Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
05/2005
05/10/2005US6890660 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture
05/10/2005US6889495 Gas turbine combustor
05/06/2005WO2005040682A2 Device for stabilizing combustion in gas turbine engines
05/06/2005WO2005040677A2 Combustion method and apparatus for carrying out same
05/05/2005US20050095542 Variable geometry combustor
05/05/2005US20050091987 Combustion chamber intermediate part for a gas turbine
05/04/2005EP1528343A1 Refractory tile with reinforcing members embedded therein, as liner for gas turbine combustion chamber
05/04/2005EP1528323A1 Methods and apparatus for attaching swirlers to turbine engine combustors
05/04/2005EP1528322A2 Combustor
05/04/2005EP1292795B1 Method for operating a burner with staged premix gas injection
05/04/2005DE19858197B4 Triebwerk Engine
05/04/2005CN1611839A Gas turbine control apparatus, gas turbine system and gas turbine control method
05/03/2005US6887067 Catalytically operating burner
05/03/2005US6886341 Gas-turbine engine combustor
04/2005
04/28/2005WO2005038447A1 Apparatus and method for testing combustion
04/28/2005WO2005038348A1 Method and device for the combustion of fuel
04/28/2005WO2004065777A3 Dynamic control system and method for multi-combustor catalytic gas turbine engine
04/28/2005WO2004033886A3 System for vaporization of liquid fuels for combustion and method of use
04/28/2005US20050086945 Combustion chamber, in particular of a gas turbine
04/28/2005US20050086944 Turbine engine fuel injector
04/28/2005US20050086941 Afterburner arrangement
04/28/2005US20050086940 Combustor
04/27/2005EP1526333A1 Turbine engine fuel injector
04/27/2005EP1526332A2 Fuel injection nozzle
04/27/2005CN1609513A Methods and apparatus for attaching swirlers to turbine engine combustors
04/27/2005CN1609427A Apparatus for film cooling gas turbine engine combustors
04/27/2005CN1609426A Methods and apparatus for cooling turbine engine combustor exit temperatures
04/26/2005US6884384 Method for making a high temperature erosion resistant material containing compacted hollow geometric shapes
04/26/2005US6883332 Fuel nozzle for turbine combustion engines having aerodynamic turning vanes
04/26/2005US6883329 Method of fuel nozzle sizing and sequencing for a gas turbine combustor
04/21/2005WO2005036058A1 Auxiliary power unit having a rotary fuel slinger
04/21/2005WO2005036057A1 Aerodynamic trip for a combustion system
04/21/2005US20050084812 Combustion method and apparatus for carrying out same
04/21/2005US20050081528 Methods and apparatus for attaching swirlers to turbine engine combustors
04/21/2005US20050081527 Methods and apparatus for film cooling gas turbine engine combustors
04/21/2005US20050081526 Methods and apparatus for cooling turbine engine combustor exit temperatures
04/21/2005US20050081508 Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
04/21/2005CA2541907A1 Auxiliary power unit having a rotary fuel slinger
04/20/2005EP1524473A1 Process and device to burn fuel
04/20/2005EP1524472A2 Apparatus for film cooling gas turbine engine combustors
04/20/2005EP1524471A1 Methods and apparatus for cooling turbine engine combuster exit temperatures
04/20/2005EP1524469A1 Premix burner for a gas turbine
04/19/2005US6880341 Low cost combustor floating collar with improved sealing and damping
04/19/2005US6880340 Combustor with turbulence producing device
04/19/2005US6880339 Combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
04/19/2005US6880325 Gas turbine combustor apparatus
04/14/2005WO2005033558A1 High temperature seal
04/14/2005US20050079464 Premix burner and method for operation thereof
04/14/2005US20050077341 Method of manufacturing an active cooling panel out of thermostructural composite material
04/14/2005US20050076650 Auxiliary power unit having a rotary fuel slinger
04/14/2005US20050076648 Method and apparatus for injecting a fuel into a combustor assembly
