157477 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
Sub-classes:GAS TURBINE ENGINE AND FUEL INJECTOR ASSEMBLY THEREFOR
#2METHOD FOR INJECTING A HYDROGEN-AIR MIXTURE FOR A TURBINE ENGINE BURNER
#3DILUTION HOLES WITH RIDGE FEATURE FOR GAS TURBINE ENGINES
#4Combustor with fuel and air mixing plenum
#5EXHAUST MIXER WITH PROTRUSIONS
#6Gas turbine
#7GUIDING ARRAY
#8Method and device for recursive sequential combustion
#9Gas turbine engine exhaust diffuser having multiple inclined surfaces at different angles
#10Combustion quality spectrum
#11Gas turbine engine
#12Tubular combustion chamber system and gas turbine unit having a tubular combustion chamber system of this type
#13Gas turbine combustor structure
#14INTEGRATED PROCESS FOR PRODUCING ACETYLENE
#15Dilution holes with ridge feature for gas turbine engines
#16System and method for a direct emission and diffusion of high-pressure combustion with exhaust into feed-water from a combustion barrel
#17Fuel manifolds
#18Internal fuel manifolds
#19Tangential onboard injector inlet extender
#20Selectable mode ramjet/rocket jet engine
#21DIFFUSER CASE HEATSHIELDS FOR GAS TURBINE ENGINES
#22Fuel manifolds
#23Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
#24COOLING HOLE FOR A GAS TURBINE ENGINE COMPONENT
#25System for combustor cooling and trim air profile control
#26Curved seal with relief cuts for adjacent gas turbine components
#27Method of holding flame with no combustion instability, low pollutant emissions, least pressure drop and flame temperature in a gas turbine combustor and a gas turbine combustor to perform the method
#28Combustion chamber with a hot compressed air deflector, in particular for a turbine intended for producing energy, in particular electrical energy
#29COMBUSTOR IGNITER ASSEMBLY
#30Fuel and air injection handling system for a combustor of a rotating detonation engine
#31Modulated combustor bypass
#32Aft frame assembly for gas turbine transition piece
#33Turbulence generating structure for liner cooling enhancement and gas turbine combustor having the same
#34Dilution holes with ridge feature for gas turbine engines
#35Canted combustor for gas turbine engine
#36Flow element and method for coating a flow element
#37Dirt collector system
#38Scramjets and associated aircraft and methods
#39Combustor for use in a turbine engine
#40Thermoinsulating tile for a combustion chamber of a gas turbine
#41Micro turbine generator with guide vane structure
#42Combustor with axially staged fuel injection
#43COMBUSTION CHAMBER
#44Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine
#45Combustion liner cooling
#46METHOD AND COMPUTER-READABLE MODEL FOR ADDITIVELY MANUFACTURING DUCTING ARRANGEMENT FOR A COMBUSTION SYSTEM IN A GAS TURBINE ENGINE
#47SUBSTRATE WITH SHAPED COOLING HOLES
#48Combustor assembly
#49Cooled Combustor Case with Over-Pressurized Cooling Air
#50Cooling system for fuel nozzles within combustor in a turbine engine
#51Cooling hole patterned surfaces
#52Rotating pulse detonation engine, power generation system including the same, and methods of making and using the same
#53Apparatus and method for air extraction at a gas turbine engine combustor
#54Sequential combustion arrangement with cooling gas for dilution
#55Gas turbine engine combustor and method of forming same
#56Trapped vortex cavity staging in a combustor
#57Igniter assembly for a gas turbine engine
#58SELECTABLE MODE RAMJET/ROCKET JET ENGINE
#59Flow sleeve deflector for use in gas turbine combustor
#60Turbine engine combustor heat shield with multi-height rails
#61THERMALLY EXPANDABLE TRANSITION PIECE
#62Atomizer and combustion device using the same
#63COMBUSTION HOLE INSERT WITH INTEGRATED FILM RESTARTER
#64TUBULAR COMBUSTION CHAMBER HAVING A FLAME TUBE END REGION AND GAS TURBINE
