Multiple ventilated rails for sealing of combustor heat shields

Angled impingement insert

Conjoined grommet assembly for a combustor

Combustion chamber arrangement

Fuel nozzle heat shield

Gas turbine engine combustor basket with inverted platefins

Combustor wall assembly for a turbine engine

Interface heat shield for a combustor of a gas turbine engine

COMBUSTOR SECTION OF A GAS TURBINE ENGINE

Gas turbine combustion acoustic damping system

Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques

Combustor igniter assembly

Liner, flow sleeve and gas turbine combustor each having cooling sleeve

Microcircuit cooling for gas turbine engine combustor

Washer of a combustion chamber tile of a gas turbine

Combustor dome heat shield

GAS TURBINE COMBUSTOR WITH TILE HAVING ACCESS HOLE FOR SPARK PLUG

GAS-TURBINE COMBUSTION CHAMBER AND METHOD FOR ITS MANUFACTURE

Impingement cooling arrangement

Combustor cooling structure

HOLE ARRANGEMENT OF LINERS OF A COMBUSTION CHAMBER OF A GAS TURBINE ENGINE WITH LOW COMBUSTION DYNAMICS AND EMISSIONS

Combustor heat-shield cooling via integrated channel

Component for attaching to a wall

Internally cooled transition duct aft frame with serpentine cooling passage and conduit

Turbomachine combustion chamber shell ring

Asymmetric combustor heat shield panels

Burner arrangement and method for operating a burner arrangement

Gas turbine engine with improved combustion liner

Low calorific fuel combustor for gas turbine

Combustion nozzle with floating aft plate

Combustor skin assembly for gas turbine engine

Gas turbine engine combustor with integrated combustor vane having swirler

Combustion chamber for a turbine engine

Impingement cooling mechanism, turbine blade and cumbustor

Impingement cooling mechanism, turbine blade and combustor

Transition duct with divided upstream and downstream portions

System for tuning a combustor of a gas turbine

Combustor heat shield with carbon avoidance feature

Dual-wall impingement, convection, effusion combustor tile

Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes

Gas turbine combustor equipped with heat-transfer device

Method of manufacturing a wall

Flow feed diffuser

Dual fuel nozzle tip assembly with impingement cooled nozzle tip

Combustion chamber with cooling passage in fastener arrangement joining inner and outer walls

Tile fastening arrangement of a gas-turbine combustion chamber

System and method for a multi-wall turbine combustor

Combustor cap assembly

Combustor and a method for cooling the combustor

Assemblies and apparatus related to combustor cooling in turbine engines

Radial flow fuel nozzle for a combustor of a gas turbine

Deformable mounting assembly

Combustor Bulkhead Cooling Array

Cooling for combustor liners with accelerating channels

Gas turbine engine combustor liner

Combustor bulkhead assembly

Gas turbine cooling circuit including a seal for a perforated plate

TURBINE COMPONENT COOLING ARRANGEMENT AND METHOD OF COOLING A TURBINE COMPONENT

Combustor liner cooling assembly

LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM

Turbine engine combustor and stator vane assembly

Combustor cap assembly

Turbine engine combustor wall with non-uniform distribution of effusion apertures

COMBUSTOR LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM

Combustor liner with improved film cooling

Combustor liner with decreased liner cooling

Combustor liner with reduced cooling dilution openings

Combustor liner with convergent cooling channel

Transition duct with late injection in turbine system

Systems and methods for a gas turbine combustor having a bleed duct

Transition nozzle combustion system

Systems and methods for dampening combustor dynamics in a micromixer

Combustor heat shield

Heat shield for a combustor

COMBUSTOR ASSEMBLY WITH IMPINGEMENT SLEEVE HOLES AND TURBULATORS

Combustor and method for distributing fuel in the combustor

Late lean injection system transition piece

SYSTEM OF INTEGRATING BAFFLES FOR ENHANCED COOLING OF CMC LINERS

Combustor having wake air injection

Combustion system having a venturi for reducing wakes in an airflow

Combustor and method for supplying flow to a combustor

COMBUSTOR AND METHOD FOR SUPPLYING FLOW TO A COMBUSTOR

FILM COOLED COMBUSTION LINER ASSEMBLY

System for cooling a multi-tube fuel nozzle

IMPINGEMENT COOLING OF COMBUSTOR LINERS

Combustor resonator section with an internal thermal barrier coating and method of fabricating the same

