GAS TURBINE ENGINE

AIRCRAFT EMISSIONS

GAS TURBINE ENGINE INCLUDING FUEL INJECTOR

FUEL SPRAY NOZZLES

GAS TURBINE ENGINE

GAS TURBINE PERFORMANCE

GAS TURBINE ENGINEAND METHOD THEREOF FOR REDUCING NONVOLATILE PARTICULATE MATTER EMISSIONS

GAS TURBINE ENGINE AND METHOD FOR REDUCING NONVOLATILE PARTICULATE MATTER EMISSIONS IN THE EXHAUST

GAS TURBINE PERFORMANCE

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

COMBUSTOR HAVING SECONDARY FUEL INJECTOR

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

POSITIONAL CONTROL OF FUEL INJECTION INTO GAS TURBINE COMBUSTORS

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

CONTROL METHOD FOR GAS TURBINE COMBUSTOR AND CONTROL DEVICE FOR GAS TURBINE COMBUSTOR

FLEX FUEL COMBUSTOR

COMBUSTION SYSTEM

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

Turbine Engine Including a Combustor

TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAME

COMBUSTOR IN GAS TURBINE ENGINE

COMBUSTOR WITH LEAN OPENINGS

ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM

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

Combustor with fuel and air mixing plenum

FUEL SYSTEM WITH PILOT AND MAIN INJECTORS FOR HYDROGEN-DRIVEN GAS TURBINE ENGINE

METHOD OF OPERATING GAS TURBINE COMBUSTOR WITH MULTIPLE FUEL STAGES

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

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

FUEL NOZZLE

Method of controlling a combustor

Apparatuses, systems, and methods for optimizing acoustic wave confinement to increase combustion efficiency

Device for distributing fuel flows for a fuel supply circuit of a turbomachine combustion chamber

Method of optimising gas turbine engine combustion equipment performance

Combustor and gas turbine equipped with the same

Gas combustion engine with combustion gas recuperation

METHOD FOR OPERATING A GAS ENGINE WITH FUEL SUPPLY DEVICE WITH SELECTION OPTION FOR DIRECT INJECTION AND/OR AIR PATH INJECTION OF FUEL

Combustor nozzle, combustor, and gas turbine including same

Liquid hydrogen-liquid oxygen fueled powerplant

Turbine engine with fuel system including a catalytic reformer

Combustor fuel nozzle assembly

Combustor with lean openings

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Methods of operating a turbomachine combustor on hydrogen

Multi-function monolithic combustion liner

Engine with rotating detonation combustion system

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

Fuel systems

Fuel nozzle

Engine with rotating detonation combustion system

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

Gas turbine load/unload path control

Multi-tube combustor and gas turbine including same

Micro-mixer and combustor having the same

Fuel nozzle structure for air assist injection

Fuel injector for a turbomachine

Combustor premixer assembly including inlet lips

Fuel distribution manifold

Systems and methods for extended emissions compliant operation of a gas turbine engine

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

Combustor and gas turbine including the same

Trapped vortex combustor and method for operating the same

Apparatuses, systems, and methods for optimizing acoustic wave confinement to increase combustion efficiency

Volute trapped vortex combustor assembly

Ultra compact combustor

Fuel nozzle assembly having the leading edges of neighboring swirler vanes spaced at different distances

Fuel manifolds

Fuel injector systems and support structures

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

Gas Turbine Combustor

Fuel nozzle assembly and gas turbine combustor including the same

Fuel manifolds

Fuel systems

Finely distributed combustion system for a gas turbine engine

Combustor premixer assembly including inlet lips

Method of selective combustor control for reduced emissions

COMBUSTOR AND COMBUSTOR ARRAY

Gas turbine load/unload path control

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

Pilot burner assembly with pilot-air supply

Premixed fuel nozzle

Fuel staging for rotating detonation combustor

Afterburner system for turbofan engine

Consumable support structures for additively manufactured combustor components

Automated tuning of multiple fuel gas turbine combustion systems

Combustor and gas turbine including the same

Fuel nozzle structure for air assist injection

Method for minimizing forces acting on turbine blades in specific frequency ranges

Burner arrangement having a peripheral staging concept

Fuel oil axial stage combustion for improved turbine combustor performance

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Engine With Rotating Detonation Combustion System

Engine with rotating detonation combustion system

Combustion chamber comprising two types of injectors in which the sealing members have a different opening threshold

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

Ultra compact combustor

Combustor assembly with primary and auxiliary injector fuel control

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

Automated tuning of gas turbine combustion systems

Power-generation Gas Turbine with Fuel Injection Using a Dielectric of a Resonator

Power-generation Gas Turbine with Fuel Injection Using a Conductor of a Resonator

