SYSTEM AND METHOD HAVING ISOTHERMAL COMBUSTION ALONG SET OF TURBINE BLADES VIA VARYING FLUID INJECTION ALONG SET OF TURBINE VANES

COMBUSTOR AND GAS TURBINE

GAS TURBINE COMBUSTOR AND GAS TURBINE

SCALEABLE ACOUSTICALLY-STABLE COMBUSTION CHAMBER AND DESIGN METHODS

ROTATING DETONATION-ENABLED AUGMENTOR SYSTEMS

TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAME

ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM

Piloting arrangement, nozzle device, gas turbine arrangement and method

System and method having flame stabilizers for isothermal expansion in turbine stage of gas turbine engine

SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE

FLAME-HOLDER DEVICE FOR A TURBOJET AFTERBURNER, COMPRISING THREE-BRANCHED ARMS

Gas turbine engine combustor with a set of dilution passages

Combustion system

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Dry low NOstaged combustion system

Combustor nozzle, combustor, and gas turbine including the same

FUEL NOZZLE FOR GAS TURBINE ENGINE COMBUSTOR

Trapped vortex combustor and method for operating the same

Control system and method for a burner with a distal flame holder

Scaleable acoustically-stable combustion chamber and design methods

CONTROL SYSTEM AND METHOD FOR A BURNER WITH A DISTAL FLAME HOLDER

Combustor and gas turbine including the combustor

Combustor and gas turbine

COMBUSTION CHAMBER ASSEMBLY FOR AN ENGINE HAVING HEAT SHIELDS AND/OR BURNER SEALS OF AT LEAST TWO DIFFERENT TYPES

Thrust chamber device and method for operating a thrust chamber device

Dilution Structure for Gas Turbine Engine Combustor

Engine with rotating detonation combustion system

Engine with rotating detonation combustion system

Engine With Rotating Detonation Combustion System

Engine with rotating detonation combustion system

Gas turbine combustor, gas turbine, and control method for gas turbine combustor

Fuel nozzle for gas turbine engine combustor

Jet engine with plasma-assisted afterburner

Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine

Gas turbine combustor flame holder

Trapped vortex combustor and method for operating the same

Burner assembly, combustor, and gas turbine

Rayleigh-Taylor assisted combustion with micro-flameholders

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

Coupling method and structure for a propulsion system hot section

Gas turbine exhaust cooling system

Scalable acoustically-stable combustion chamber and design methods

BURNER AND SUPPORT STRUCTURE WITH A PERFORATED FLAME HOLDER

Flame-holder device

Engine aft section structure

Systems and methods for flame holding avoidance in gas turbine combustors

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

Gas turbine combustor and gas turbine

Afterburner and aircraft engine

Combustor for gas turbine engine

APPARATUS AND METHOD FOR DAMPENING ACOUSTICS

Thrust increasing device

Sequential combustor and method for operating the same

In-stream burner module

Afterburner and aircraft engine

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

Fuel lance cooling for a gas turbine with sequential combustion

Lobe lance for a gas turbine combustor

Combustor dome damper system

Combustor and gas turbine

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

Fuel injection device

Sequential combustion with dilution gas mixer

Annular combustion chamber in a turbine engine

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

Process for operating a dual-mode combustor

Combustion device having a distribution plenum

Gas turbine engine and method of operating thereof

Gas turbine engine and method of operating thereof

Method and Apparatus for Enhanced Flameholding in Augmentors

Combustion systems and combustion system components for rotary ramjet engines

MICRO-MIXER/COMBUSTOR

System for reducing combustion dynamics

Gas turbine combustor including a premixing chamber having an inner diameter enlarging portion

Reheat burner arrangement having an increasing flow path cross-section

Gas turbine combustor

System for reducing combustion dynamics

MULTI-STEP COMBUSTOR

Air fuel premixer having arrayed mixing vanes for gas turbine combustor

Flow straightener and mixer

Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone

Ejector purge of cavity adjacent exhaust flowpath

Method and apparatus for enhanced flameholding in augmentors

Burner including non-uniformly cooled tetrahedron vortex generators and method for cooling

Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel

GAS TURBINE COMBUSTOR FLAME STABILIZER

Fuel nozzle for a gas turbine engine and method for fabricating the same

Flame holder for minimizing combustor screech

Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel

Combustor

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

Monobloc flameholder arm for an afterburner device of a bypass turbojet

Device for stabilizing combustion in gas turbine engines

Burner for a gas-turbine combustion chamber

System and method having flame stabilizers for isothermal expansion in turbine stage of gas turbine engine