Combustion control device, combustion system, combustion control method and program

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

Combustor arrangement for a gas turbine

Combustor with axial staging for a gas turbine engine

Combustor arrangement for a gas turbine

Method of operating a multi-stage flamesheet combustor

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

Bulk flame temperature regulator for dry low emission engines

Sequential combustion with dilution gas

Multi-stage combustor with a linear actuator controlling a variable air bypass

Multifuel gas turbine combustor

METHOD OF OPERATING A GAS TURBINE WITH STAGED AND/OR SEQUENTIAL COMBUSTION

Axially staged gas turbine combustor with interstage premixer

Sequential combustor arrangement with a mixer

Gas turbine combustor

Combined Gas Turbine Auxiliary Systems

Multifuel gas turbine combustor with fuel mixing chamber and supplemental burner

SYSTEMS AND METHODS FOR COHERENCE REDUCTION IN COMBUSTION SYSTEM

Apparatus and a method of controlling the supply of fuel to a combustion chamber

Systems and methods for variation of injectors for coherence reduction in combustion system

Fuel delivery system with moveably attached fuel tube

Trapped vortex fuel injector and method for manufacture

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

Power generation system, driving method for power generation system, and combustor

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

MULTI-FUEL-CAPABLE GAS TURBINE COMBUSTOR

System and method for control of combustion dynamics in combustion system

Combustion system for a gas turbine engine and method of operating same

Turbine engine combustion assembly with a variable air supply

Combustor assembly for a turbine engine

Sequential combustion arrangement with dilution gas

METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR

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

LATE LEAN INJECTION MANIFOLD MIXING SYSTEM

Sequential combustion with dilution gas mixer

Wake reducing structure for a turbine system

Automated extended turndown of a gas turbine engine combined with incremental tuning to maintain emissions and dynamics

Gas turbine with sequential combustion arrangement

TURBOMACHINE COMBUSTOR HAVING AN EXTERNALLY FUELED LATE LEAN INJECTION (LLI) SYSTEM

GAS TURBINE AND METHOD TO OPERATE THE GAS TURBINE

Combustor and method of fuel supply and converting fuel nozzle for advanced humid air turbine

Sequential combustion with dilution gas mixer

Burner arrangement and method for operating a burner arrangement

Gas turbine with improved part load emissions behavior

System for performing staging control of a multi-stage combustor

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

Combustor apparatus in a gas turbine engine

Fuel air premix chamber for a gas turbine engine

Gas turbine engine system and an associated method thereof

Combustor and method for supplying fuel to a combustor

Method and arrangement for injecting an emulsion into a flame

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

Combustor with fuel staggering for flame holding mitigation

Methods and systems for controlling the products of combustion

Methods relating to downstream fuel and air injection in gas turbines

Hot gas path duct for a combustor of a gas turbine

Continuous combustion liner for a combustor of a gas turbine

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

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

Multi-zone combustor

Rich burn, quick mix, lean burn combustor

Two-shaft gas turbine

Stabilizing a gas turbine engine via incremental tuning during transients

Lean-rich axial stage combustion in a can-annular gas turbine engine

Fuel injector for supplying fuel to a combustor

Systems and methods for late lean injection premixing

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

SYSTEM FOR PROVIDING FUEL TO A COMBUSTOR ASSEMBLY IN A GAS TURBINE ENGINE

Fuel injection assemblies in combustion turbine engines

Damper arrangement for reducing combustion-chamber pulsation

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

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

Combuster with radial fuel injection

Multipoint fuel injection arrangements

SYSTEM AND METHOD FOR STAGING FUEL TO A COMBUSTOR

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

Gas turbine assembly and corresponding operating method

Reheat burner and method of mixing fuel/carrier air flow within a reheat burner

System for supplying a working fluid to a combustor

Gas turbine combustor and operating method for gas turbine combustor

Gas turbine combustion system

METHOD OF REDUCING COMBUSTION INDUCED OSCILLATIONS IN A TURBINE ENGINE

Secondary Combustion System

Fuel injector with mixing circuit

System for supplying a working fluid to a combustor

System and method for supplying a working fluid to a combustor

Transition duct with late injection in turbine system

System for supplying fuel to a late-lean fuel injector of a combustor

System for supplying fuel to late-lean fuel injectors of a combustor

Low emissions combustion apparatus and method

Combustor and method for supplying fuel to a combustor

System for supplying a fuel and a working fluid through a liner to a combustion chamber

System for supplying a fuel and working fluid mixture to a combustor

LATE LEAN INJECTION SYSTEM

Liquid fuel swirler

Rational late lean injection

SYSTEM AND METHOD FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR

System and method for supplying a working fluid to a combustor

Late lean injection system transition piece

Combustor assembly in a gas turbine engine

System for secondary fuel injection in a gas turbine engine

Flowsleeve of a turbomachine component

Combustor of a turbomachine including multiple tubular radial pathways arranged at multiple circumferential and axial locations

System and method for flame stabilization

Two-stage combustor for gas turbine engine

Two-stage combustor for gas turbine engine

Two-stage combustor for gas turbine engine

Fuel nozzle and method of repair

COMBUSTOR ASSEMBLY FOR A GAS TURBOMACHINE

Multi-combustor turbine

INJECTION APPARATUS

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

Use of an emissions sensor to control fuel flow staging

Cast manifold for dry low NOx gas turbine engine

Fuel injector

Flow balancing valve

Multipoint injectors with auxiliary stage

Assemblies and apparatus related to integrating late lean injection into combustion turbine engines

Assemblies and apparatus related to integrating late lean injection into combustion turbine engines

Methods relating to integrating late lean injection into combustion turbine engines

Combustor portion for a turbomachine and method of operating a turbomachine

REDUCTION OF CO AND O2 EMISSIONS IN OXYFUEL HYDROCARBON COMBUSTION SYSTEMS USING OH RADICAL FORMATION WITH HYDROGEN FUEL STAGING AND DILUENT ADDITION

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

Methods and systems for cooling a transition nozzle

Controlling a combustion device to lower combustion-induced pulsations by changing and resetting fuel stagings at different rates of change

TURBOMACHINE COMBUSTORS HAVING DIFFERENT FLOW PATHS

INJECTOR APPARATUS

Integrated late lean injection on a combustion liner and late lean injection sleeve assembly

Multipoint injectors with standard envelope characteristics

MULTI-FUEL COMBUSTION SYSTEM

Communicating structure between adjacent combustors and turbine portion and gas turbine

Gas turbine combustor having a fuel nozzle for flame anchoring

Axial stage combustor for gas turbine engines

Fuel injector

FUEL INJECTOR

Combustor with fuel staggering for flame holding mitigation

Gas turbine combustor and fuel supply method used for the same

Low calorific value fuel combustion systems for gas turbine engines

Combustion chamber and method for operating a combustion chamber

Burner arrangement with deflection elements for deflecting cooling air flow

Fuel gas cooling system for combustion basket spring clip seal support

Combustor and the method of fuel supply and converting fuel nozzle for advanced humid air turbine

BURNER FOR A GAS COMBUSTOR AND A METHOD OF OPERATING THE BURNER THEREOF

Methods and systems for controlling the products of combustion

Self-regulating fuel staging port for turbine combustor

Combustor exit temperature profile control via fuel staging and related method

Multiple Zone Pilot For Low Emission Combustion System

Combustor with Pre-Mixing Primary Fuel-Nozzle Assembly

AERODYNAMIC FLAME STABILIZER

Gas turbine combustor with staged combustion

Bled diffuser fed secondary combustion system for gas turbines

FUEL INJECTION IN SECONDARY FUEL NOZZLE

Low NOx combustor for hydrogen-containing fuel and its operation

MULTI-FUEL COMBUSTION SYSTEM

Fuel nozzle and method of repair

System and method using low emissions gas turbine cycle with partial air separation

Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine

Method of fuel staging in combustion apparatus

Combustion cavity layouts for fuel staging in trapped vortex combustors

Vortex premixer for combustion apparatus

Inlet premixer for combustion apparatus

Burner

Fuel Staging in a Burner

Size scaling of a burner

Quarls in a burner

COMBUSTOR CASING

Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor

Low emissions combustion apparatus and method

Stabilizing a gas turbine engine via incremental tuning

Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle

COMBUSTOR OF GAS TURBINE

Gas turbine control method and gas turbine power generating apparatus

Secondary combustion system for reducing the level of emissions generated by a turbomachine

At least one combustion apparatus and duct structure for a gas turbine engine

Gas turbine combustor including separate fuel injectors for plural zones

Fuel nozzle with multiple fuel passages within a radial swirler

Conical gas turbine burner having a fuel lance with inclined side nozzles

Late lean injection fuel staging configurations

Late lean injection for fuel flexibility

Late lean injection with expanded fuel flexibility

Late lean injection control strategy

Quench jet arrangement for annular rich-quench-lean gas turbine combustors

DLN DUAL FUEL PRIMARY NOZZLE

STAGED COMBUSTION SYSTEMS AND METHODS

Combustor for a gas turbine engine with effusion cooled baffle

Methods of reducing emissions for a sequential combustion gas turbine and combustor for a gas turbine

Combustor Apparatus for Use in a Gas Turbine Engine

Combustor assembly in a gas turbine engine

Burner fuel staging

COMBUSTOR SYSTEM AND METHOD OF REDUCING COMBUSTION INSTABILITY AND/OR EMISSIONS OF A COMBUSTOR SYSTEM

Gas Turbine Burner and Method of Operating a Gas Turbine Burner

Combustor apparatus in a gas turbine engine

Burner and fuel lance for a gas turbine installation

Axially staged combustion system for a gas turbine engine

Apparatus for Modifying the Content of a Gaseous Fuel

Combustion cap with crown mixing holes

Fuel distribution system for a gas turbine with multistage burner arrangement

Apparatus and method for controlling the secondary injection of fuel

Secondary fuel delivery system

Multi-stage axial combustion system

Methods and systems to facilitate reducing NOemissions in combustion systems

Fuel injector for a gas turbine engine combustion chamber

Method and apparatus for reducing gas turbine engine emissions

Gas turbine engine combustion systems

Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor

Combustor for gas turbine

Burner system with staged fuel injection

Multimode fuel injector for combustion chambers, in particular of a jet engine

Gas turbine engine premix injectors

Independent pilot fuel control in secondary fuel nozzle

Low emission combustion and method of operation

Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement

Combustor for gas turbine engine

Multi-point staging strategy for low emission and stable combustion

Method and system for operating a multi-stage combustor

Thermal power plant with sequential combustion and reduced-COemission, and a method for operating a plant of this type

Inboard radial dump venturi for combustion chamber of a gas turbine

Catalytic combustor having fuel flow control responsive to measured combustion parameters

Fuel system

Trapped vortex combustor cavity manifold for gas turbine engine

Low emissions combustion apparatus and method

Non-catalytic combustor for reducing NOx emissions

Method and system for controlling fuel supply in a combustion turbine engine

Fuel supply method and fuel supply system for fuel injection device

Fuel supply method and fuel supply system

Multi-point staging strategy for low emission and stable combustion

Gas turbine engine combustor can with trapped vortex cavity

Multi-stage combustion using nitrogen-enriched air

System and method for fuel injection in turbine section of gas turbine engine

Hydrogen capable fuel injector assembly

Axial fuel stage injector creating air curtain

Axial fuel stage injector with fuel injection in same direction as high-pressure air flow

Gas turbine adaptive secondary fuel filling profile

Cluster of swirled mini-mixers for fuel-staged, axially staged combustion

Combustion section with a primary combustion chamber and a secondary combustion chamber

Fuel injection assembly for a combustor

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

Gas turbine engine combustor with primary and secondary fuel injectors

Methods of operating a turbomachine combustor on hydrogen

Integrated combustion nozzle having a unified head end

Tangential annular combustor with premixed fuel and air for use on gas turbine engines

Tangential and flameless annular combustor for use on gas turbine engines