CO-FIRING COMBUSTOR WITH GAS FUEL AND LIQUID AMMONIA

SUPER COMPACT COMBUSTOR

Gas Turbine System

NONPREMIXED, RICH, RELAX, LEAN COMBUSTOR

METHOD OF GENERATING GAS TURBINE FUEL AND GAS TURBINE SYSTEM

SYSTEM AND METHOD FOR GENERATING ELECTRICITY AND HEAT FROM THE COMBUSTION OF TAIL GAS CONTAINING BIOGENIC METHANE USING A GAS TURBINE

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

POWERPLANT WITH MULTIPLE INTEGRATED GAS TURBINE ENGINES

Method and device for recursive sequential combustion

BIMODAL COMBUSTION SYSTEM

Liquid hydrogen-liquid oxygen fueled powerplant

METHOD OF GENERATING GAS TURBINE FUEL AND GAS TURBINE SYSTEM

Mixer

Axial fuel staging system for gas turbine combustors

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

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

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

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

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

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

MIXER

Fuel injectors and methods of use in gas turbine combustor

Method and equipment for combustion of ammonia

Vortex generating device

Vortex generating device

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

Dual fuel concentric nozzle for a gas turbine

Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device

Sequential combustion with dilution gas mixer

Burner assembly for a burner of a gas turbine

Constant-volume combustion module for a turbine engine, comprising communication-based ignition

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

Integrated combustor nozzle for a segmented annular combustion system

GAS TURBINE WITH SEQUENTIAL COMBUSTION ARRANGEMENT

Burner for a can combustor

Burner for a can combustor

Staged fuel and air injection in combustion systems of gas turbines

Turbine engine assembly and method of assembling the same

Sequential combustion arrangement with cooling gas for dilution

Sequential combustor and method for operating the same

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

Mixing system

Vortex generating arrangement for a pre-mixing burner of a gas turbine and gas turbine with such vortex generating arrangement

Sequential combustor arrangement with a mixer

Separate feedings of cooling and dilution air

Mixer for admixing a dilution air to the hot gas flow

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

Sequential burner for an axial gas turbine

Burner of a gas turbine with a lobed shape vortex generator

Fuel lance cooling for a gas turbine with sequential combustion

Lobe lance for a gas turbine combustor

Combustor arrangement for a gas turbine

Combustor arrangement for a gas turbine

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

Sequential combustion with dilution gas

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

Sequential combustor arrangement with a mixer

Gas turbine engine

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

Sequential combustion with dilution gas mixer

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

Method for a part load CO reduction operation for a sequential gas turbine

Sequential combustion with dilution gas mixer

Burner arrangement and method for operating a burner arrangement

Gas turbine with improved part load emissions behavior

Combustion device having a distribution plenum

Gas turbine engine and method of operating thereof

Gas turbine engine and method of operating thereof

Gas turbine engine and method of operating thereof

Check valve for propulsive engine combustion chamber

GAS TURBINE

Method for operating a gas turbine burner with a swirl generator

Reheat burner arrangement having an increasing flow path cross-section

Damper arrangement for reducing combustion-chamber pulsation

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

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

Gas turbine assembly and corresponding operating method

Gas turbine combustion system

System for supplying a working fluid to a combustor

System and method for supplying a working fluid to a combustor

Combustor and method for supplying fuel to a combustor

System for secondary fuel injection in a gas turbine engine

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

Multi-combustor turbine

Fuel injector

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

TURBOMACHINE COMBUSTORS HAVING DIFFERENT FLOW PATHS

Flow straightener and mixer

Reheat burner injection system with fuel lances

Gas turbine reheat combustor including a fuel injector for delivering fuel into a gas mixture together with cooling air previously used for convectively cooling the reheat combustor

Reheat burner injection system

Burner arrangement with deflection elements for deflecting cooling air flow

Reheat burner

Reheat burner

Gas turbine with improved part load emissions behavior

Gas turbine system having premixed injector vanes

AERODYNAMIC FLAME STABILIZER

Sequential combustor gas turbine including a plurality of gaseous fuel injection nozzles and method for operating the same

Method for switching over a gas turbine plant from gaseous fuel to liquid fuel and vice-versa

Method for operating a gas turbine plant

Aerodynamic pylon fuel injector system for combustors

Fuel injection method

Burner of a gas turbine

Burner for a gas turbine and method for feeding a gaseous fuel in a burner

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

Combustor for a gas turbine engine with effusion cooled baffle

Fuel lance for a gas turbine engine including outer helical grooves

Gas turbogroup

Exhaust gas guide of a gas turbine and method for mixing the exhaust gas of the gas turbine

Gas turbine system and method of operation

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

Concentric fixed dilution and variable bypass air injection for a combustor

Reheat combustion system for a gas turbine

System and method for generating electricity and heat from the combustion of tail gas containing biogenic methane using a gas turbine

Method of operating a combustor with a variable combustion chamber