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

Flowpath Assembly with Composite Tube Array

COMBUSTION LINER FOR GAS TURBINE ENGINE

Additively Manufactured Combustion Chambers, Manifold Structures and Hybrid Additive Processes Related Thereto

COOLING NOZZLE VANES OF A TURBINE ENGINE

Micro Gas Turbine Engine and Related Methods of Manufacture

WALL MEMBER AND MANUFACTURING METHOD THEREOF

ARTICLE AND METHOD FOR MANUFACTURING AN EXPANDED COMBUSTOR LINER

ASSEMBLY, METHOD FOR MANUFACTURING ASSEMBLY, BURNER, AND METHOD FOR MANUFACTURING BURNER

ADDITIVE CLOCKED FUEL INJECTOR BOLT

COMBUSTOR ASSEMBLY FOR A TURBO MACHINE

THERMALLY STABLE THIN-FILM REFLECTIVE COATING AND COATING PROCESS

A FUEL NOZZLE FOR A GAS TURBINE, COMBUSTOR INCLUDING THE FUEL NOZZLE, AND GAS TURBINE

TILE FOR A GAS TURBINE ENGINE COMBUSTOR

SCALEABLE ACOUSTICALLY-STABLE COMBUSTION CHAMBER AND DESIGN METHODS

COMBUSTOR FOR A GAS TURBINE ENGINE

Additively Manufactured Combustion Chambers, Manifold Structures and Hybrid Additive Processes Related Thereto

Material deposition for fuel nozzle joint

CTE MATCHING HANGER SUPPORT FOR CMC STRUCTURES

FUEL SPRAY NOZZLE FOR GAS TURBINE ENGINE AND METHOD FOR MANUFACTURING THE SAME

Pilot arrangement, nozzle device, method and gas turbine arrangement

METHOD FOR ADDITIVE MANUFACTURING OF A WALL FOR A TURBINE ENGINE, COMPRISING AT LEAST ONE COOLING APERTURE

COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

Impingement cooling apparatus support structure and method of manufacture

Method of optimising gas turbine engine combustion equipment performance

Sectional fuel manifolds

Thermally stable thin-film reflective coating and coating process

Production by additive manufacturing of complex parts

Combustor

Integral flow rate limiter and fuel injector for a gas turbine combustor

Material deposition for fluid nozzle joints

Combustor panels for gas turbine engines

Sintered body, method of manufacturing sintered body, combustor panel, and method of manufacturing combustor panel

RESONATOR RING FOR COMBUSTION CHAMBER SYSTEMS

HEAT TRANSFER DEVICE, TURBOMACHINE CASING AND RELATED STORAGE MEDIUM

Combustor for a gas turbine engine

Methods and apparatus for securing an autoclave bag to a composite fixture

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

ARTICLE WITH COOLING HOLES AND METHOD OF FORMING THE SAME

Combustor for gas turbine engine and method of manufacture

FLOWPATH ASSEMBLY WITH COMPOSITE TUBE ARRAY

Torch igniter cooling system

Torch igniter cooling system

Spall plate for consumable combustor support structures

Adhesion of a substrate onto a CMC component

Aerodynamic component for a gas turbine engine

Sectional fuel manifolds

Environmental barrier coating

Article and method for manufacturing an expanded combustor liner

METHOD OF MANUFACTURING FIBER REINFORCED BARRIER COATING

Fixture assembly for coating combustor panels

Monolithic combustor for attritiable engine applications

Panel burn through tolerant shell design

Heat transfer arrangements and methods of making heat transfer arrangements

Gas turbine combustor and method of manufacturing burner component

Combustor component, combustor, gas turbine, and manufacturing method for combustor component

