FUEL INJECTION ASSEMBLY BOSS HAVING A COOLING CIRCUIT AND COMBUSTOR PROVIDED THEREWITH

COOLING RING FOR COMBUSTOR SYSTEM

DOVETAIL FEATURES ON PANEL RAILS OR IMPINGEMENT SHEET TO HOLD PANELS

SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERY

WALL MEMBER AND MANUFACTURING METHOD THEREOF

COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

COMBUSTOR WITH DILUTION OPENINGS

COMBUSTOR WITH DILUTION OPENINGS

DILUTION HOLES WITH RIDGE FEATURE FOR GAS TURBINE ENGINES

STEAM COOLING TURBINE ENGINE COMBUSTOR WALL

Cooling combustor wall boss

APPARATUS AND METHOD FOR MITIGATING AIRFLOW SEPARATION AROUND ENGINE COMBUSTOR

MAIN MIXER IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE

Impingement cooling apparatus support structure and method of manufacture

Combustor with a variable volume primary zone combustion chamber

Impingement cooling apparatus for turbomachine

Combustor with a dilution hole structure

Combustor with dilution openings

Combustor liner

Hollow plank design and construction for combustor liner

Turbine engine combustor and combustor liner

Combustor dome-deflector and liner having flexible connections

Combustor liner having cooling dispersing member for localized liner cooling

Combustor with dilution openings

COMBUSTOR WITH DILUTION OPENINGS

Pre-vaporization tube for a turbine engine combustion chamber

Combustor arrangement

Combustor panels for gas turbine engines

Flange cooling structure for gas turbine engine

Combustor with dilution holes

HEAT TRANSFER DEVICE, TURBOMACHINE CASING AND RELATED STORAGE MEDIUM

Combustor having fuel sweeping structures

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE

Gas turbine component with fluid intake hole free of angled surface transitions

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE

Combustion liner

Coolant delivery via an independent cooling circuit

Internally-mounted torch igniters with removable igniter heads

ENGINE COMPONENT ASSEMBLY

Combustor and gas turbine including the same

Cooling insert for a turbomachine

Impingement panel for a turbomachine

Impingement panel support structure and method of manufacture

Impingement plate with cooling tubes and related insert for impingement plate

Deflector for conduit inlet within a combustor section plenum

Dilution holes with ridge feature for gas turbine engines

Preferential flow distribution for gas turbine engine component

Main mixer in an axial staged combustor for a gas turbine engine

MULTI-WALLED STRUCTURE FOR A GAS TURBINE ENGINE

Heat shield panel manufacturing process

Combustor shell with shaped impingement holes

Combustor bulkhead with circular impingement hole pattern

Burner nozzles for well test burner systems

INSPECTION PORT FOR AN ATTRITABLE ENGINE SUPPORT STRUCTURE

Impingement cooling with impingement cells on impinged surface

Combustor panels for gas turbine engines

Combustor panels for gas turbine engines

Combustor of gas turbine engine and method

Combustor floating collar mounting arrangement

Combustor and gas turbine including the same

Backside features with intermitted pin fins

Plug resistant effusion holes for gas turbine engine

Combustor wall assembly for gas turbine engine

COMBUSTOR LINER PANEL WITH MICRO-CIRCUIT CORE COOLING

Impingement cooling dust pocket

Sensor arrangement for measuring gas turbine combustor temperatures

Heatshield for a gas turbine engine

Quench aperture body for a turbine engine combustor

Backside features with intermitted pin fins

BONDED COMBUSTOR WALL FOR A TURBINE ENGINE

Alignment tools and methods for assembling combustors

Combustor cooling panel stud

Combustor cooling panel with flow guide

Dirt tolerant pins for combustor panels

Preferential flow distribution for gas turbine engine component

Combustor cooled quench zone array

System and method for providing compressed air to a gas turbine combustor

Gas turbine engine dual-wall hot section structure

Film cooling a combustor wall of a turbine engine

Flow control wall assembly for heat engine

Method for constructing impingement/effusion cooling features in a component of a combustion turbine engine

Combustion chamber assembly with shingle part and positioning facility

Tapered panel rail

Combustor panel

Systems and methods for combustor panel

Shell and tiled liner arrangement for a combustor

One-piece combustion chamber

Combustion chamber assembly with a flow guiding device comprising a wall element

DUAL-WALL IMPINGEMENT, CONVECTION, EFFUSION COMBUSTOR TILE

Apparatus and method for mitigating airflow separation around engine combustor

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Interrupted midrail for combustor panel

