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

FLEXIBLE FLANGE DESIGN

MONOLITHIC FUEL NOZZLE ASSEMBLY MANUFACTURED USING ADDITIVE MANUFACTURING

COMPONENTS FOR COMBUSTOR

COMBUSTOR FOR A TURBINE ENGINE INCLUDING AN INSULATING MEMBER

COMBUSTOR OF GAS TURBINE

DOVETAIL FEATURES ON PANEL RAILS OR IMPINGEMENT SHEET TO HOLD PANELS

ASSEMBLY METHOD AND ASSEMBLY DEVICE

ATTACHING POWERPLANT STRUCTURES TOGETHER USING FUEL INJECTOR BOLTS

COMBUSTOR LINER PANELS

GAS TURBINE ENGINE COMBUSTOR HAVING CERAMIC MATRIX COMPOSITE (CMC) LINERS AND CMC DOME

GAS TURBINE ENGINE COMBUSTOR

COUPLING ASSEMBLY FOR A TURBINE ENGINE

COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE

ARTICULATABLE DUCTING SYSTEMS

DOME-DEFLECTOR ASSEMBLY FOR A COMBUSTOR OF A GAS TURBINE

FUEL INJECTION ASSEMBLY HAVING PARTIAL DIRECT INJECTORS

COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME

LINER ASSEMBLY FOR A COMBUSTOR

COMBUSTOR ASSEMBLY FOR A TURBO MACHINE

Support pin for igniter assembly

GAS TURBINE ENGINE

COMBUSTION SECTION WITH A PRIMARY COMBUSTOR AND A SET OF SECONDARY COMBUSTORS

COMBUSTOR OF GAS TURBINE

REINFORCED FILM FLOATWALL FOR A GAS TURBINE ENGINE

COMBUSTOR OF GAS TURBINE

COMBUSTOR ASSEMBLY

TURBINE ENGINE SUPPORT STRUCTURE WITH AIRFLOW PORTS

GAS TURBINE ENGINE WITH IMPROVED HIGH PRESSURE COMPRESSOR LEAKAGE PATH GUIDE STRUCTURE

COMBUSTION MODULE FOR A TURBOMACHINE

Fuel Injectors for Multipoint Arrays

CMC COMBUSTOR DEFLECTOR

GAS TURBINE ENGINE CONFIGURED FOR DECREASED DIFFUSER WINDAGE AND METHOD OF ASSEMBLING THE SAME

ANNULAR DOME ASSEMBLY FOR A COMBUSTOR

Combustion section with a casing shielding

Fuel injector assembly for gas turbine engine

COMBUSTOR SECTION SUPPORT STRUCTURES

Combustor section support structures

COMBUSTOR SECTION SUPPORT STRUCTURES

COMBUSTOR FOR A GAS TURBINE ENGINE

Dome-deflector assembly for a combustor of a gas turbine

COMBUSTOR DEFLECTOR ASSEMBLY

COUPLING ASSEMBLY FOR A TURBINE ENGINE

COMPONENTS FOR COMBUSTOR

Combustor assembly for a turbine engine

Radiation shield for a gaseous fuel circuit

TONGUE JOINT INCLUDING MATING CHANNEL FOR COOLING

Combustion chamber with wall cooling

Coupling assembly for a turbine engine

COMPONENTS FOR COMBUSTOR

CTE MATCHING HANGER SUPPORT FOR CMC STRUCTURES

DOME-DEFLECTOR JOINT COOLING ARRANGEMENT

Combustion module for a turbomachine

Subassembly comprising means for compensating for a difference in expansion

FUEL INJECTOR ASSEMBLY FOR A TURBINE ENGINE

Combustor casing component for a gas turbine engine

Fuel manifold adapter

COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

Combustor with a dilution hole structure

Combustor chamber mesh structure

Method of optimising gas turbine engine combustion equipment performance

Hollow plank design and construction for combustor liner

Plank hanger structure for durable combustor liner

Combustor and gas turbine

Combustor deflector assembly

Liner assembly for a combustor

Dome-deflector joint cooling arrangement

Combustor dome-deflector and liner having flexible connections

Combustor with a variable primary zone combustion chamber

Spark plug for a single-piece combustion chamber

COMBUSTION CHAMBER HAVING A CERAMIC HEAT SHIELD AND SEAL

Tongue joint including mating channel for cooling

Ceramic composite combustor dome and liners

Combustor swirler to CMC dome attachment

Combustor swirler to dome attachment

ANNULAR COMBUSTOR DILUTION WITH SWIRL VANES FOR LOWER EMISSIONS

Combustor liner

ASSEMBLY FOR A TURBINE ENGINE

Combustion cylinder mounting method and combustion cylinder mounting jig

Combustor assembly with moveable interface dilution opening

Fuel manifold adapter

Integral ceramic matrix composite fastener with non-polymer rigidization

Combustor for a gas turbine engine

Combustor for a gas turbine engine

Method for mounting combustor component, combustor component set, hanging jig, and hanging jig set

COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

Turbo machine combustor assembly having separable portions coupled at a fitted interface

Integral ceramic matrix composite fastener with polymer rigidization

CMC combustor panel attachment arrangement

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

Mounting a ceramic component to a non-ceramic component in a gas turbine engine

FLOW CONTROL WALL FOR HEAT ENGINE

Combustion chamber comprising means for cooling an annular casing zone downstream of a chimney

CMC combustor deflector

MODULE OF AN AIRCRAFT TURBINE ENGINE

TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE

TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE

Piston ring assembly for a turbine engine

Resonator, method for producing such a resonator, and combustor arrangement equipped with such a resonator

Fuel injector assembly for a turbine engine

PRESSURE REGULATED PISTON SEAL FOR A GAS TURBINE COMBUSTOR LINER

Combustor assembly for a turbine engine

Spall plate for consumable combustor support structures

Combustion chamber

Trapped vortex combustor for a gas turbine engine with a driver airflow channel

Aerodynamic component for a gas turbine engine

Combustion chamber for a turbomachine

Preferential flow distribution for gas turbine engine component

Gas turbine engine combustor with ceramic matrix composite liner

Combustor and gas turbine including the same

Combustor assembly for a turbine engine

Combustion liners and attachments for attaching to nozzles

Sleeve assemblies and methods of fabricating same

RAIL AND TUBE ASSEMBLY

Liner cooling device, combustor including same, and gas turbine including same

Fuel nozzle of gas turbine combustor and manufacturing method thereof, and gas turbine combustor

Combustor for a gas turbine engine with ceramic matrix composite sealing element

Mounting a ceramic component to a non-ceramic component in a gas turbine engine

Combustor for a gas turbine engine with ceramic matrix composite heat shield

Combustor for a gas turbine engine with ceramic matrix composite heat shield and seal retainer

Spall plate for consumable combustor support structures

Combustor assembly for a turbine engine

Axial retention assembly for combustor components of a gas turbine engine

Axial retention assembly for combustor components of a gas turbine engine

Combustor of gas turbine engine and method

Fuel injectors for multipoint arrays

COMBUSTOR MOUNTING STRUCTURES FOR GAS TURBINE ENGINES

Combustor floating collar mounting arrangement

Anti-rotation feature for a burner

CMC combustor deflector

Integrated additive fuel injectors for attritable engines

Pressure regulated piston seal for a gas turbine combustor liner

AERODYNAMIC COMPONENT FOR A GAS TURBINE ENGINE

Single cavity trapped vortex combustor with CMC inner and outer liners

Beaded finger attachment

Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly

Gas turbine engine

Captured compliant coil seal

Combustor panel stud cooling effusion through heat transfer augmentors

Combustor cooling panel stud

Combustor cooling panel with flow guide

Stand-off device for double-skin combustor liner

COMBUSTOR SLIDING JOINT

Combustor, a tile holder and a tile

Preferential flow distribution for gas turbine engine component

Combustor assembly for a turbine engine

Ring assembly for double-skin combustor liner

Thermally coupled CMC combustor liner

Flange stress-reduction features

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

Retention hardware

Integral ceramic matrix composite fastener with non-polymer rigidization

Gas turbine combustor

Axial stop configuration for a combustion liner

Cross fire tube retention system

Silo combustion chamber and method for retrofitting same

Transition piece

Method and apparatus for mounting a transition duct in a gas turbine engine

Combustor liner attachment assembly for gas turbine engine

Combustor liner attachment assembly for gas turbine engine

Consumable support structures for additively manufactured combustor components

Attachment for high temperature CMC combustor panels

Combustor heat shield and attachment features

Combustor assembly for a turbo machine

Flow control wall for heat engine

Combustion chamber assembly with shingle part and positioning facility

Tapered panel rail

Shell and tiled liner arrangement for a combustor

DUAL-WALL IMPINGEMENT, CONVECTION, EFFUSION COMBUSTOR TILE

Airfoil fluid curtain to mitigate or prevent flow path leakage

Flow path assembly with airfoils inserted through flow path boundary

Internal manifold for multipoint injection

Combustor heat shield sealing

Combustor shell attachment

Combustion module for a gas turbo engine with chamber bottom stop

Deflector for combustor of gas turbine engine

Turbine engine combustion chamber

Flamesheet diffusion cartridge

Combustor bolted segmented architecture

CTE matching hanger support for CMC structures

Fuel injectors having air sealing structures

Fuel injectors for turbomachines

Igniter seal arrangement for a combustion chamber

Bearing support assembly

Combustor assembly with structural cowl and decoupled chamber

Combustion system with deflector

Fastener assembly having a leak resistant threaded insert

Combustor liner

Nozzle for combustors, combustor, and gas turbine including the same

Gas turbine combustor and transition piece assembly

Combustor panel standoff pin

Combustor having coupling structure for nozzle plate and outer cap, and gas turbine including the same