Heat shield panel manufacturing process

Bonding system for dual walled turbine components

Feature based cooling using in wall contoured cooling passage

Integrated fuel swirlers

Fuel injector systems and support structures

COMBUSTOR TO VANE SEALING ASSEMBLY AND METHOD OF FORMING SAME

Article with cooling holes and method of forming the same

SINTERED-BONDED HIGH TEMPERATURE COATINGS FOR CERAMIC TURBOMACHINE COMPONENTS

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

INSPECTION PORT FOR AN ATTRITABLE ENGINE SUPPORT STRUCTURE

Guiding device in a combustion chamber

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

Support structure for a turbine vane of a gas turbine engine

Spall plate for consumable combustor support structures

Scaleable acoustically-stable combustion chamber and design methods

INJECTOR DEVICE AND METHOD FOR MANUFACTURING AN INJECTOR DEVICE

Combustor assembly for a turbine engine

Object with tear-shaped suspension for annular bodies

Sectional fuel manifolds

Combustor panels for gas turbine engines

Backside features with intermitted pin fins

System and method for high frequency accoustic dampers with caps

Sintered-bonded high temperature coatings for ceramic turbomachine components

Systems and methods for manufacturing film cooling hole diffuser portion

Monolithic combustor for attritiable engine applications

Combustor wall assembly for gas turbine engine

AERODYNAMIC COMPONENT FOR A GAS TURBINE ENGINE

Method for injecting a loaded slurry into a fibrous texture

Backside features with intermitted pin fins

BONDED COMBUSTOR WALL FOR A TURBINE ENGINE

Stand-off device for double-skin combustor liner

Diffusing hole for rail effusion

Gas turbine engine with integral combustion liner and turbine nozzle

Systems and methods for optimal source material deposition along hole edges

Thermally coupled CMC combustor liner

Combustor dome via additive layer manufacturing

Gas turbine engine dual-wall hot section structure

Consumable support structures for additively manufactured combustor components

CMC combustor shell with integral chutes

Production of a combustion chamber made of composite material

Additive integral combustor expansion spring

ADDITIVE MANUFACTURING METHOD FOR THE ADDITION OF FEATURES WITHIN COOLING HOLES

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

Combustor assembly for a turbo machine

Tapered panel rail

Systems and methods for combustor panel

Unitary flow path structure

Method of manufacturing conductive film holes

Airfoil fluid curtain to mitigate or prevent flow path leakage

Flow path assembly with airfoils inserted through flow path boundary

Reduced stress boss geometry for a gas turbine engine

Heat shield panel manufacturing process

Combustor heat shield sealing

Pre-swirl pressure atomizing tip

And manufacturing process for directed impingement punched plates

Method of controllably coating a fiber preform during ceramic matrix composite (CMC) fabrication

Combustor bolted segmented architecture

CTE matching hanger support for CMC structures

Turbine engine part coated in a thermal barrier, and a method of obtaining it

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

Undercut combustor panel rail

Pull-plane effusion combustor panel

Panel burn through tolerant shell design

Fuel injector systems and support structures

Vibration-damping components, gas turbine engine and method of forming such components

Plate swirler with converging swirl passages

Additively manufactured wall and floating ferrule having a frangible member between the floating ferrule and a build support arm

Method to produce jet engine combustor heat shield panels assembly

Method to produce jet engine combustor heat shield panels assembly

Liquid bond coatings for barrier coatings

Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics

Gas turbine combustion liner comprising heat transfer cell heat pipes

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

Fixture assembly for coating combustor panels

Method of forming a hole in a coated component

Arcuate directionally solidified components and manufacture methods

Dilution holes for gas turbine engines

Combustor panel standoffs with cooling holes

Sintered body, method of manufacturing sintered body, combustor panel, and method of manufacturing combustor panel

Slotted ceramic coatings for improved CMAS resistance and methods of forming the same

Coated ceramic matrix composition component and a method for forming a coated ceramic matrix composition component

Engine component with cooling passages

Systems and methods for manufacturing film cooling hole diffuser portion

CTE matching hanger support for CMC structures

Sintered-bonded high temperature coatings for ceramic turbomachine components

Method for real-time simultaneous and calibrated additive and subtractive manufacturing