#65COMBUSTION CHAMBER FOR A GAS TURBINE, AND TOOL AND METHOD FOR PRODUCING COOLING DUCTS IN A GAS TURBINE COMPONENT
#66Gas turbine engine combustor bulkhead assembly
#67METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS
#68Sealing device for a gas turbine combustor
#69Fuel nozzle
#70Turbine engine diffuser assembly with airflow mixer
#71Apparatus and method incorporating a transition AFT support for a gas turbine engine
#72Method and tool for installation of a transition duct
#73Cylinder of combustor, method of manufacturing of cylinder of combustor, and pressure vessel
#74Gas turbine system with a transition duct having axially extending cooling channels
#75Debris removal system
#76Cooling hole for a gas turbine engine component
#77Gas turbine engine component with combined mate face and platform cooling
#78Combustor assembly with chutes
#79Combustor liners with U-shaped cooling channels
#80Combustor heat shield for a gas turbine engine
#81Combustor for gas turbine engine
#82Conjoined grommet assembly for a combustor
#83CONTINUOUS DETONATION WAVE TURBINE ENGINE
#84Combustion chamber of a gas turbine
#85Combustion chamber of a gas turbine
#86Inner diffuser case struts for a combustor of a gas turbine engine
#87Combustor igniter assembly
#88Liner, flow sleeve and gas turbine combustor each having cooling sleeve
#89GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY
#90Combustor for a sequential gas turbine having a deflection unit between first and second combustion chambers
#91Swirling midframe flow for gas turbine engine having advanced transitions
#92GAS TURBINE COMBUSTOR WITH TILE HAVING ACCESS HOLE FOR SPARK PLUG
#93Gas turbine combustor with annular flow sleeves for dividing airflow upstream of premixing passages
#94COMBUSTOR LINER STOP
#95Annular combustion chamber in a turbine engine
#96RIJKE TYPE COMBUSTION ARRANGEMENT AND METHOD
#97Air regulation for film cooling and emission control of combustion gas structure
#98Slinger combustor
#99Elliptical air opening at an upstream end of a fuel injector shroud and a gas turbine engine combustion chamber
#100GAS TURBINE COMBUSTION CHAMBER
#101Gas turbine combustor including burner having plural gaseous fuel manifolds
#102Systems and Methods for Adverse Combustion Avoidance and Correction
#103System and method for fuel and steam injection within a combustor
#104Compressed air energy storage system having variable generation modes
#105Gas turbine
#106Retaining collar for a gas turbine combustion liner
#107Self-sealing tube for a gas turbine secondary air system
#108Can annular combustion arrangement with flow tripping device
#109COMBUSTION CHAMBER INSERTS AND ASSOCIATED METHODS OF USE AND MANUFACTURE
#110Casing for a gas turbine engine
#111Gas turbine combustor having counterflow injection mechanism and method of use
#112System and method for flow control in gas turbine engine
#113System and method for flow control in gas turbine engine
#114METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR
#115Tunable transition duct side seals in a gas turbine engine
#116Method for operating a burner and burner, in particular for a gas turbine
#117APPARATUS AND METHOD FOR MINIMIZING AND/OR ELIMINATING DILUTION AIR LEAKAGE IN A COMBUSTION LINER ASSEMBLY
#118Combustor having a flow sleeve
#119Systems and methods of providing high pressure air to a head end of a combustor
#120Combustor Can Flow Conditioner
#121Combustor liner
#122Method and apparatus for operating a turbine engine
#123Counterflow injection mechanism having coaxial fuel-air passages
#124Gas turbine combustor having counterflow injection mechanism
#125Turbine exhaust catalyst
#126System and method for improving thermal efficiency of dry low emissions combustor assemblies
#127Combustor inlet plenum and baffle