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)
06/2005
06/28/2005US6910336 Combustion liner cap assembly attachment and sealing system
06/23/2005WO2005022061A3 Heat shield block for lining a combustion chamber wall, combustion chamber and gas turbine
06/23/2005US20050136367 Simultaneous combustion with premixed and non-premixed fuels and fuel injector for such combustion
06/23/2005US20050132716 Reduced exhaust emissions gas turbine engine combustor
06/23/2005US20050132714 Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith
06/23/2005US20050132708 Cooling and sealing design for a gas turbine combustion system
06/22/2005EP1544545A1 Split vane flow blocker
06/22/2005EP1544185A2 Environmental barrier coating comprising a gas velocity reducing top layer
06/22/2005EP1543272A1 Turbine engine fuel nozzle
06/22/2005CN1629541A Thick coated combustor liner
06/21/2005US6908303 Premixed air-fuel mixture supply device
06/21/2005US6907920 Heat exchanger panel
06/21/2005US6907736 Gas turbine combustor having an acoustic energy absorbing wall
06/21/2005US6907724 Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
06/16/2005WO2005054632A1 Sliding joint between combustor wall and nozzle platform
06/16/2005WO2005028960A3 Pilot combustor for stabilizing combustion in gas turbine engines
06/16/2005US20050130089 Premixed air-fuel mixture supply device
06/16/2005US20050129973 Velocity barrier layer for environmental barrier coatings
06/16/2005US20050129501 Split vane flow blocker
06/16/2005US20050127537 Premixed air-fuel mixture supply device
06/16/2005US20050126180 Multi-point staging strategy for low emission and stable combustion
06/16/2005US20050126178 Method for operating a gas turbine and gas turbine system for carrying out the method
06/15/2005EP1540247A1 Stress relief feature for aerated gas turbine fuel injector
06/15/2005EP0920575B1 Microturbomachinery
06/15/2005CN1626877A Burner of gas turbine
06/14/2005US6904757 Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor
06/14/2005US6904747 Heat exchanger for power generation equipment
06/14/2005US6904676 Methods for replacing a portion of a combustor liner
06/09/2005WO2005051866A1 Oxidation barrier coatings for silicon based ceramics
06/09/2005WO2005008135A3 Trapped vortex combustor
06/09/2005US20050120718 Gas turbine combustor sliding joint
06/09/2005US20050120717 Fuel injection method and apparatus for a combustor
06/08/2005EP1537363A1 Gas turbine
06/08/2005EP1536887A1 Catalyst
06/07/2005US6901758 Method for repairing an air cooled combustor liner segment edge portion and repaired segment
06/07/2005US6901757 Heat shield arrangement with sealing element
06/07/2005US6901756 Device for the injection of fuel into the flow wake of swirler vanes
06/07/2005CA2152536C Method and apparatus for ultrasonically assisted melt extrusion of fibers
06/02/2005WO2005049312A1 High-temperature layered system for dissipating heat and method for producing said system
06/02/2005WO2005026675A3 Catalyst module overheating detection and methods of response
06/02/2005US20050115244 Premix burner
06/01/2005EP1534997A2 Burner
06/01/2005EP1534996A1 Process for combustion of a liquid hydrocarbon
06/01/2005EP1534652A1 Ceramic material having ceramic matrix composite backing and method of manufacturing
06/01/2005CN1623031A Method for operating a turbine group
06/01/2005CN1623030A Wing structure of air swirling device for internal combustion engine
06/01/2005CN1621671A Method and device for monitoring gas turbine combustion dynamics
05/2005
05/31/2005US6898938 Differential pressure induced purging fuel injector with asymmetric cyclone
05/31/2005US6898937 Gas only fin mixer secondary fuel nozzle
05/31/2005US6898926 Cooled purging fuel injectors
05/26/2005WO2005047670A2 Method and apparatus for actuating fuel trim valves in a gas turbine
05/26/2005US20050114010 Method for controlling fuel splits to gas turbine combustor