Gas turbine engine components with air-cooling features, and related methods of manufacturing the same

Adhesion of a substrate onto a CMC component

Method of manufacturing conductive film holes

Panel surface pockets for coating retention

Impingement cooled components having integral thermal transfer features

Ceramic matrix composite components reinforced for managing multi-axial stresses and methods for fabricating the same

Turbomachine component with radially inward projecting strut cooling features

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

Method for manufacturing a burner assembly for a gas turbine combustor and burner assembly for a gas turbine combustor

Apparatus with thermal break

Unitary flow path structure

Unitary flow path structure

Unitary flow path structure

Fuel injectors and methods of fabricating same

Gas turbine fuel injectors and processes

Combustor heat shield sealing

HOLLOW-WALL HEAT SHIELD FOR FUEL INJECTOR COMPONENT

Portable jig and fixture for precision machining

Fuel manifold with integrally formed retainer for a pilot nozzle in a combustor of a gas turbine engine

Feature based cooling using in wall contoured cooling passage

Plate-shaped structural component of a gas turbine

Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers

Nested article by additive manufacturing with non-removable internal supporting structure

Cast combustor liner panel radius for gas turbine engine combustor

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

Scalable acoustically-stable combustion chamber and design methods

COMBUSTOR WALL ELEMENT AND METHOD FOR MANUFACTURING THE SAME

Component assembly for a gas turbine engine

Combustor heat shield and attachment features

Cast gas turbine engine cooling components

COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE

Systems and methods for combustor panel

Method and computer-readable model for additively manufacturing ducting arrangement with injector assemblies forming a shielding flow of air

Combustor cooling panel, transition piece and combustor including the same, and gas turbine including combustor

Structure for supporting nozzle guide of gas turbine engine

Auxetic Structures With Distorted Projection Slots In Engineered Patterns To Provide NPR Behavior And Improved Stress Performance

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

Combustor Effusion Plate Assembly

Method of manufacturing an insulated flowpath assembly

Ceramic and ceramic matrix composite attachment methods and systems

Combustor thermal shield fabrication method

Porous rotating machine component, combustor and manufacturing method

Fuel injector

METHOD AND COMPUTER-READABLE MODEL FOR ADDITIVELY MANUFACTURING DUCTING ARRANGEMENT FOR A COMBUSTION SYSTEM IN A GAS TURBINE ENGINE

Combustor panels having recessed rail

Sleeve assemblies and methods of fabricating same

System having layered structure and method of making the same

Combustor assembly for a gas turbine engine

Surface contouring of a flowpath wall of a gas turbine engine

Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine

Assembly for turbomachine combustion chamber comprising a boss and an annular element

CMC articles having small complex features for advanced film cooling

Combustor panels having angled rail

Combustion liner for use in a combustor assembly and method of manufacturing

Article having multi-layered coating

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

Additive layer manufacturing for fuel injectors

Combustor tile with monolithic inserts

Ceramic matrix composite component and process of producing a ceramic matrix composite component

Annular turbomachine combustion chamber

CMC COMBUSTOR SHELL WITH INTEGRAL CHUTES

Trapped vortex fuel injector and method for manufacture

Gas turbine engine combustor and method of forming same

Annular combustion chamber in a turbine engine

Gas turbine engine wall assembly interface

Full nozzle for gas turbine combustor

Reduced stress boss geometry for a gas turbine engine

Machinable CMC insert

Machinable CMC insert

Heat recovery system

Ceramic and metal engine components with gradient transition from metal to ceramic