Methods and features for positioning a flow path assembly within a gas turbine engine

Undercut combustor panel rail

Ducting arrangement with injector assemblies configured to form a shielding flow of air injected into a combustion stage in a gas turbine engine

COMBUSTION CHAMBER ARRANGEMENT

Combustor assembly for a turbine engine

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

Support ring with fluid flow metering

Gas turbine annular combustor arrangement

Gas turbine engine with igniter stack or borescope mount having noncollinear cooling passages

Fuel swirler with anti-rotation features

COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

Heat shield panels with overlap joints for a turbine engine combustor

Combustor and gas turbine including the same

Heat shield assembly of a combustion chamber having a disk spring set

Turbine engine combustion chamber with fixed duct geometry

Aerospace turbofan engines

Combustor and gas turbine including the same

Thermal panel with a corrugated ceramic composite sheet having unequal ridge widths

Cooling configuration for combustor attachment feature

Cooling configurations for combustor attachment features

Cooling configurations for combustor attachment features

COOLING CONFIGURATIONS FOR COMBUSTOR ATTACHMENT FEATURES

Cooling configurations for combustor attachment features

Transition piece support structure, gas turbine combustor including same, and method of installing same

Method to produce jet engine combustor heat shield panels assembly

Method to produce jet engine combustor heat shield panels assembly

Plate for supporting nozzle tubes and method of assembling the same

Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor

Aircraft component and gas turbine engine for aircraft

Integral ceramic matrix composite fastener with polymer rigidization

CMC combustor deflector

Combustor heat shield and attachment features

Gas turbine engine with diffuser having an annular dividing guide body

Combustor assembly with CMC combustor dome

Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustor

Turbine component assembly

Turbine component assembly

Transition structure

CTE matching hanger support for CMC structures

Single cavity trapped vortex combustor with CMC inner and outer liners

CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE

Segmented liner

Turbomachine coupling assembly

Fuel swirler with anti-rotation features

Combustor panel mounting systems and methods

HYBRID COMPONENT COMPRISING A METAL-REINFORCED CERAMIC MATRIX COMPOSITE MATERIAL

COMBUSTOR ATTACHMENT COOLING

COMBUSTION PANEL GROMMET

Combustion liners and attachments for attaching to nozzles

Additively manufactured mechanical fastener with cooling fluid passageways

FILM STARTERS IN COMBUSTORS OF GAS TURBINE ENGINES

Washer for combustor assembly

Combustor heat shield sealing

Combustor liner with gasket for gas turbine engine

Combustion chamber shingle arrangement of a gas turbine

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

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

Methods for assembling a unitary flow path structure

Methods and features for positioning a flow path assembly within a gas turbine engine

Flow path assembly with pin supported nozzle airfoils

Flow path assembly with airfoils inserted through flow path boundary

Combustor liner panel end rail with curved interface passage 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

COATED COMBUSTOR PANEL SHELL FOR A GAS TURBINE ENGINE COMBUSTOR

Combustion systems having bayonet features

Combustion can maintenance apparatus and method

Combustor assembly for a gas turbine engine

Combustor heat shield sealing

Combustion chamber arrangement

Fuel nozzle assembly with flange orifice

Combustion chamber in a turbine engine

Attachment of ceramic matrix composite panel to liner

System and method for impingement cooling of turbine system components

Axial non-linear interface for combustor liner panels in a gas turbine combustor

Combustor assembly with mounted auxiliary component

Gas turbine combustor

Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor

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

Combustion chamber and a combustion chamber fuel injector seal

Tool and method for decoupling cross-fire tube assemblies in gas turbine engines

Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device

Combustor heat shield and attachment features

Combustor heat shield and attachment features

Combustor heat shield and attachment features

Clamping device and an associated method thereof

METHOD FOR TREATING COATED ARTICLE AND TREATED ARTICLE

COMBUSTION CHAMBER WALL OF A GAS TURBINE WITH A FIXTURE OF A COMBUSTION CHAMBER SHINGLE

Burner assembly for a burner of a gas turbine

COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE

Interchangeable liner support for gas turbine combusters

ANNULAR COMBUSTOR FOR A GAS TURBINE ENGINE

Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device

Method of assembling an annular combustion chamber assembly

Structure for supporting nozzle guide of gas turbine engine

Combustion chamber

Flame-holder device

Combustion chamber assembly and a combustion chamber segment

Structure for cooling gas turbine engine

Compact multi-piece spring-loaded crossfire tube

COMBUSTOR ANTI-SURGE RETENTION SYSTEM

Transition Duct Exit Holder and Inlet Ring Support Arrangement

Axisymmetric components and methods for forming axisymmetric components

Combustor cassette liner mounting assembly

Sealing arrangement on combustor to turbine interface in a gas turbine

Transition Duct Support Arrangement for a Gas Turbine Engine

Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine