AXIAL STAGED COMBUSTION SYSTEM FOR SUPPRESSING GENERATION OF NITROGEN OXIDES FROM AMMONIA OR HYDROGEN FLAME

TURBINE ENGINE COMBUSTOR WITH A FIRST FUEL INJECTOR AND A SECOND FUEL INJECTOR

COMBUSTION SECTION WITH A PRIMARY COMBUSTION CHAMBER AND A SECONDARY COMBUSTION CHAMBER

GAS TURBINE EMISSIONS

CO-FIRING COMBUSTOR WITH GAS FUEL AND LIQUID AMMONIA

FUEL INJECTION ASSEMBLY HAVING A BOSS WITH A SERPENTINE COOLING PASSAGE

GAS TURBINE ENGINE INCLUDING FUEL INJECTOR

GAS TURBINE ENGINE AND FUEL NOZZLE ASSEMBLY THEREFOR

FUEL SUPPLY SYSTEM FOR A COMBUSTOR

FUEL SPRAY NOZZLES

GAS TURBINE EMISSIONS

SUPER COMPACT COMBUSTOR

AXIAL FUEL STAGE INJECTOR WITH AXIALLY ELONGATED MIXING CHAMBERS WITH AXIALLY WAVY INLETS

AXIAL FUEL STAGE INJECTOR WITH AXIALLY ELONGATED MIXING CHAMBERS, AND COMBUSTOR AND GT SYSTEM INCLUDING SAME

DUAL FUEL COMBUSTOR FOR A TURBINE ENGINE

NONPREMIXED, RICH, RELAX, LEAN COMBUSTOR

AIRCRAFT COMPRISING A GAS TURBINE ENGINE HAVING PRIMARY AND SECONDARY FUEL-INJECTORS

MULTI-FUEL COMBUSTION SYSTEM

COOLING IN STAGED FUEL SYSTEMS

GAS TURBINE ENGINE HAVING A COMBUSTION SECTION WITH STEAM PROVIDED TO SECOND COMBSUTOR PLENUM

TURBINE ENGINE HAVING A COMBUSTION SECTION WITH A FUEL SUPPLY ASSEMBLY

APPARATUS FOR FUEL-AIR MIXING AND FLAME-HOLDING IN PULSE COMBUSTORS

SEQUENTIAL COMBUSTION GAS TURBINE ENGINE INCLUDING A STEAM SYSTEM FOR INJECTING STEAM TO EACH COMBUSTOR

INJECTOR WITH INJECTOR ELEMENTS IN CIRCUMFERENTIAL ROWS THAT ALTERNATE BETWEEN COUNTER-CLOCKWISE AND CLOCKWISE SWIRL

Controllable fuel nozzle valves with redundancy

STAGED BLADE INJECTOR

FUEL INJECTION ASSEMBLY HAVING A BOSS WITH A SERPENTINE COOLING PASSAGE

COMBUSTION SYSTEM

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

GAS TURBINE OPERATING CONDITIONS

COMBUSTOR APPARATUS

TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAME

COMBUSTOR IN GAS TURBINE ENGINE

Central staged combustion chamber with self-excited sweeping oscillating fuel injection nozzles

Fuel system and method for supplying a combustion chamber in an aircraft turboshaft engine with fuel

FUEL INJECTOR

Gas turbine combustor fuel nozzle assembly and combustor liner having dilution holes in arrangements

VARIABLE COOLING OF SECONDARY CIRCUIT OF FUEL NOZZLES

Combustor with fuel and air mixing plenum

THERMAL COMPRESSION REHEATING CYCLE

Gas turbine combustor with dynamics mitigation system

METHOD OF OPERATING GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGES

GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGES AND METHOD OF OPERATION

MULTI-STAGE AXIAL FUEL INJECTION SYSTEM WITH DISCRETE AIR SUPPLIES

COMBUSTOR RE-LIGHT PROCEDURE

LEAN BURN COMBUSTION SYSTEM

GAS TURBINE OPERATING CONDITIONS

Gas turbine combustor injector assembly comprising an air supply unit having an inclined surface relative to an inclined injection pipe

INJECTION TECHNIQUES FOR GAS TURBINE SYSTEMS

Method of operating a gas turbine combustor comprising injecting a diluent into the primary and secondary combustion zones

REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE

BURNER WITH A BILAMINAR COUNTERDIRECTIONAL VORTEX FLOW

MULTIPHASE FUEL INJECTOR

Proportional force modification of passive spool for control of secondary nozzle circuits

Variable restriction of a fuel circuit of a fuel nozzle

Variable restriction of a secondary circuit of a fuel injector

Variable restriction of fuel nozzle with an auxiliary circuit

COMBUSTOR SYSTEMS AND METHODS

COMBUSTOR FOR A GAS TURBINE ENGINE

Redundant electro-hydraulic servo valve (EHSV) control in a fuel metering system

Combustor with secondary fuel nozzle in dilution fence

Combustor with a variable volume primary zone combustion chamber

Method of optimising gas turbine engine combustion equipment performance

Combustor and gas turbine equipped with the same

Ammonia fired combustor operating method

FUEL SUPPLY SYSTEM FOR A COMBUSTOR

Micro-mixer with multi-stage fuel supply and gas turbine including same

Multi-nozzle fuel injection method for gas turbine

Combustor fuel nozzle assembly

Gas turbine engine injector module with thermally coupled fuel lines having respective outlets

Methods of operating a turbomachine combustor on hydrogen

Multitube pilot injector having a split airflow for a gas turbine engine

Staged combustion

SYSTEMS AND METHODS FOR ADDITION OF FUEL ADDITIVES TO CONTROL TURBINE CORROSION

Controlling soot

Gas turbine combustor having secondary fuel nozzles with plural passages for injecting a diluent and a fuel

Combustor having fuel sweeping structures

Combustor for a gas turbine engine

Systems and methods for addition of fuel additives to control turbine corrosion

Systems and methods for addition of fuel additives to control turbine corrosion

Systems and methods for addition of fuel additives to control turbine corrosion

Second stage combustion for igniter

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

PURGING SYSTEM FOR TURBINE FRACTURING APPARATUS GROUP, PURGING METHOD AND TURBINE FRACTURING APPARATUS GROUP

SYSTEM AND METHOD FOR LOAD CONTROL WITH DIFFUSION COMBUSTION IN A STOICHIOMETRIC EXHAUST GAS RECIRCULATION GAS TURBINE SYSTEM

Gas turbine load/unload path control

Combustor nozzle, combustor, and gas turbine including same

Fuel nozzle structure for air assist injection

Dual schedule flow divider valve, system, and method for use therein

Fuel nozzle and associated method of assembly

Dual schedule flow divider valve, system, and method for use therein

COMBUSTION SYSTEM AND METHOD FOR ATTENUATION OF COMBUSTION DYNAMICS IN A GAS TURBINE ENGINE

Fuel distribution manifold

Combustor for gas turbine and gas turbine having the same

Combustor air flow path

Systems and methods for determination of gas turbine fuel split for head end temperature control

Injector with injector elements in circumferential rows that alternate between counter-clockwise and clockwise swirl

Two-stage combustor for gas turbine engine

Low emissions combustor assembly for gas turbine engine

Gas turbine combustor having main fuel valves independently adjustable

Cooling in staged fuel system

Trapped vortex combustor and method for operating the same

Gas turbine engine and methods of controlling emissions therefrom

Volute trapped vortex combustor assembly

Water injection

Staged combustion

Fuel supply system

Fluid mixing apparatus using liquid fuel and high- and low-pressure fluid streams

Combustor with dual pressure premixing nozzles

System and methods for igniting and operating a gas turbine engine with alternative fuels

Mixer

METHOD AND SYSTEM FOR ROTATING DETONATION COMBUSTION

Axially staged rich quench lean combustion system

Casing integrated fluid distribution system

Assembly of a servo pump and a hydraulic motor

Combustor having inner and outer tubular oxygen nozzles about a tubular fuel supply unit

Combustor floating collar mounting arrangement

Method for operating a burner arrangement of a gas turbine

Combustor with axial fuel staging system and gas turbine having the same

Second stage combustion for igniter

Method of selective combustor control for reduced emissions

FUEL INJECTOR FOR A TURBINE ENGINE

Gas turbine load/unload path control

Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine

Enhancement for fuel spray breakup

Fuel spray nozzle for gas turbine engine

Multipoint fuel injection for radial in-flow swirl premix gas fuel injectors

Combustion section and fuel injector assembly for a heat engine

Combustor and gas turbine

Device to correct flow non-uniformity within a combustion system

Combustor with axially staged fuel injection

Prefilming fuel/air mixer

Gas turbine engine with a unitary structure and method for manufacturing the same

