157531 ⎘
Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor Effusion cooled combustion chamber walls or domes
Gas turbine combustion device
#302GAS TURBINE COMBUSTORS WITH DUAL WALLED LINERS
#303Various layered gas turbine engine component constructions
#304Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel
#305Apparatus for combusting a fuel at high pressure and high temperature, and associated system
#306Combustor tile mounting arrangement
#307Effusion cooled dual wall gas turbine combustors
#308Cooling arrangement for a combustion chamber
#309Combustion chamber head of a gas turbine
#310System and method for thermal control in a cap of a gas turbine combustor
#311COOLED HYBRID STRUCTURE FOR GAS TURBINE ENGINE AND METHOD FOR THE FABRICATION THEREOF
#312Thimble Fan for a Combustion System
#313COMBUSTOR CAP WITH SHAPED EFFUSION COOLING HOLES
#314COMBINED CONVECTION/EFFUSION COOLED ONE-PIECE CAN COMBUSTOR
#315Gas Turbine Combustion System
#316Effusion cooled one-piece can combustor
#317Combustion system
#318COOLING A ONE-PIECE CAN COMBUSTOR AND RELATED METHOD
#319Fuel injector arrangement having porous premixing chamber
#320Combustors with inserts between dual wall liners
#321COMBUSTION PRE-CHAMBER
#322DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE
#323DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE
#324Combustor with improved cooling holes arrangement
#325Combustor for a gas turbine engine with effusion cooled baffle
#326Effusion cooling techniques for combustors in engine assemblies
#327COMBUSTOR SYSTEM AND METHOD OF REDUCING COMBUSTION INSTABILITY AND/OR EMISSIONS OF A COMBUSTOR SYSTEM
#328Gas turbine engine reverse-flow combustor
#329Impingement and effusion cooled combustor component
#330Combustor liner replacement panels
#331Hole pattern for gas turbine combustor
#332Combustor dynamic attenuation and cooling arrangement
#333Wall cooling arrangement
#334Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell
#335Scalable pyrospin combustor
#336Combustion chamber lining
#337EFFUSION COOLING FOR GAS TURBINE COMBUSTORS
#338Combustor end cap assembly
#339System for injecting a mixture of air and fuel into a turbomachine combustion chamber
#340BURNER FOR A COMBUSTOR OF A TURBOGROUP
#341Method of producing effusion holes
#342Gas-turbine combustion chamber wall
#343DEVICE FOR INJECTING A MIXTURE OF AIR AND FUEL, AND COMBUSTION CHAMBER AND TURBOMACHINE WHICH ARE PROVIDED WITH SUCH A DEVICE
#344Annular combustion chamber for a turbomachine
#345Wall elements for gas turbine engine components
#346Combustor heat shield
#347Injection assembly for a combustor
#348Noise reducing combustor
#349Combustor with improved swirl
#350Combustor liner for gas turbine engine
#351Method of Optimum Controlled Outlet, Impingement Cooling and Sealing of a Heat Shield and a Heat Shield Element
#352Gas turbine engine combustor with improved cooling
#353Combustor
#354Wall elements for gas turbine engine combustors
#355Segmented effusion cooled gas turbine engine combustor
#356Performance of a combustion chamber by multiple wall perforations
#357Annular combustion chamber for a turbomachine
#358Burner, gas turbine combustor, burner cooling method, and burner modifying method
#359Gas turbine engine combustor with improved cooling
#360Method for controlling carbon formation on repaired combustor liners
#361Combustor cooling hole pattern
#362Inboard radial dump venturi for combustion chamber of a gas turbine
#363Cooled gas turbine transition duct
#364Methods and apparatus for cooling gas turbine engine components
#365Gas turbine combustor heat shield panel or exhaust panel including a cooling device
#366Combustor exit duct
#367Combustor and method of improving manufacturing accuracy thereof
#368Combustor heat shield and method of cooling
#369Film effectiveness enhancement using tangential effusion
#370Effusion momentum control
#371Combined effusion and thick TBC cooling method
#372Combustion apparatus
#373Transition duct apparatus having reduced pressure loss
#374Uniform effusion cooling method for a can combustion chamber
#375Cooling and sealing design for a gas turbine combustion system
#376Cooling jets
#377Transpiration cooling system
#378Double wall combustor tile arrangement
#379Foam wall combustor construction
#380Combustion liner having cooling holes with stepped lateral sidewalls
#381Turbine cooling system with energy separation
#382Dome structure providing a dome-deflector cavity with counter-swirled airflow