157531 ⎘
Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor Effusion cooled combustion chamber walls or domes
CYLINDRICAL BODY
#2COMBUSTOR AND POWER GENERATOR INCLUDING THE SAME
#3SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERY
#4CONVECTION COOLING AT LOW EFFUSION DENSITY REGION OF COMBUSTOR PANEL
#5COOLING SYSTEM AND METHOD FOR COMBUSTORS
#6COMBUSTOR OF GAS TURBINE
#7ANNULAR DOME ASSEMBLY FOR A COMBUSTOR
#8DILUTION HOLES WITH RIDGE FEATURE FOR GAS TURBINE ENGINES
#9GAS TURBINE ENGINE COMBUSTOR WITH A SET OF DILUTION PASSAGES
#10DOME-DEFLECTOR JOINT COOLING ARRANGEMENT
#11MAIN MIXER IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE
#12DOME-DEFLECTOR FOR A COMBUSTOR OF A GAS TURBINE
#13Hollow plank design and construction for combustor liner
#14Annular dome assembly for a combustor
#15Coupling a fuel nozzle purge flow directly to a swirler
#16Controlling soot
#17Combustor with dilution holes
#18SYSTEM AND METHOD FOR COMBUSTION OF NON-GASEOUS FUELS AND DERIVATIVES THEREOF
#19Effusion cooling for dilution/quench hole edges in combustor liner panels
#20Coating occlusion resistant effusion cooling holes for gas turbine engine
#21Gas turbine component with fluid intake hole free of angled surface transitions
#22COMBUSTOR
#23Method for manufacturing an engine component with a cooling duct arrangement and engine component
#24Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#25Impingement plate with cooling tubes and related insert for impingement plate
#26Dilution holes with ridge feature for gas turbine engines
#27Main mixer in an axial staged combustor for a gas turbine engine
#28Plug resistant effusion holes for gas turbine engine
#29Combustion chamber with particle separator
#30Convection cooling at low effusion density region of combustor panel
#31Combustor bulkhead with circular impingement hole pattern
#32Combustor liner with shield holes
#33Combustor panel
#34System and method for combustion of non-gaseous fuels and derivatives thereof
#35Liner for a combustor with strain isolated inserts
#36Combustor panels for gas turbine engines
#37Effusion cooling for dilution/quench hole edges in combustor liner panels
#38Plug resistant effusion holes for gas turbine engine
#39COMBUSTOR TILE FOR A COMBUSTOR OF A GAS TURBINE ENGINE
#40Combustor heat shield panel
#41Liner cooling structure with reduced pressure losses and gas turbine combustor having same
#42HGP component with effusion cooling element having coolant swirling chamber
#43Quench aperture body for a turbine engine combustor
#44Combustor panel stud cooling effusion through heat transfer augmentors
#45Combustor cooling panel stud
#46Combustor cooling panel with flow guide
#47Combustor and gas turbine including the combustor
#48Combustor cooled quench zone array
#49Plug resistant effusion holes for gas turbine engine
#50System and method for cleaning cooling passages of a combustion chamber
#51Cooling hole with shaped meter
#52Tapered panel rail
#53Cooled grommet for a combustor wall assembly
#54DUAL-WALL IMPINGEMENT, CONVECTION, EFFUSION COMBUSTOR TILE
#55Double wall combustors with strain isolated inserts
#56Combustor quench aperture cooling
#57Converging duct with elongated and hexagonal cooling features
#58Combustor heat shield edge cooling
#59Hooded entrance to effusion holes
#60Burner with fuel and air supply incorporated in a wall of the burner
#61Combustor panel standoff pin
#62Pull-plane effusion combustor panel
#63Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#64Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#65Combustor heat shield
#66W501D5/D5A DF42 combustion system
#67Gas turbine annular combustor arrangement
#68Apparatus and method for mitigating particulate accumulation on a component of a gas turbine engine
#69Heat shield panels with overlap joints for a turbine engine combustor
#70Dilution holes with ridge feature for gas turbine engines
#71Combustor mixer purge cooling structure
#72Combustor with particle collection panel having a plurality of particle collection chambers
#73Cooling configuration for combustor attachment feature
#74Cooling configurations for combustor attachment features
#75Cooling configurations for combustor attachment features