Fuel injector systems and support structures

Injectors for gas turbine combustion chamber

Method of controlling fuel injection in a reheat combustor for a combustor unit of a gas turbine

Volute trapped vortex combustor assembly

SEGMENTED FUEL DISTRIBUTOR

Gas turbine combustor flame holder

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

GAS TURBINE COMBUSTOR AND GAS TURBINE

Trapped vortex combustor and method for operating the same

Premixing fuel injectors and methods of use in gas turbine combustor

GAS TURBOMACHINE FUEL SYSTEM, CONTROL SYSTEM AND RELATED GAS TURBOMACHINE

Acoustic damper with barrier member configured to dampen acoustic energy propogating upstream in gas flow

Pilot nozzle with inline premixing

Auxiliary torch ignition

Auxiliary Torch Ingnition

System and method for igniting liquid fuel in a gas turbine combustor

Liquid fuel cartridge unit for gas turbine combustor and method of assembly

Cooling of liquid fuel cartridge in gas turbine combustor head end

FUEL NOZZLE ASSEMBLY FOR REDUCING MULTIPLE TONE COMBUSTION DYNAMICS

Fuel injectors and methods of fabricating same

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

Combustor

Flexible swirlers

Method and equipment for combustion of ammonia

System for dissipating fuel egress in fuel supply conduit assemblies

TOROIDAL COMBUSTION CHAMBER

Combustor for rotating detonation engine and method of operating same

Model-less combustion dynamics autotune

Mini mixing fuel nozzle assembly with mixing sleeve

Sequential combustion with dilution gas mixer

Slinger combustor having main combustion chamber and sub-combustion chamber, and gas turbine engine system having the same

Bluff body fuel mixer

Burner, combustor, and gas turbine

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

Combustors and methods of assembling the same

Method and device for combustion with pulsed fuel split

Burner, combustor, and gas turbine

SINGLE CAN VORTEX COMBUSTOR

Integrated combustor nozzle for a segmented annular combustion system

Segmented annular combustion system

Panel fuel injector

GAS TURBINE WITH SEQUENTIAL COMBUSTION ARRANGEMENT

Segmented annular combustion system

COMBUSTOR AND GAS TURBINE ENGINE

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

Method for combusting a fuel, and combustion device

Flow volume ratio calculation device, control device equipped with same, gas turbine plant equipped with this control device, flow volume ratio calculation method, and fuel line control method

Fuel injector

Segmented annular combustion system with axial fuel staging

FUEL SUPPLY SYSTEM FOR AN ENGINE

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

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

Staged fuel and air injectors in combustion systems of gas turbines

Combustion staging system

Fuel supply conduit assemblies

Burner for a can combustor

Cooling system for fuel nozzles within combustor in a turbine engine

Catalytic ignition system

Burner for a can combustor

Fuel injector with a center body assembly for liquid prefilm injection

System for Injecting a Liquid Fuel into a Combustion Gas Flow Field

Staged fuel and air injection in combustion systems of gas turbines

Fuel injection device

Fuel nozzle with fluid lock and purge apparatus

Pressure damping device for fuel manifold

Gas turbine combuster

Afterburner and aircraft engine

Method and device to control a fuel split in a combustion device

Combustor for gas turbine engine

ENGINE LUBRICATION SYSTEM USING DE-OXYGENATED FUEL

Sequential combustion arrangement with cooling gas for dilution

Combustor assembly for a gas turbine engine and method of making same

Trapped vortex cavity staging in a combustor

Fuel nozzle structure for air assist injection

Afterburner and aircraft engine

Systems and methods for control of combustion dynamics in combustion system

Multi-point injection device for an aircraft engine

Air shrouds with improved air wiping

Combustor and gas turbine

Fuel nozzle for a gas turbine engine

Fuel staging in a gas turbine engine

Angled radial fuel/air delivery system for combustor

Fuel supply system for a gas turbine combustor

Fuel injection device for a gas turbine having streamlined bodies with lobe structure

Flexible swirlers

Bluff body fuel mixer

Method and system for injecting fuel into an engine combustion chamber

Separate feedings of cooling and dilution air

Injection systems for fuel and gas

Injector apparatus with reheat combustor and turbomachine

Injector apparatus and reheat combustor

Injecting apparatus with reheat combustor and turbomachine

Device for determining a fuel split, as gas turbine or an aircraft engine comprising such a device and application of the same