TURBINE COMBUSTOR AND METHOD FOR TEMPERATURE CONTROL AND DAMPING A PORTION OF A COMBUSTOR

Pin fin arrangement for heat shield of gas turbine engine

WALL ELEMENTS FOR GAS TURBINE ENGINES

COMBUSTOR LINER COOLING SYSTEM

Two stage serial impingement cooling for isogrid structures

Assemblies and apparatus related to integrating late lean injection into combustion turbine engines

Methods relating to integrating late lean injection into combustion turbine engines

Microcircuit cooling for gas turbine engine combustor

Distributed cooling for gas turbine engine combustor

Multi-stage amplification vortex mixture for gas turbine engine combustor

Turbomachine combustor assembly including a vortex modification system

Flow sleeve impingement cooling baffles

SYSTEM AND METHOD FOR ADAPTIVE IMPINGEMENT COOLING

COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME

COMBUSTOR HAVING A PRESSURE FEED

Impingement sleeve and methods for designing and forming impingement sleeve

Turbine combustion system coupling with adjustable wear pad

Method of forming a multi-panel outer wall of a component for use in a gas turbine engine

Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities

Head part of an annular combustion chamber

Cooled double walled article

Apparatus and method for cooling a combustor

Aft frame and method for cooling aft frame

Impingement sleeve and methods for designing and forming impingement sleeve

Combustion chamber having a ventilated spark plug

Method and apparatus for mounting transition piece in combustor

Thermally isolated wall assembly

METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR

Resonator system with enhanced combustor liner cooling

FUEL INJECTION ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME

SYSTEM FOR DAMPING VIBRATION IN A GAS TURBINE ENGINE

Fuel nozzle, gas turbine combustor with the same, and gas turbine with the same

Combustor assemblies for use in turbine engines and methods of assembling same

Fuel atomization dual orifice fuel nozzle

COOLING FLOWPATH DIRT DEFLECTOR IN FUEL NOZZLE

Gas turbine combustion chamber

Turbine transition component formed from an air-cooled multi-layer outer panel for use in a gas turbine engine

Low calorific fuel combustor for gas turbine

Ultra low emissions gas turbine combustor

Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece

Apparatus and method for cooling a combustor cap

Apparatus and method for cooling a combustor

FUEL INJECTION ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME

Burner arrangement with deflection elements for deflecting cooling air flow

Cooling arrangement for a turbine component

Apparatus and filtering systems relating to combustors in combustion turbine engines

Apparatus and filtering systems relating to combustors in combustion turbine engines