#76COOLING CONFIGURATIONS FOR COMBUSTOR ATTACHMENT FEATURES
#77Cooling configurations for combustor attachment features
#78Dirt collector system
#79Combustor panel, combustor, combustion device, gas turbine, and method of cooling combustor panel
#80End rail mate-face low pressure vortex minimization
#81Engine component with hollow turbulators
#82Combustor panel standoffs with cooling holes
#83Auxiliary torch ignition
#84System and method for cleaning cooling passages of a combustion chamber
#85Gas turbine engine component having engineered vascular structure
#86Combustor panel endrail interface
#87Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#88Combustion cylinder, gas turbine combustor, and gas turbine
#89Gas turbine engine components with air-cooling features, and related methods of manufacturing the same
#90Combustor panel cooling arrangements
#91Combustor liner with gasket for gas turbine engine
#92Impingement cooled components having integral thermal transfer features
#93REDUCING FILM SCRUBBING IN A COMBUSTOR
#94Regulated combustor liner panel for a gas turbine engine combustor
#95System and method for combustion of non-gaseous fuels and derivatives thereof
#96Combustion chamber shingle arrangement of a gas turbine
#97Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor
#98Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
#99Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor
#100Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
#101WALL COMPONENT OF A GAS TURBINE WITH IMPROVED COOLING
#102Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
#103Non-planar combustor liner panel for a gas turbine engine combustor
#104Non-planar combustor liner panel for a gas turbine engine combustor
#105Combustor assembly for a gas turbine engine
#106TURBINE ENGINE ASSEMBLY INCLUDING A ROTATING DETONATION COMBUSTOR
#107Plate-shaped structural component of a gas turbine
#108Main mixer in an axial staged combustor for a gas turbine engine
#109Gas turbine engine combustor main mixer with vane supported centerbody
#110Gas turbine combustion chamber with wall contouring
#111Annular wall of a combustion chamber with optimised cooling
#112COMBUSTION CHAMBER OF A GAS TURBINE
#113Cast combustor liner panel radius for gas turbine engine combustor
#114Cooling hole with shaped meter
#115Combustor liner with dual wall cooling structure
#116Auxetic Structures With Distorted Projection Slots In Engineered Patterns To Provide NPR Behavior And Improved Stress Performance
#117Combustor Effusion Plate Assembly
#118Combustion chamber having a hook and groove connection
#119GAS TURBINE COMBUSTION CHAMBER
#120Turbomachine combustion chamber
#121Gas turbine engine variable porosity combustor liner
#122Transition duct assembly with late injection features
#123Operation and turndown of a segmented annular combustion system
#124Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
#125Combustor panels having recessed rail
#126Combustor assembly for a gas turbine engine
#127Combustor assembly with a deflector in between swirlers on the base portion
#128CMC articles having small complex features for advanced film cooling
#129Wall of a structural component, in particular of gas turbine combustion chamber wall, to be cooled by means of cooling air
#130Gas turbine combustion acoustic damping system
#131Gas turbine engine wall assembly with enhanced flow architecture
#132Liner for a combustor of a gas turbine engine with metallic corrugated member
#133Effusion cooling holes
#134Cooling hole patterned surfaces
#135Array of effusion holes in a dual wall combustor
#136Axially staged micromixer cap
#137Afterburner and aircraft engine
#138Turbine engine assembly and method of assembling the same
#139Heat shield labyrinth seal
#140Cooling apparatus for a fuel injector
#141Combustor cooling system
#142Combustor heat shield with carbon avoidance feature
#143Sequential combustion arrangement with cooling gas for dilution
#144Combustion chamber and a combustion chamber segment
#145Gas turbine engine combustor and method of forming same
#146Trapped vortex cavity staging in a combustor
#147Stepped heat shield for a turbine engine combustor
#148Sealed conical-flat dome for flight engine combustors