TOROIDAL COMBUSTION CHAMBER

Combustor arrangement for a gas turbine

Combustor with axial staging for a gas turbine engine

Combustor arrangement for a gas turbine

Automated tuning of gas turbine combustion systems

Automated tuning of multiple fuel gas turbine combustion systems

Combustion chamber and a method of mixing fuel and air in a combustion chamber

Dilution gas or air mixer for a combustor of a gas turbine

Low NOturbine exhaust fuel burner assembly

Fuel injector to facilitate reduced NOemissions in a combustor system

Sequential combustor arrangement with a mixer

TURBO MACHINE COMBUSTION ASSEMBLY COMPRISING AN IMPROVED FUEL SUPPLY CIRCUIT

Multifuel gas turbine combustor with fuel mixing chamber and supplemental burner

SYSTEM AND METHOD FOR CONTROL OF COMBUSTION DYNAMICS IN COMBUSTION SYSTEM

Ultra compact combustor having reduced air flow turns

BURNER WITH ADJUSTABLE RADIAL FUEL PROFILE

Fuel delivery system with moveably attached fuel tube

Systems and methods for control of combustion dynamics and modal coupling in gas turbine engine

System for cooling a fuel injector extending into a combustion gas flow field and method for manufacture

Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine

Toroidal combustion chamber

Combustor with fuel injector pegs for reducing combustion pressure oscillations

Combustor assembly for a turbine engine

System and method for reducing modal coupling of combustion dynamics

SYSTEMS AND METHODS FOR REDUCING MODAL COUPLING OF COMBUSTION DYNAMICS

System and method for reducing modal coupling of combustion dynamics

Combustor

Sequential combustion arrangement with dilution gas

Combustor for a sequential gas turbine having a deflection unit between first and second combustion chambers

Sequential combustion with dilution gas mixer

Gas turbine with sequential combustion arrangement

Fuel injection device

Burner of gas turbine with fuel nozzles to inject fuel

Dual-fuel injector with a double pipe sleeve gaseus fuel flow path

Flamesheet combustor contoured liner

Sequential combustion with dilution gas mixer

Mixing arrangement for mixing a fuel with a stream of oxygen containing gas

GAS TURBINE COMBUSTOR

Combustion device having a distribution plenum

Gas turbine engine and method of operating thereof

Combustor apparatus in a gas turbine engine

Gas turbine engine system and an associated method thereof

Combustor and method for supplying fuel to a combustor

Fuel injector having an ignitor for igniting a combustor of a gas turbine

Combustor with fuel staggering for flame holding mitigation

Can combustor for a can-annular combustor arrangement in a gas turbine

Two-branch mixing passage and method to control combustor pulsations

Combustor support assembly for mounting a combustion module of a gas turbine

Flow sleeve for a combustion module of a gas turbine

Continuous combustion liner for a combustor of a gas turbine

System for providing fuel to a combustor

Systems and apparatus relating to downstream fuel and air injection in gas turbines

Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece

Multi-zone combustor

System for providing a working fluid to a combustor

Combustor apparatus in a gas turbine engine

Two-shaft gas turbine

Detecting flashback by monitoring engine-dynamic spikes

Systems and methods for late lean injection premixing

System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system

Turbomachine and staged combustion system of a turbomachine

Combustor and method of supplying fuel to the combustor

Method for operating a gas turbine burner with a swirl generator

Reheat burner arrangement having an increasing flow path cross-section

Burner for a combustion chamber of a gas turbine having a mixing and injection device

One-piece fuel nozzle for a thrust engine

Air management arrangement for a late lean injection combustor system and method of routing an airflow

Combuster with radial fuel injection

Flamesheet combustor dome

Variable length combustor dome extension for improved operability

Seal for use between injector and combustion chamber in gas turbine

Method for mixing a dilution air in a sequential combustion system of a gas turbine

Combustor

Combustion chamber and a method of mixing fuel and air in a combustion chamber

Combustor With Multiple Combustion Zones With Injector Placement for Component Durability

System and method for supplying a working fluid to a combustor

Combustor and method for supplying fuel to a combustor

Combustion device with pulsed fuel split

FUEL INJECTOR WITH INCREASED FEED AREA

COMBUSTOR AND METHOD FOR REDUCING THERMAL STRESSES IN A COMBUSTOR

System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold

Combustor assembly in a gas turbine engine

Symmetric fuel injection for turbine combustor

System for secondary fuel injection in a gas turbine engine

Automated tuning of multiple fuel gas turbine combustion systems

Gas turbine engine and annular combustor with swirler

Gas turbine engine including secondary combustion chamber integrated with the stator vanes in the turbine/expansion section of the engine and a method of operating the same

Methods and systems for cooling a transition nozzle

Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications

Fuel-air mixture distribution for gas turbine engine combustors

Fuel injection assembly for use in turbine engines and method of assembling same

Flashback resistant tubes for late lean injector and method for forming the tubes

System and method for damping combustor nozzle vibrations

System and method for conditioning a working fluid in a combustor

Split control unit

Premixing apparatus for gas turbine system

Method for operating a firing plant

Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines

Cooling scheme for an increased gas turbine efficiency