Heat shield panel manufacturing process

And manufacturing process for directed impingement punched plates

Combustor quench aperture cooling

Internally cooled dilution hole bosses for gas turbine engine combustors

Combustion chamber assembly with different curvatures for a combustion chamber wall and a combustion chamber shingle fixed thereto

Combustor heat shield edge cooling

Hooded entrance to effusion holes

Inner cooling shroud for transition zone of annular combustor liner

Combustor panel standoff pin

Impingement cooling features for gas turbines

Undercut combustor panel rail

Pull-plane effusion combustor panel

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Combustor heat shield

Combustor Assembly for a Turbine Engine

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Gas turbine engine components having internal cooling features

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE ENGINE

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE ENGINE

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Combustor chamber arrangement with sealing ring

Gas turbine annular combustor arrangement

Turbine engine with combustor

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine engine

COMBUSTOR IGNITER ASSEMBLY

Combustor and gas turbine including the same

Double skin combustor

Heat shield panels with overlap joints for a turbine engine combustor

Combustor and gas turbine including the same

Gas turbine engine having a flow-conducting assembly formed of nozzles to direct a cooling medium onto a surface

Turbine engine combustion chamber with fixed duct geometry

Dilution holes with ridge feature for gas turbine engines

Combustor with particle collection panel having a plurality of particle collection chambers

Cooling configurations for combustor attachment features

FLOAT WALL COMBUSTOR PANELS HAVING HEAT TRANSFER AUGMENTATION

Dirt collector system

Heat shield with round top pin fins and flat top pin fins for improved manufacturing processes

Cooling path structure for concentrated cooling of seal area and gas turbine combustor having the same

Fuel nozzle heat shield

Combustor panel, combustor, combustion device, gas turbine, and method of cooling combustor panel

Combustion chamber

Method and apparatus for minimizing cross-flow across an engine cooling hole

Combustor panel endrail interface

Combustor, gas turbine including the same and method of distributing compressed air in combustor

Combustor panel mounting systems and methods

COMBUSTOR LINER PANEL END RAIL

Washer for combustor assembly

Dual-fuel fuel nozzle with liquid fuel tip

Combustion chamber of a turbine engine

Combustor liner with gasket for gas turbine engine

Impingement cooled components having integral thermal transfer features

Regulated combustor liner panel for a gas turbine engine combustor

Hybrid dimple-and-void auxetic structures with engineered patterns for customized NPR behavior

Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor

Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor

Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor

Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor

Combustor liner panel shell interface for a gas turbine engine combustor

Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor

Non-planar combustor liner panel for a gas turbine engine combustor

Non-planar combustor liner panel for a gas turbine engine combustor

Arrangement for a gas turbine combustion engine

ACOUSTIC DAMPING SYSTEM FOR A COMBUSTOR OF A GAS TURBINE ENGINE

Coolable wall element with impingement plate

ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT

Combustion chamber and a combustion chamber fuel injector seal

Cooling structure for vane

Main mixer in an axial staged combustor for a gas turbine engine

Systems and methods for combustor panel

System and method for impingement cooling of turbine system components

COMBUSTION CHAMBER OF A GAS TURBINE

Cast combustor liner panel gating feature for a gas turbine engine combustor

Combustion chamber and a combustion chamber fuel injector seal

Combustion chamber arrangement of a gas turbine and aircraft gas turbine

Acoustic dampening liner cap and gas turbine combustor including the same

Combustor dome heat shield

Burner nozzels for well test burner systems

Systems and methods for combustor panel

Cross fire tube with guide ring and angled cooling holes

Structure for cooling gas turbine engine

Combustion chamber assembly and a combustion chamber segment

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

Combustor assembly for a turbine engine

Combustor liner with dual wall cooling structure

Combustor assembly for a turbine engine

Combustor assembly for a turbine engine

Transition part assembly and combustor including the same

Small exit duct for a reverse flow combustor with integrated cooling elements

Engine component assembly

Combustion chamber having a hook and groove connection

GAS TURBINE COMBUSTION CHAMBER

Gas-turbine combustion chamber with impingement-cooled bolts of the combustion chamber tiles