#149Combustor tile
#150CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGINE COMBUSTOR
#151D5/D5A DF-42 integrated exit cone and splash plate
#152W501 D5/D5A DF42 COMBUSTION SYSTEM
#153Dilution passage arrangement for gas turbine engine combustor
#154Multi-streamed dilution hole configuration for a gas turbine engine
#155Cooled grommet for a combustor wall assembly
#156Thermal mechanical dimple array for a combustor wall assembly
#157Combustor dilution hole cooling system
#158Cooling an igniter body of a combustor wall
#159Combustor dome heat shield
#160Cooling a combustor heat shield proximate a quench aperture
#161Combustor heat shield
#162Combustor panels and configurations for a gas turbine engine
#163Combustor quench aperture cooling
#164Co-swirl orientation of combustor effusion passages for gas turbine engine combustor
#165Combustor having a beveled grommet
#166Attachment stud on a combustor floatwall panel with internal cooling holes
#167Gas turbine engine wall assembly with offset rail
#168Turbine engine combustor heat shield with multi-angled cooling apertures
#169Turbine engine combustor heat shield with one or more cooling elements
#170Combustion chamber and a combustion chamber segment
#171COMBUSTOR AND HEAT SHIELD CONFIGURATIONS FOR A GAS TURBINE ENGINE
#172Combustor wall with tapered cooling cavity
#173Passage geometry for gas turbine engine combustor
#174Sealing of a radial gap between effusion tiles of a gas-turbine combustion chamber
#175Heat shield panels with overlap joints for a turbine engine combustor
#176COMBUSTOR LINER EFFUSION COOLING HOLES
#177Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustor
#178Sealed combustor liner panel for a gas turbine engine
#179Gas turbine engine wall assembly with support shell contour regions
#180Contoured dilution passages for gas turbine engine combustor
#181Separate feedings of cooling and dilution air
#182Cooled wall assembly for a combustor and method of design
#183Impingement film-cooled floatwall with backside feature
#184GAS TURBINE ENGINE COMBUSTOR LINER PANEL
#185Cooled component
#186Gas turbine engine combustor liner panel
#187Liner element for a combustor, and a related method
#188Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling
#189Cooled component
#190Cooled component
#191Combustor and gas turbine having the same
#192Combustor front panel
#193Gas turbine engine component having engineered vascular structure
#194Film cooling circuit for a combustor liner
#195Single-walled combustor for a gas turbine engine and method of manufacture
#196Gas turbine engines with plug resistant effusion cooling holes
#197Heat shield labyrinth seal
#198Combustor cap assembly
#199Combustor cap assembly
#200Combustor panel T-junction cooling
#201Combustor for gas turbine engine
#202Gas turbine system with a transition duct having axially extending cooling channels
#203Combustor heat shield
#204Liner element for a combustor
#205Active cooling of grommet bosses for a combustor panel of a gas turbine engine
#206Annular combustion chamber wall arrangement
#207Damage tolerant cooling of high temperature mechanical system component including a coating
#208Conical-flat heat shield for gas turbine engine combustor dome
#209Combustor cooling structure
#210Gas turbine engine component with combined mate face and platform cooling
#211Gas turbine engine component with upstream-directed cooling film holes
#212Combustor heat shield
#213Combustor assembly with chutes
#214Annular combustion chamber of a gas turbine and gas turbine with such a combustion chamber
#215Combustor liners with U-shaped cooling channels
#216Multiple ventilated rails for sealing of combustor heat shields
#217Turbine engine wall having at least some cooling orifices that are plugged
#218Combustion liner with bias effusion cooling
#219Conjoined grommet assembly for a combustor
#220Gas turbine engine combustor basket with inverted platefins
#221Gas turbine combustion acoustic damping system
#222Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques
#223Microcircuit cooling for gas turbine engine combustor
#224Washer of a combustion chamber tile of a gas turbine
#225Combustion device for a gas turbine
#226TURBOMACHINE COMBUSTOR ASSEMBLY