Combustor panels and configurations for a gas turbine engine

Fuel injector device

Combustor wall cooling channel formed by additive manufacturing

Method of manufacturing fiber reinforced barrier coating

Line replaceable fuel nozzle apparatus, system and method

Passage geometry for gas turbine engine combustor

Combustor panel having material transition region

Bonded combustor wall for a turbine engine

Swirler for a turbine engine combustor

Cold spray manufacturing of MAXMET composites

Turbulator structure on combustor liner

Thermal barrier coating of a combustor dilution hole

Sequential burner for an axial gas turbine

Airblast nozzle with upstream fuel distribution and near-exit swirl

Cooled component

Fuel reformer chamber with tubular mesh insert supporting a catalyst

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 front panel

Method of manufacturing gas turbine engine component from a molybdenum-rich alloy

Film cooling circuit for a combustor liner

Single-walled combustor for a gas turbine engine and method of manufacture

Cylinder of combustor, method of manufacturing of cylinder of combustor, and pressure vessel

Joint for sealing a gap between casing segments of an industrial gas turbine engine combustor

Laser clad fuel injector premix barrel

Arcuate directionally solidified components and manufacture methods

Method and an apparatus for producing cooling apertures in a combustion chamber head

Method of shaping green part and manufacturing method using same

Additive manufactured surface finish

Additive manufacturing method for the addition of features within cooling holes

PROCESS OF ASSEMBLING FUEL NOZZLE END COVER

Insulated flowpath assembly

Hollow-wall heat shield for fuel injector component

Gas turbine transition piece aft frame assemblies with cooling channels and methods for manufacturing the same

Additive manufacture from machined surface

Combustor assembly for a gas turbine engine having a braze layer having a centerline eutectic free region

Trapped vortex fuel injector and method for manufacture

Grommet assembly and method of design

Gas turbine combustion chamber and method for manufacturing the same

Combustion chamber wall and a method of manufacturing a combustion chamber wall

System having layered structure and method of making the same

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

BRAZELESS END COVER FOR A COMBUSTION SYSTEM

Gas turbine combustor and gas turbine

Method for manufacturing a metallic or ceramic component by selective laser melting additive manufacturing

Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine

Microcircuit cooling for gas turbine engine combustor

Thermally free liner retention mechanism

Combustion chamber

Process for making a turbulator by additive manufacturing

Wake reducing structure for a turbine system

Ceramic matrix composite component and method of forming thereof

Combustor dome heat shield

GAS-TURBINE COMBUSTION CHAMBER AND METHOD FOR ITS MANUFACTURE

Gas turbine combustor

Gas turbine engines having fuel injector shrouds with interior ribs

Method of manufacturing an article by hot pressing and ultrasonically inspecting the article

Method for applying heat resistant protection components onto a surface of a heat exposed component

Micro-mixer fuel plenum and methods for fuel tube installation

Component for attaching to a wall

COMBUSTOR OF A GAS TURBINE WITH PRESSURE DROP OPTIMIZED LINER COOLING

Gas turbine combustion chamber tile having effusion cooling holes including straight and offset sections

Gas turbine engine with improved combustion liner

Combustors with complex shaped effusion holes

Gas turbine engine combustor with integrated combustor vane having swirler

Wake reducing structure for a turbine system and method of reducing wake

Reverse flow ceramic matrix composite combustor

Process for producing a layer system

Auxetic structure with stress-relief features

Combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly

Vaned structure and a method of manufacturing a vaned structure

Method of forming a microchannel cooled component

Pressure casting slip and refractory ceramic produced therefrom for gas turbine units

COMBUSTOR COMPONENT WITH COOLING HOLES FORMED BY ADDITIVE MANUFACTURING

Method of manufacturing a wall

Micromixer assembly for a turbine system and method of distributing an air-fuel mixture to a combustor chamber

Fuel plenum annulus

Gas turbine combustor including burner having plural gaseous fuel manifolds

Gas turbine engine combustor with integrated combustor vane

Methods of resizing holes

Gas turbine engine cooling hole with circular exit geometry

Method of casting parts using heat reservoir, gating used by such method, and casting made thereby

COMBUSTOR INCLUDING COMBUSTION NOZZLE AND AN ASSOCIATED METHOD THEREOF