Flame tolerant secondary fuel nozzle

Mesh cooled conduit for conveying combustion gases

Ejector purge of cavity adjacent exhaust flowpath

Method of repairing a gas turbine engine combustor

Combustor head plate assembly with impingement

Combustor liner cooling at transition duct interface and related method

Apparatus and method for a fuel nozzle

IMPINGEMENT STRUCTURES FOR COOLING SYSTEMS

Angled vanes in combustor flow sleeve

HYBRID VENTURI COOLING SYSTEM

Gas turbine combustion device

Combustor liner segment seal member

GAS TURBINE COMBUSTORS WITH DUAL WALLED LINERS

Combustor liner segment seal member

Turbulated aft-end liner assembly and cooling method

Impingement cooling plate for a hot gas duct of a thermal machine

GUIDING AN IGNITION SPARK PLUG IN A TURBOMACHINE COMBUSTION CHAMBER

Combustor assembly for a turbine engine with enhanced cooling

Impingement cooled crossfire tube assembly

Impingement cooled transition piece aft frame

Effusion cooled dual wall gas turbine combustors

System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle

Cooling arrangement for a combustion chamber

Washer with cooling passage for a turbine engine combustor

High volume fuel nozzles for a turbine engine

COOLED HYBRID STRUCTURE FOR GAS TURBINE ENGINE AND METHOD FOR THE FABRICATION THEREOF

Thimble, sleeve, and method for cooling a combustor assembly

APPARATUS AND METHOD FOR COOLING GAS TURBINE ENGINE COMBUSTORS

Combustor liner cooling system

PATTERN COOLED COMBUSTOR LINER

Combustion chamber

DUAL WALLED COMBUSTORS WITH IMPINGEMENT COOLED IGNITERS

Gas turbine with welded combustor liners

Interlocking retention strip

Cooling structure of gas turbine combustor

GAS TURBINE COMBUSTOR

COOLING A ONE-PIECE CAN COMBUSTOR AND RELATED METHOD

Ring cooling for a combustion liner and related method

Cooled flameholder swirl cup

GAS TURBINE COMBUSTION CHAMBER

Combustors with inserts between dual wall liners

Eccentric chamfer at inlet of branches in a flow channel

DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE

DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE

Structures with adaptive cooling

Impingement cooled combustor seal

Gas turbine transition duct

Segmented combustor cap

COMBUSTOR SYSTEM AND METHOD OF REDUCING COMBUSTION INSTABILITY AND/OR EMISSIONS OF A COMBUSTOR SYSTEM

Gas turbine engine reverse-flow combustor

Contoured Impingement Sleeve Holes

Thermal machine

Impingement and effusion cooled combustor component

Flow sleeve impingement cooling baffles

Flow sleeve impingement cooling using a plenum ring

Flow sleeve with tabbed direct combustion liner cooling air

COMBUSTOR STRUCTURE

Impingement cooling device

Hole pattern for gas turbine combustor

Combustor

Fuel nozzle

TRANSITION PIECE IMPINGEMENT SLEEVE AND METHOD OF ASSEMBLY

Cooling arrangement for CMC components with thermally conductive layer

Combustion chamber lining

Combustor end cap assembly

Turbomachine combustion chamber

Impingement cooled can combustor

Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber

Combustion chamber of a turbomachine including cooling grooves

Extended impingement cooling device and method

Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters

Hot-gas-ducting housing element, protective shaft jacket and gas turbine system

APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR

Impingement jets coupled to cooling channels for transition cooling

Zero-cross-flow impingement via an array of differing length, extended ports

Gas-turbine combustion chamber wall

Floatwall dilution hole cooling

System for reducing combustor dynamics

Method for impingement air cooling for gas turbines

DEVICE FOR INJECTING A MIXTURE OF AIR AND FUEL, AND COMBUSTION CHAMBER AND TURBOMACHINE WHICH ARE PROVIDED WITH SUCH A DEVICE

Methods and system for cooling integral turbine nozzle and shroud assemblies

Heat Shield Element

Combustor dome panel heat shield cooling

Combustor assembly for gas turbine engine

Splash plate dome assembly for a turbine engine

Combustor with enhanced cooling access

Method and apparatus for cooling gas turbine engine combustors

Method of Optimum Controlled Outlet, Impingement Cooling and Sealing of a Heat Shield and a Heat Shield Element

Methods and system for reducing pressure losses in gas turbine engines

Combustor

Gas turbine combustion chamber wall with dampening effect on combustion chamber vibrations

Method and apparatus for heat shielding gas turbine engines

Transverse wall of a combustion chamber provided with multi-perforation holes

Dual wall combustor liner

Combustion chamber end wall with ventilation

Gas turbine combustor bulkhead panel

Igniter tube and method of assembling same

METHOD AND APPARATUS FOR COOLING GAS TURBINE FUEL NOZZLES

Tile and exo-skeleton tile structure

Heat shield

Method and apparatus for assembling gas turbine engine combustors

High thrust gas turbine engine with improved core system

Waffled impingement effusion method

Heatshielded article

Method and apparatus for cooling combustor liner and transition piece of a gas turbine

Method and apparatus for cooling combustor liner and transition piece of a gas turbine

Cooling structure of gas turbine tail pipe

Method and apparatus for reducing gas turbine engine emissions

Burner for a gas turbine engine

Extended impingement cooling device and method

Bulkhead panel for use in a combustion chamber of a gas turbine engine

Combustion chamber, in particular of a gas turbine

Combustor

Methods and apparatus for cooling turbine engine combustor exit temperatures

Cooling jets

Method and apparatus for reducing gas turbine engine emissions

Combustor

Gas turbine can annular combustor

Methods and apparatus for cooling gas turbine engine combustors

Combustor with additively manufactured combustor body having aft frame with heat transfer augmentation

Additively manufactured combustor liner v-band cooling ring

Boss for a fuel injection assembly having cooling circuit and combustor provided therewith

T-head bolts or hollow flanged bushing with one thread or grooved end in a multi-liner arrangement

Dovetail features on panel rails or impingement sheet to hold panels

Cooling nozzle vanes of a turbine engine

Combustor liner having dilution openings with swirl vanes