#227GAS TURBINE COMBUSTOR WITH TILE HAVING ACCESS HOLE FOR SPARK PLUG
#228Heat shield for a gas turbine combustion chamber
#229Gas turbine combustion liner with triangular heat transfer element
#230Hot gas path component with impingement and pedestal cooling
#231Device for cooling a wall of a component
#232Reverse bulk flow effusion cooling
#233Component for attaching to a wall
#234Turbomachine combustion chamber shell ring
#235Asymmetric combustor heat shield panels
#236Burner arrangement and method for operating a burner arrangement
#237COMBUSTOR OF A GAS TURBINE WITH PRESSURE DROP OPTIMIZED LINER COOLING
#238Gas turbine engine component having foam core and composite skin with cooling slot
#239Methods and apparatus for inspecting cooling holes
#240Gas turbine combustion chamber tile having effusion cooling holes including straight and offset sections
#241Mixing arrangement for mixing a fuel with a stream of oxygen containing gas
#242Asymmetric baseplate cooling with alternating swirl main burners
#243Combustors with complex shaped effusion holes
#244Combustor skin assembly for gas turbine engine
#245Micro gas turbine engine for powering a generator
#246Turbine blade
#247Slinger combustor
#248Gas turbine engine variable porosity combustor liner
#249Annular wall of a combustion chamber with improved cooling at the level of primary and/or dilution holes
#250Check valve for propulsive engine combustion chamber
#251Combustor heat shield with carbon avoidance feature
#252Dual-wall impingement, convection, effusion combustor tile
#253Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
#254Method of manufacturing a wall
#255Combustion chamber wall
#256Effusion plate using additive manufacturing methods
#257Combustion chamber with cooling passage in fastener arrangement joining inner and outer walls
#258Gas turbine engine combustor with integrated combustor vane
#259Combustion chamber tile of a gas turbine
#260Combustion system
#261Reverse-flow annular combustor for reduced emissions
#262Combustor Bulkhead Cooling Array
#263Cooling for combustor liners with accelerating channels
#264Gas turbine engine combustor liner
#265Combustor bulkhead assembly
#266Combustor liner cooling assembly
#267Turbine engine combustor and stator vane assembly
#268Turbine engine combustor wall with non-uniform distribution of effusion apertures
#269Annular combustion chamber for a turbine engine including improved dilution openings
#270Method of forming a cooling hole by laser drilling
#271Combustor having a beveled grommet
#272Combustor heat shield
#273Tri-lobed cooling hole and method of manufacture
#274Combustor for gas turbine engine
#275Fuel injection system for turbojet engine and method of assembling such an injection system
#276EFFUSION COOLED NOZZLE AND RELATED METHOD
#277Multi-pierced combustion chamber with counter-rotating tangential flows
#278WALL ELEMENTS FOR GAS TURBINE ENGINES
#279Microcircuit cooling for gas turbine engine combustor
#280BURNER, GAS TURBINE COMBUSTOR, BURNER COOLING METHOD, AND BURNER MODIFYING METHOD
#281Turbomachine combustion chamber having a perforated chamber end wall and with no deflector
#282Methods and systems for cooling a transition nozzle
#283Reverse-flow annular combustor for reduced emissions
#284Head part of an annular combustion chamber
#285Internal combustion engine hot gas path component with powder metallurgy structure
#286Cooled double walled article
#287GAS TURBINE ENGINE COMPONENT
#288Aft frame and method for cooling aft frame
#289Hole producing system
#290Combustion liner with open cell foam and acoustic damping layers
#291Gas-turbine combustion chamber with a cooling-air supply device
#292METHOD OF FABRICATING A COMPONENT USING A FUGITIVE COATING
#293SUBSTRATE WITH SHAPED COOLING HOLES AND METHODS OF MANUFACTURE
#294SYSTEM AND METHOD FOR COOLING A NOZZLE
#295System and method for cooling a nozzle
#296FUEL INJECTION ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME
#297Burner arrangement with deflection elements for deflecting cooling air flow
#298Method of repairing a gas turbine engine combustor
#299Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations
#300Combustor head plate assembly with impingement