Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
01/2003
01/02/2003US20030000216 Gas turbine combustor
01/02/2003EP1271059A2 Methods and systems for cooling gas turbine engine combustors
01/02/2003EP1271058A2 Gas turbine combustor
01/02/2003EP1271057A2 Gas turbine combustor
01/02/2003EP1271056A1 Gas turbine combustion chamber and process for supplying air therein
01/02/2003EP1270902A1 Procedure for the start of a gas turbine system
01/02/2003EP1270874A1 Gas turbine with an air compressor
01/02/2003EP1268981A1 Turbine installation
12/2002
12/31/2002US6499993 External dilution air tuning for dry low NOX combustors and methods therefor
12/31/2002CA2098523C Device for operating a swirler which controls combustion air of a burner for gas turbine engines
12/27/2002WO2002103176A1 Power generator with low co2 emissions and associated method
12/26/2002US20020197580 Device for burning a gaseous fuel/oxidant mixture
12/26/2002US20020197578 Method and apparatus for a fuel-rich catalytic reactor
12/26/2002US20020194851 Method for running up a gas turbine plant
12/25/2002CN1097153C Method and device for monitoring supply system of gas turbine with multiple jet burners
12/24/2002US6497105 Low cost combustor burner collar
12/24/2002US6497104 Damped combustion cowl structure
12/24/2002US6497103 Methods for decreasing combustor emissions
12/24/2002US6497098 Method and device for generating hot combustion waste gases
12/24/2002CA2089295C One-piece cowl for a double annular combustor
12/19/2002US20020192615 Fluid distributor,burner device, gas turbine engine, and cogeneration system
12/19/2002US20020190137 Steam injection nozzle design of gas turbine combustion liners for enhancing power output and efficiency
12/19/2002US20020189260 Gas turbine combustion chambers
12/19/2002US20020189259 Fuel manifold block and ring with macrolaminate layers
12/19/2002US20020189258 Gas turbine combustor
12/19/2002US20020189257 Premix burner arrangement for operating a combustion chamber field of technology
12/18/2002EP1267128A2 Gas turbine combustor
12/18/2002EP1267127A1 Method for replacing combustor liner panels
12/18/2002EP1267121A1 Duct burner diffuser
12/18/2002EP1266718A2 Methods for replacing nuggeted combustor liner panels
12/18/2002EP1266176A1 Method and apparatus for a fuel-rich catalytic reactor
12/17/2002US6495207 Open cell metal foam core layer bonded to an inner and an outer cladding layer; manufacturing a combustor for a gas turbine engine having an air permeable open cell metal foam core bounded by perforated thin metal or ceramic walls
12/17/2002US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
12/17/2002US6494031 Gas turbine apparatus with heat exchanger
12/12/2002WO2002099337A1 Low cost combustor burner collar
12/12/2002WO2002090831A8 Device and method for injecting a liquid fuel in an air flow for a combustion chamber
12/12/2002US20020184893 Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
12/12/2002US20020184892 Fastening a CMC combustion chamber in a turbomachine using brazed tabs
12/12/2002US20020184891 Architecture for a combustion chamber made of ceramic matrix material
12/12/2002US20020184890 Resilient mount for a CMC combustion of a turbomachine in a metal casing
12/12/2002US20020184889 Fastening a CMC combustion chamber in a turbomachine using the dilution holes
12/12/2002US20020184888 Connection for a two-part CMC chamber
12/12/2002US20020184887 Combustion chamber provided with a system for fixing the chamber end wall
12/12/2002US20020184886 Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine
12/12/2002US20020184883 Damped combustion cowl structure
12/12/2002US20020184871 Bypass air injection method and apparatus for gas turbines
12/12/2002US20020184763 Methods for replacing nuggeted combustor liner panels
12/12/2002US20020184762 Methods for replacing combustor liner panels
12/12/2002DE10126926A1 Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung Combustion chamber with inner shell made from a ceramic composite material and method for producing
12/11/2002EP1265037A1 Fixation of turbine ceramic matrix composite combustion chamber using dilution holes
