Gas turbine fuel nozzle end cover using Au—Ni braze and method producing same

METHOD OF MANUFACTURING AN IMPINGEMENT SLEEVE FOR A TURBINE ENGINE COMBUSTOR

TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME

Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same

Method for perforating a wall of a combustion chamber

Method for working of combustor float wall panels

Method of forming a cooling hole by laser drilling

MICROMIXER ASSEMBLY OF A TURBINE SYSTEM AND METHOD OF ASSEMBLY

Combustors with quench inserts

Laser clad fuel injector premix barrel

GAS TURBINE ENGINE COMPONENT WITH CUSPED, LOBED COOLING HOLE

MULTI-LOBED COOLING HOLES IN GAS TURBINE ENGINE COMPONENTS HAVING THERMAL BARRIER COATINGS

Cooling hole with asymmetric diffuser

Process of fabricating a fuel nozzle assembly

Fuel nozzle and process of fabricating a fuel nozzle

Cast manifold for dry low NOx gas turbine engine

Transition piece of combustor, gas turbine having the same, and producing method for transition piece

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

Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same

Combustor heat shield with integrated louver and method of manufacturing the same

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

Coated gas turbine components

Strain tolerant combustor panel for gas turbine engine

CELL STRUCTURE THERMAL BARRIER COATING

Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber

Gas turbine engine combustor with lobed, three dimensional contouring

Combustion chamber for a turbine engine

Process for making a wall with a porous element for component cooling

Ceramic combustor liner panel for a gas turbine engine

Method for manufacturing a ceramic composite article

Hole producing system

Combustor nozzle and method for fabricating the combustor nozzle

APPARATUS FOR VIBRATION SUPPORT IN COMBUSTORS AND METHOD FOR FORMING APPARATUS

Combustion Chamber End Cover Without Welding or Brazing

Stress reduction feature to improve fuel nozzle sheath durability

Ceramic combustor liner panel for a gas turbine engine

SUBSTRATE WITH SHAPED COOLING HOLES AND METHODS OF MANUFACTURE

Turbine Component Having Easily Removable Protective Layer, Set of Turbine Components, a Turbine and a Method for Protecting a Turbine Component

Ultraviolet angled spray nozzle

Gas turbine combustion chamber made of CMC material and subdivided into sectors

METAL INJECTION MOLDING PROCESS AND COMPONENTS FORMED THEREWITH

COMBUSTION LINER STOP BLOCKS HAVING INSERTABLE WEAR FEATURES AND RELATED METHODS

Combustors with quench inserts

Gas turbine combustor liner cap assembly

Height ratios for a transition piece of a combustor

Apparatus and method for a fuel nozzle

Material mixture for producing a fireproof material, fireproof molded body and method for the manufacturing thereof

Turbine Combustor End Cover

Burner arrangement

Burner arrangement

Coating Systems for Protection of Substrates Exposed to Hot and Harsh Environments and Coated Articles

Methods for Coating Articles Exposed to Hot and Harsh Environments

Plates having cooling channels, and method for welding the plates and increasing a dimension of the cooling channels adjacent the welded section

Pilot burner of a gas turbine engine, combustor, and gas turbine engine

Coating process and corrosion protection coating for turbine components

Fuel nozzle assembly that exhibits a frequency different from a natural operating frequency of a gas turbine engine and method of assembling the same

Monolithic fuel injector and related manufacturing method

METHOD OF DEPOSITING PROTECTIVE COATINGS ON TURBINE COMBUSTION COMPONENTS

Fuel nozzle assembly for a gas turbine engine

Process for producing combustor structural member, and combustor structural member, combustor for gas turbine and gas turbine

Reverse flow ceramic matrix composite combustor

Fuel nozzle liquid cartridge including a fuel insert

METHOD FOR THE PROVISION OF A COOLING-AIR OPENING IN A WALL OF A GAS-TURBINE COMBUSTION CHAMBER AS WELL AS A COMBUSTION-CHAMBER WALL PRODUCED IN ACCORDANCE WITH THIS METHOD

Drilled and integrated secondary fuel nozzle and manufacturing method

GAS TURBINE COMBUSTOR

Method for coating a component

Method of manufacturing a unitary conduit for transporting fluids

Multi passage fuel manifold and methods of construction

Thermal machine

COMPONENT WITH DIAGONALLY EXTENDING RECESSES IN THE SURFACE AND PROCESS FOR OPERATING A TURBINE

Method of manufacturing a thermal insulation article

Elimination of plate fins in combustion baskets by CMC insulation installed by shrink fit

Composite material part with a silicon-containing ceramic matrix protected against corrosion

REPAIRABLE FUEL NOZZLE

METHOD OF MANUFACTURING A FUEL DISTRIBUTOR

Unitary conduit for transporting fluids

Swirlers

Fuel nozzle

METHOD OF MANUFACTURING A UNITARY VENTURI

VENTURI

Mixer for a combustor

Fuel distributor

METHOD OF ASSEMBLING A FUEL NOZZLE

METHOD OF MANUFACTURING A UNITARY SWIRLER

METHOD OF MANUFACTURING MIXERS

METHOD OF REPAIRING A FUEL NOZZLE

REPAIR OF FUEL NOZZLE COMPONENT

METHOD OF FORMING COOLING HOLES AND TURBINE AIRFOIL WITH HYBRID-FORMED COOLING HOLES

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

Method for the production of a sealing segment, and sealing segment to be use in compressor and turbine components

Method of producing effusion holes

Combustor heat shield with integrated louver and method of manufacturing the same

Fuel injector nozzle with macrolaminate fuel swirler

Stress reduction feature to improve fuel nozzle sheath durability

Combustion chamber air inlet

Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith

Modular fuel nozzle and method of making

Welded gas turbine engine parts with different thicknesses and method

Modular fuel nozzle and method of making

Annular combustion chamber with a removable end wall

Method of manufacturing a metal injection moulded combustor swirler

Drilled and integrated secondary fuel nozzle and manufacturing method

Combustion liner for gas turbine formed of cast nickel-based superalloy

Reduced thermal stress fuel nozzle assembly

Method for casting cooling holes

Film cooling for microcircuits

Modular fuel nozzle and method of making

Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers

Component, method for coating a component, and powder

Electroplated fuel nozzle/swirler wear coat

Gas turbine combustor heat shield panel or exhaust panel including a cooling device

Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same

Single crystal combustor panels having controlled crystallographic orientation

Macrolaminate radial injector

Combustion liner having cooling holes with stepped lateral sidewalls

Ceramic matrix composite component with corrugated wall

CMC component with cover plate

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

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

Combustor body and axial fuel stage immersed injectors additively manufactured with different materials