04/14/2005US20050076647 Method and apparatus for mixing substances
04/14/2005US20050076644 Quiet combustor for a gas turbine engine
04/14/2005US20050076643 Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine
04/14/2005DE4406399B4 Wärmeerzeuger Heat source
04/14/2005CA2539948A1 High temperature seal
04/13/2005EP1522792A1 Combustor
04/13/2005EP1522695A1 Combustor cooling for gas turbine engines
04/12/2005CA2198420C Fuel injection device for aircraft ramjet
04/07/2005US20050073114 Seal assembly
04/07/2005US20050072163 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner
04/07/2005DE19814588B4 Hochtemperaturfeste oxidische Faserverbundwerkstoffe, ihre Herstellung und Verwendung High-temperature oxide fiber composites, their preparation and use
04/06/2005EP1521037A1 Method and system for controlling fuel supply in a combustion turbine engine
04/06/2005EP1521036A1 Seal assembly
04/06/2005EP1521018A1 High temperature seal
04/05/2005US6874323 Low emissions hydrogen blended pilot
04/05/2005CA2284761C Bypass air volume control device for combustor used in gas turbine
03/2005
03/31/2005WO2005028960A2 Pilot combustor for stabilizing combustion in gas turbine engines
03/31/2005US20050070431 combustion gas turbine engines; ceramic powder doped with a catalyst species
03/31/2005US20050067506 Nozzle assembly with fuel tube deflector
03/31/2005US20050066663 Catalytic combustors
03/31/2005DE10341515A1 Anordnung zur Kühlung hoch wärmebelasteter Bauteile Arrangement for cooling high heat-stressed components
03/31/2005DE10340826A1 Homogene Gemischbildung durch verdrallte Einspritzung des Kraftstoffs Homogeneous mixture formation by swirling injection of the fuel
03/31/2005DE102004032062A1 Verfahren und Vorrichtung zum Zuführen von Speiseluft in Turbinenbrennkammern Method and device for supplying feed air into turbine combustors
03/30/2005EP1519116A1 Catalytic combustors
03/30/2005EP1519115A2 Method to operate a gas turbine with different fuels
03/30/2005CN1601181A Method and apparatus for reducing gas turbine engine emissions
03/29/2005US6871503 Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low nox combustion
03/29/2005US6871501 Method and apparatus to decrease gas turbine engine combustor emissions
03/29/2005US6871488 Natural gas fuel nozzle for gas turbine engine
03/29/2005CA2284474C Combined cycle electric power plant
03/29/2005CA2237843C Dichotomous reheat system reducing losses in dry operation
03/29/2005CA2194897C Boiler with pressurized circulating fluidized bed firing
03/24/2005WO2005026675A2 Catalyst module overheating detection and methods of response
03/24/2005US20050062237 Turbine spring clip seal
03/24/2005US20050061004 Method and apparatus for reducing gas turbine engine emissions
03/23/2005EP1517088A2 Method and apparatus for reducing gas turbine engine emissions
03/23/2005EP1517087A1 Method and apparatus to decrease combustor acoustics
03/23/2005CN1598408A Combustor dome assembly of a gas turbine engine having improved deflector plates
03/23/2005CN1598407A Combustor dome assembly of a gas turbine engine having a free floating swirler
03/22/2005US6869082 Turbine spring clip seal
03/22/2005US6868676 Turbine containing system and an injector therefor
03/22/2005US6868675 Apparatus and method for controlling combustor liner carbon formation
03/17/2005US20050058537 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
03/17/2005US20050056022 Method and apparatus to decrease combustor acoustics
03/17/2005US20050056020 Tube cooled combustor
03/17/2005US20050056007 Internal combustion engine catalytic converter
03/17/2005DE4446945B4 Gasbetriebener Vormischbrenner Gas premix burner
03/16/2005EP1515090A1 Thick coated combustor liner
03/16/2005EP1478832A4 Wing structure of air swirling device for internal combustion engine
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