Binary fuel staging scheme for improved turndown emissions in lean premixed gas turbine combustion

Thrust chamber device and method for operating a thrust chamber device

Gas turbine combustor and operating method thereof

Fuel nozzle structure for air assist injection

Fuel oil axial stage combustion for improved turbine combustor performance

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

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

Jet swirl air blast fuel injector for gas turbine engine

Axial fuel staging system for gas turbine combustors

Fuel injection assemblies for axial fuel staging in gas turbine combustors

Thimble assemblies for introducing a cross-flow into a secondary combustion zone

Combustor and gas turbine including the same

Involute trapped vortex combustor assembly

Volute trapped vortex combustor assembly

Method of operating a combustion system with main and pilot fuel circuits

Transfer tube assembly of nested tubes and a connecting segment having parallel and offset bores

Fuel manifold with nested annular passages and radially extending channels

Axially staged rich quench lean combustion system

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

Combustion system and method for attenuation of combustion dynamics in a gas turbine engine

Low emissions combustor assembly for gas turbine engine

DETERMINATION OF A FUEL DELIVERY FAULT IN A GAS TURBINE ENGINE

Jet in cross flow fuel nozzle for a gas turbine engine

Combined power generation system comprising a fuel cell and a gas turbine engine

Nozzle assembly for a combustion chamber of an engine

Systems and methods for a multi-fuel premixing nozzle with integral liquid injectors/evaporators

Combustion staging system

Combustion staging system

Combustion staging system

Combustion staging system

Gas turbine combustor with heat exchanger between rich combustion zone and secondary combustion zone

System and method for combusting liquid fuel in a gas turbine combustor with staged combustion

Low Profile Axially Staged Fuel Injector

Dual fuel injectors and methods of use in gas turbine combustor

Fuel injectors with multiple outlet slots for use in gas turbine combustor

Device to correct flow non-uniformity within a combustion system

COMBUSTION SYSTEM WITH INJECTOR ASSEMBLY INCLUDING AERODYNAMICALLY-SHAPED BODY AND/OR EJECTION ORIFICES

Fuel flow rate setting method, device for implementing said method, and gas turbine plant provided with said device

ULTRA-LOW NOX EMISSION GAS TURBINE ENGINE IN MECHANICAL DRIVE APPLICATIONS

Cooling in staged fuel systems

Rotating detonation engine multi-stage mixer

MIXER

Combustion System with Axially Staged Fuel Injection

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

Fuel injectors and methods of fabricating same

Combustor with axially staged fuel injector assembly

Flow ratio calculation device, control device provided with same, gas turbine plant provided with said control device, flow ratio calculation method, and method for controlling fuel system

Gas turbine fuel injectors and processes

Combustor

Fuel injectors and methods of use in gas turbine combustor

Fuel injectors and methods of use in gas turbine combustor

System for dissipating fuel egress in fuel supply conduit assemblies

GAS TURBINE TRANSITION DUCT WITH LATE LEAN INJECTION HAVING REDUCED COMBUSTION RESIDENCE TIME

Staged dual fuel radial nozzle with radial liquid fuel distributor

Dual fuel radial flow nozzles

Staged radial air swirler with radial liquid fuel distributor

FUEL SUPPLY SYSTEM

FUEL SUPPLY SYSTEM

Start biased liquid fuel manifold for a gas turbine engine

FUEL SUPPLY SYSTEM

Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine

Combustor with axially staged fuel injection

Vortex generating device

Emissions modeling for gas turbine engines for selecting an actual fuel split

Vortex generating device

Mini mixing fuel nozzle assembly with mixing sleeve

Combustor assembly with mounted auxiliary component

APPARATUS AND METHODS OF OPERATING A COMBUSTION ENGINE

Circumferential fuel shifting and biasing in an axial staged combustor for a gas turbine engine

Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine

Pilot injector fuel shifting in an axial staged combustor for a gas turbine engine