Cooled component having effusion cooling apertures

Gas turbine engine variable porosity combustor liner

Transition duct assembly with late injection features

Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system

Cooling of integrated combustor nozzle of segmented annular combustion system

Staged fuel and air injectors in combustion systems of gas turbines

ACOUSTIC DAMPING SYSTEM FOR A COMBUSTOR OF A GAS TURBINE ENGINE

Cooling device for cooling platforms of a guide vane ring of a gas turbine

Combustor panels having recessed rail

Combustor and gas turbine

Combustor assembly

Combustion chamber having an annular outer wall with a concave bend

Combustor assembly with a deflector in between swirlers on the base portion

Impingement holes for a turbine engine component

IMPINGEMENT COOLED WALL ARRANGEMENT

Film cooling hole arrangement for acoustic resonators in gas turbine engines

Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine

Impingement cooling arrangement having a snap-in plate

COOLED COMBUSTOR FOR A GAS TURBINE ENGINE

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

Wall of a structural component, in particular of gas turbine combustion chamber wall, to be cooled by means of cooling air

Gas turbine combustion acoustic damping system

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

Gas turbine engine wall assembly with enhanced flow architecture

Liner for a combustor of a gas turbine engine with metallic corrugated member

Array of effusion holes in a dual wall combustor

Engine components with impingement cooling features

Cooling apparatus for a fuel injector

Internally cooled dilution hole bosses for gas turbine engine combustors

Wear pad system for turbine combustion systems and method for coupling wear pad into turbine combustion system

Combustor heat shield with carbon avoidance feature

Article and manifold for thermal adjustment of a turbine component

Combustion chamber and a combustion chamber segment

Film cooling a combustor wall of a turbine engine

Stepped heat shield for a turbine engine combustor

Sealed conical-flat dome for flight engine combustors

Combustor tile

Cooling a quench aperture body of a combustor wall

CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGINE COMBUSTOR

Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine

Combustor liners with rotatable air guiding caps

Angled impingement inserts with cooling features

Cooling flow for leading panel in a gas turbine engine combustor

Thermal mechanical dimple array for a combustor wall assembly

System and method having fuel nozzle

Combustor dilution hole cooling system

Cooling an igniter body of a combustor wall

Combustor dome heat shield

Cooling a combustor heat shield proximate a quench aperture

Combustor heat shield

Combustor panels and configurations for a gas turbine engine

Combustor quench aperture cooling

Cooling a quench aperture body of a combustor wall

Co-swirl orientation of combustor effusion passages for gas turbine engine combustor

Flow sleeve deflector for use in gas turbine combustor

Heat shield for a combustor

Cooling a multi-walled structure of a turbine engine

Gas turbine engine wall assembly with offset rail

Turbine engine multi-walled structure with internal cooling element(s)

Turbine engine multi-walled structure with cooling element(s)

Turbine engine combustor heat shield with multi-angled cooling apertures

Turbine engine combustor heat shield with one or more cooling elements

Sequential liner for a gas turbine combustor

Combustor wall with tapered cooling cavity

Passage geometry for gas turbine engine combustor

Bonded combustor wall for a turbine engine

Heat shield panels with overlap joints for a turbine engine combustor

Combustion chamber having axially extending and annular coolant manifolds

COMBUSTOR LINER EFFUSION COOLING HOLES

Bore-cooled film dispensing pedestals

Wall for a hot gas channel in a gas turbine

Sealed combustor liner panel for a gas turbine engine

Hybrid through holes and angled holes for combustor grommet cooling

Gas turbine engine wall assembly with support shell contour regions

Contoured dilution passages for gas turbine engine combustor

Boss for combustor panel

Fuel injector guide(s) for a turbine engine combustor

Gas turbine engine combustor bulkhead assembly

Cooled wall assembly for a combustor and method of design

Fuel lance cooling for a gas turbine with sequential combustion

Lobe lance for a gas turbine combustor

Nozzle guide for a combustor of a gas turbine engine

Impingement film-cooled floatwall with backside feature

Combustor wall aperture body with cooling circuit

Can combustion chamber

GAS TURBINE ENGINE COMBUSTOR LINER PANEL

Gas turbine engine combustor liner panel

Sealing device for a gas turbine combustor

Gas turbine engine combustor liner panel

Liner element for a combustor, and a related method

Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling

Cooled component

Combustor cap assembly

Combustor cap assembly

Combustor cap assembly

Combustor panel T-junction cooling

Gas turbine system with a transition duct having axially extending cooling channels

Active cooling of grommet bosses for a combustor panel of a gas turbine engine

Additive manufactured surface finish

Finned ignitor grommet for a gas turbine engine

Dilution hole assembly

Self-cooled orifice structure

Combustor cooling structure

Gas turbine engine component with upstream-directed cooling film holes

Heat-transfer device and gas turbine combustor with same

Impingement cooled wall arrangement

Annular combustion chamber of a gas turbine and gas turbine with such a combustion chamber

Combustor liners with U-shaped cooling channels