12/11/2002EP1265036A1 Elastic mounting of a ceramic matrix composite combustion chamber inside a metallic casing
12/11/2002EP1265035A1 Double mounting of a ceramic matrix composite combustion chamber
12/11/2002EP1265034A1 Mounting of a turbine ceramic matrix composite combustion chamber with brazed mounting lungs
12/11/2002EP1265033A1 Combustion chamber with a system for mounting the chamber end wall
12/11/2002EP1265032A1 Ceramic matrix composite material gas turbine combustion chamber
12/11/2002EP1265031A1 Fixing of metallic cowls on turbomachine combustion chamber liners made of CMC materials
12/11/2002EP1265030A1 Mounting of a metallic matrix composite combustion chamber with flexible linking shrouds
12/11/2002CN1384908A 燃烧器 Burner
12/10/2002US6492034 Heat shield
12/10/2002US6491236 Method and device for injecting a fuel/liquid mixture into the combustion chamber of a burner
12/05/2002WO2002097332A1 Heat shield arrangement for a hot-gas conducting component, in particular for structural pieces of gas turbines and method for production of said arrangement
12/05/2002US20020182555 Catalyzer
12/05/2002US20020182553 Burner for the production of a hot gas
12/05/2002US20020182551 Catalyzer
12/05/2002US20020179731 Ultrasonically enhanced continuous flow fuel injection apparatus and method
12/05/2002US20020178734 Low cost combustor burner collar
12/05/2002US20020178732 Method and apparatus for mixing fuel to decrease combustor emissions
12/05/2002US20020178728 Methods for reducing heat load in combustor panels
12/05/2002US20020178727 Methods and apparatus for injecting fuel into gas turbine engines
12/05/2002US20020178726 Combustor for gas turbine engines with low air flow swirlers
12/04/2002EP1262719A2 Method and apparatus for controlling combustor emissions
12/04/2002EP1262718A2 Method and apparatus for mixing fuel to decrease combustor emissions
12/04/2002EP1262715A2 Pilot nozzle for a gas turbine combustor and supply path converter
12/03/2002US6487994 Sub-critical water-fuel composition and combustion system
12/03/2002US6487861 Combustor for gas turbine engines with low air flow swirlers
11/2002
11/28/2002WO2002095293A1 Burner apparatus for burning fuel and air
11/28/2002US20020177093 Method for injecting fuel into a burner
11/28/2002US20020174658 Slot cooled combustor line
11/28/2002US20020174657 Apparatus for forming a combustion mixture in a gas turbine engine
11/28/2002US20020174656 Turbine engine burner
11/27/2002EP1260768A2 A combustion chamber
11/27/2002EP1260767A1 Heat shield assembly for a high temperature gas conveying component, in particular for structural components of gas turbines, as well as process for producing such an assembly
11/27/2002CN2522757Y Thermoelectric conversion heat-insulation combustor
11/26/2002US6484509 Combustion chamber/venturi cooling for a low NOx emission combustor
11/26/2002US6484505 Combustor liner cooling thimbles and related method
11/26/2002US6484489 Method and apparatus for mixing fuel to decrease combustor emissions
11/26/2002CA2048728C Double dome combustor
11/21/2002US20020172904 Combustion chamber
11/21/2002US20020170294 Thermal turbomachine and process for igniting the thermal turbomachine
11/21/2002US20020170293 Methods and systems for cooling gas turbine engine igniter tubes
11/20/2002EP1258682A2 Methods and systems for cooling gas turbine engine igniter tubes
11/20/2002EP1258681A2 Methods and apparatus for cooling gas turbine engine combustors
11/19/2002US6481209 Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer
11/19/2002CA2246219C Three-dimensional swirler
11/14/2002WO2002090831A1 Device and method for injecting a liquid fuel in an air flow for a combustion chamber
11/14/2002DE10064893A1 Brenner mit gestufter Brennstoffeindüsung Burner with staged fuel injection
11/13/2002EP1255952A1 Device in a burner for gas turbines
11/13/2002EP1064510B1 Wall segment for a combustion chamber and combustion chamber
11/07/2002WO2002088604A1 Gas turbine with combined can-type and annular combustor and method of operating a gas turbine
11/07/2002WO2002088603A1 Ultra low nox emissions combustion system for gas turbine engines