05/26/2005US20050112381 Oxidation barrier coatings for silicon based ceramics
05/26/2005US20050109036 Cascade ignition of catalytic combustors
05/25/2005EP1533574A1 Gas turbine combustion chamber with lining elements and method to apply or remove these elements
05/25/2005EP1533573A1 Method for controlling fuel splits to a gas turbine combustor
05/25/2005EP1533572A1 Gas turbine combustion chamber and gas turbine
05/25/2005EP1533113A1 High temperature layered system for heat dissipation and method for making it
05/25/2005EP1532400A1 Method and device for combusting a fuel-oxidising agent mixture
05/25/2005EP1532395A1 Method and device for mixing fluid flows
05/25/2005EP1532394A1 Hybrid burner and corresponding operating method
05/25/2005EP1532358A2 Orbiting combustion nozzle engine
05/25/2005DE10392526T5 Katalytisches Verbrennungssystem und Verfahren zum Betreiben einer Gasturbine, die ein derartiges System beinhaltet The catalytic combustion system and method of operating a gas turbine, which includes such a system
05/25/2005CN1619122A Method for controlling fuel splits to gas turbine combustor
05/24/2005US6896509 Combustion method and burner for carrying out the method
05/24/2005US6895761 Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
05/24/2005US6895759 Premix burner and method of operation
05/24/2005US6895758 Fluidic control of fuel flow
05/24/2005US6895757 Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
05/24/2005US6895756 Compact swirl augmented afterburners for gas turbine engines
05/24/2005US6895755 Nozzle with flow equalizer
05/19/2005US20050107942 Gas turbine control apparatus, gas turbine system and gas turbine control method
05/19/2005US20050106520 Device for stabilizing combustion in gas turbine engines
05/19/2005US20050106519 Burner, method for operating a burner and gas turbine
05/19/2005US20050103023 Ultra low Nox emissions combustions system for gas turbine engines
05/19/2005US20050103021 Method and apparatus to decrease combustor emissions
05/19/2005US20050103020 Method and apparatus to decrease combustor emissions
05/19/2005US20050103018 Combustion chamber for a gas turbine
05/19/2005DE4212810B4 Brenner mit zusätzlicher Zuführungsmöglichkeit für fluidische Stoffe, insbesondere für Gasturbinen, und Verfahren zu seinem Betrieb Burner with an additional supply possibility for fluid substances, in particular for gas turbines, and method for its operation
05/18/2005EP1531305A1 Multi-point fuel injector
05/18/2005EP1531303A1 Improved fuel staging process for low NOx operations
05/18/2005EP1125087B1 Burner assembly
05/18/2005EP1033536B1 Combustor for gas turbine
05/18/2005CN1617951A High-temperature protection layer
05/18/2005CN1616884A Fuel staging process for low NOx operations
05/18/2005CN1616806A Seal assembly
05/17/2005US6892543 Gas turbine combustor and combustion control method thereof
05/12/2005WO2005043058A2 Ceramic thermal shield with integrated reinforcing elements, especially for lining the wall of a gas turbine combustion chamber
05/12/2005WO2005005888A8 Cooling structure of gas turbine tail pipe
05/12/2005US20050100846 Burner
05/12/2005US20050097895 Method and apparatus for actuating fuel trim valves in a gas turbine
05/12/2005US20050097894 Combustion chamber for combusting a combustible fluid mixture
05/12/2005US20050097891 Arrangement for the cooling of thermally highly loaded components
05/12/2005US20050097890 Gas turbine combustor
05/11/2005EP1529181A1 Gas turbine combustion chamber
05/11/2005EP1529180A1 Premixed exit ring pilot burner
05/11/2005EP1268981B1 Turbine installation
05/11/2005CN1615417A Combustion device for circular combustion chamber in a gas turbine plant
05/11/2005CN1615416A Combustion chamber in a gas turbine plant
05/11/2005CN1201115C Combustor with stepped fuel spray and its running process
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