Clamping device and an associated method thereof

Sequential combustion with dilution gas mixer

Burner assembly for a burner of a gas turbine

MULTI-TUBE LATE LEAN INJECTOR

Fuel injector with heat pipe cooling

Burner, combustor, and gas turbine

Reducing noise from a combustor of a gas turbine engine

Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine

Fuel delivery system for a gas turbine engine

Combustor with staged, axially offset combustion

Combustors and methods of assembling the same

Burner, combustor, and gas turbine

Integrated combustor nozzle for a segmented annular combustion system

Segmented annular combustion system

Panel fuel injector

Combustion staging system

Combustion staging system

GAS TURBINE WITH SEQUENTIAL COMBUSTION ARRANGEMENT

Segmented annular combustion system

Combustor and method for damping vibrational modes under high-frequency combustion dynamics

METHOD FOR COMBUSTING A FUEL, AND COMBUSTION APPLIANCE

Method for combusting a fuel, and combustion device

Fuel injector

Segmented annular combustion system with axial fuel staging

Transition duct assembly with late injection features

Segmented annular combustion system with dual fuel capability

Combustion system with panel fuel injector

Segmented annular combustion system

Mounting of integrated combustor nozzles in a segmented annular combustion system

Turbine nozzle cooling with panel fuel injector

Radially stacked fuel injection module for a segmented annular combustion system

Operation and turndown of a segmented annular combustion system

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

Cooling of integrated combustor nozzle of segmented annular combustion system

Transition duct assembly with late injection features

AXIALLY STAGED FUEL INJECTOR ASSEMBLY

STAGED FUEL AND AIR INJECTORS IN COMBUSTION SYSTEMS OF GAS TURBINES

Staged fuel and air injectors in combustion systems of gas turbines

AXIALLY STAGED FUEL INJECTOR ASSEMBLY MOUNTING

Combustion chamber system and a method of operating a combustion chamber system

Combustion staging system

Combustion liner cooling

Fuel supply conduit assemblies

SPACERS AND CONDUIT ASSEMBLIES HAVING THE SAME

Methods and systems for controlling the products of combustion

Burner for a can combustor

FUEL INJECTORS AND METHODS OF FABRICATING SAME

Cooling system for fuel nozzles within combustor in a turbine engine

FUEL INJECTION SYSTEM FOR A TURBINE ENGINE

STAGED FUEL AND AIR INJECTION IN COMBUSTION SYSTEMS OF GAS TURBINES

Burner for a can combustor

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

FUEL INJECTORS AND STAGED FUEL INJECTION SYSTEMS IN 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

Staged fuel and air injection in combustion systems of gas turbines

Prefilming fuel/air mixer

GAS TURBINE WITH A SEQUENTIAL COMBUSTION ARRAGEMENT AND FUEL COMPOSITION CONTROL

SYSTEM AND METHOD FOR MAINTAINING EMISSIONS COMPLIANCE WHILE OPERATING A GAS TURBINE AT TURNDOWN CONDITION

Trapped vortex fuel injector and method for manufacture

Fuel staging

Combustor replacement method and gas turbine plant

First stage turbine vane arrangement

Combustion chamber comprising additional injection devices opening up directly into corner recirculation zones, turbomachine comprising such a chamber and fuel supply method for such a chamber

Trapped vortex cavity staging in a combustor

Sequential combustor and method for operating the same

GAS TURBINE CONTROL SYSTEM

Fuel nozzle structure for air assist injection

Gas turbine fuel components

Fuel injection locations based on combustor flow path

Cooling in staged fuel systems

IR-radar image generator to provide a decoy and associated method of operation

TWO-STAGE COMBUSTOR FOR GAS TURBINE ENGINE

Axial staged combustor with restricted main fuel injector

Fuel nozzle with dual-staged main circuit

Circumferentially and axially staged can combustor for gas turbine engine

Fuel nozzles

INJECTION BOSS FOR A UNIBODY COMBUSTOR

Fuel nozzle for axially staged fuel injection

Combustion staging system

AIR SHIELD FOR A FUEL INJECTOR OF A COMBUSTOR

AIR SHIELD FOR A FUEL INJECTOR OF A COMBUSTOR

Fuel staging in a gas turbine engine

Circumferentially and axially staged annular combustor for gas turbine engine

Combustion staging system

Angled radial fuel/air delivery system for combustor

Fuel supply system for a gas turbine combustor

METHOD OF CONTROLLING THE FUEL DISTRIBUTION AMONG DIFFERENT STAGES OF A GAS TURBINE COMBUSTION CHAMBER

Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation

Sequential combustor arrangement with a mixer

Axially staged mixer with dilution air injection

Separate feedings of cooling and dilution air

Fuel nozzle structure

Sequential burner for an axial gas turbine