gas turbine engine having improved core system
09/25/2008US20080229750 Location ring arrangement
09/24/2008EP1972851A2 Burner
09/24/2008EP1971804A1 Method for the operation of a firing plant
09/23/2008US7426833 Gas turbine combustor and fuel supply method for same
09/23/2008CA2365821C Gas turbine combustion device
09/23/2008CA2340391C Arrangement for reduction of acoustic vibrations in a combustion chamber
09/18/2008WO2008110554A1 Burner fuel staging
09/18/2008US20080227039 Premixing Burner Arrangement for Operating a Combustion Chamber in Addition to a Method for Operating a Combustion Chamber
09/17/2008EP1970629A1 Burner fuel staging
09/17/2008EP1970628A2 Methods of forming fan-shaped effusion holes in combustors
09/16/2008US7425127 Stagnation point reverse flow combustor
09/16/2008US7424804 Premix burner
09/16/2008CA2496621C Cooling construction of transition piece of a gas turbine
09/12/2008WO2008108812A2 Turbine engine having folded annular jet combustor
09/12/2008WO2008108810A2 Splash plate dome assembly for a turbine engine
09/12/2008WO2008057685A3 Combustor nozzle for a fuel-flexible combustion system
09/11/2008US20080216481 System for Damping Thermo-Acoustic Instability in a Combustor Device for a Gas Turbine
09/10/2008EP1967696A1 Turbine part
09/10/2008EP1966539A2 Turbine spring clip seal
09/10/2008EP1872075B1 Heat shield element for lining a combustion chamber wall, combustion chamber and gas turbine
09/10/2008CN101261014A High velocity combustion heating equipment
09/09/2008US7421844 Method for the combustion of a fuel-oxidizer mixture
09/04/2008WO2008037554A3 Improvements in or relating to gas turbine engines
09/04/2008US20080209909 Gas turbine combustor and fuel supply method for same
09/04/2008US20080209728 Methods and apparatus for attaching swirlers to turbine engine combustors
09/03/2008EP1963748A1 Combustion chamber with burner and associated operating method
09/03/2008EP1466124B1 Burner arrangement for the annular combustion chamber of a gas turbine
09/03/2008CN101255821A Method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit
09/03/2008CN100416063C Fuel injector laminated fuel strip
09/03/2008CN100416062C Combustion chamber inlet booster with blowing attached layer
09/02/2008CA2622113A1 Process for starting a gas turbine helicopter engine, fuel supply system of said engine, and engine with said system
08/2008
08/28/2008WO2008030214A3 Turbine spring clip seal
08/28/2008US20080202122 Arrangement with a twist-lock coupling for a turbomachine combustion chamber
08/28/2008CA2622116A1 High-pressure turbine of a turbomachine
08/27/2008EP1962018A1 Combustion chamber for gas turbine engine
08/27/2008EP1961833A1 Thermal barrier coating systems and materials
08/27/2008EP1960650A2 Improved airflow distribution to a low emission combustor
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