GAS TURBINE ENGINE WITH FUEL DISTRIBUTING COMPRESSOR IMPELLER

CRYOGENIC FUEL START UP SYSTEM

FUEL-COOLED ENGINE COMPONENT(S)

PROPULSION SYSTEM COMPRISING A HYDROGEN-BURNING GAS TURBINE ENGINE

FUEL SUPPLY METHOD, FUEL SUPPLY SYSTEM, FUEL COMBUSTION SYSTEM PROVIDED WITH FUEL SUPPLY SYSTEM, AND GAS TURBINE PLANT

Gas turbine plant with ammonia decomposition system

HYDROGEN FUEL SYSTEM

FUEL INJECTOR AIR SWIRLER STRUCTURE WITH CANTED FLOW GUIDE SURFACE

TURBINE ENGINE FUEL INJECTOR ASSEMBLY WITH ANNULAR FUEL OUTLET

COMBINED AIR SWIRLER AND FUEL DISTRIBUTOR

SYSTEM AND METHOD HAVING FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE

Alternative fuel fast start systems for gas turbine engines

INJECTION TECHNIQUES FOR GAS TURBINE SYSTEMS

System and Method for Diluting Vapor and Generating Electricity

Fuel-cooled engine component(s)

REGENERATIVE COOLING AND ADJUSTABLE THROAT FOR ROTATING DETONATION ENGINE

Fuel injectors assemblies with tangential flow component

METHODS AND SYSTEMS FOR STARTING HYDROGEN POWERED GAS GENERATORS

AIRCRAFT POWER PLANT WITH HYDROGEN TURBO-EXPANDER

Pericritical fluid systems for turbine engines

Jet nozzle, combustor, and gas turbine including same

Jet nozzle, combustor, and gas turbine including same

FUEL SUPPLY METHOD, FUEL SUPPLY SYSTEM, FUEL COMBUSTION SYSTEM PROVIDED WITH FUEL SUPPLY SYSTEM, AND GAS TURBINE PLANT

Afterburner structure with self-excited sweeping oscillating fuel injection nozzles

PURGE SYSTEM FOR A HYDROGEN FUEL SYSTEM

System and method for diluting vapor and generating electricity

Fuel system including driving turbine

Fuel injector with splash plate for an engine

IGNITER INTEGRATED WITH TURBINE FUEL INJECTOR

Liquid hydrogen-liquid oxygen fueled powerplant

MULTIPLE TURBOEXPANDER SYSTEM HAVING SELECTIVE COUPLER

FUEL SUPPLY SYSTEM FOR A COMBUSTOR

NOZZLE ASSEMBLY WITH NOZZLE HEAD HAVING GUIDE ELEMENT

Method for determining characteristics of a fuel supplied to an aircraft engine

SYSTEM FOR PURGING A FUEL HAVING REACTIVE GAS

Burner component of a burner, and burner of a gas turbine having a burner component of this type

TANGENTIAL TURBOFAN PROPULSION SYSTEM

Fuel delivery system with purge gas step and fuel gas flushing step and method thereof

Fuel circuit for a fuel injector

Water fuel emulsion system and method for gas turbine

RADIAL EQUILIBRATED COMBUSTION NOZZLE ARRAY

ENGINE USING HEATED AND TURBO-EXPANDED AMMONIA FUEL

Methods and systems for starting hydrogen powered gas generators

Heat shield for fuel nozzle

Multi-fuel, fuel injection system for a turbine engine

Regenerative cooling and adjustable throat for rotating detonation engine

TURBINE ENGINE FUEL INJECTOR WITH NON-CIRCULAR NOZZLE PASSAGE

Removing safety markers from a hydrogen fuel system

FUEL MIXER

Fuel-cooled engine component(s)

Injection nozzle, combustor including same nozzle, and gas turbine including same combustor

Injection nozzle, combustor including same, and gas turbine including same

Hydrogen fuel system

Fuel delivery system for delivering hydrogen fuel to a fuel injection system in a complex cycle gas turbine engine

Fuel injector assembly for a turbine engine

Combustor nozzle, and combustor and gas turbine including the same

Fuel circuit for a fuel injector

Fuel injector

Fluid distributors for fluid nozzles

ENGINE USING HEATED AND TURBO-EXPANDED AMMONIA FUEL

FUEL INJECTION DEVICE FOR GAS TURBINE

Gas Turbine Combustor and Fuel Nozzle Manufacturing Method

Jet engine

NOZZLE WITH JET GENERATOR CHANNEL FOR FUEL TO BE INJECTED INTO A COMBUSTION CHAMBER OF AN ENGINE

FUEL INJECTION DEVICE FOR GAS TURBINE

Organic Rankine Cycle for combined-cycle power plant

Liquid fuel injection body

Combustion chamber of a gas turbine, gas turbine and method for operating the same

METHOD AND SYSTEM FOR AERO-SHAPED LIQUID FUEL POSTS FOR MICROMIXERS

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

Injector of an over-enriched fuel-and-air mixture to the combustion chamber of internal combustion engines

AIR-SHIELDED FUEL INJECTION ASSEMBLY TO FACILITATE REDUCED NOX EMISSIONS IN A COMBUSTOR SYSTEM

CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE

Rotating detonation engine multi-stage mixer

METHOD FOR IMPROVING THE PERFORMANCE AND EFFICIENCY OF DIESEL, GAS-TURBINE, TURBO-JET COMBUSTION ENGINE

Cooled component having effusion cooling apertures

Diffuser mounted fuel-air heat exchanger

Air-shielded fuel injection assembly to facilitate reduced NOemissions in a combustor system

FUEL VAPORIZER FOR A TURBINE ENGINE COMBUSTOR

Cooled cooling air taken directly from combustor dome

Gas turbine engine systems and methods involving enhanced fuel dispersion

System and method for reducing modal coupling of combustion dynamics

Bundled tube fuel injector with outer shroud and outer band connection

LATE LEAN INJECTION MANIFOLD MIXING SYSTEM

Cavity swirl fuel injector for an augmentor section of a gas turbine engine

Gas turbine centripetal annular combustion chamber and method for flow guidance

SYSTEM FOR CONDITIONING AIR FLOW INTO A MULTI-NOZZLE ASSEMBLY

METHOD AND ASSEMBLY FOR RETROFITTING A GAS TURBINE COMBUSTOR END COVER

Apparatus for fuel injection in a turbine engine

Gas turbine engine systems and methods involving enhanced fuel dispersion

Ejectors with separably secured nozzles, adjustable size nozzles, or adjustable size mixing tubes

Gas turbine integrated with fuel catalytic partial oxidation

Rotary injector

Gas turbine engine hydrogen supply system and method

Fuel-air mixer for turbine engine combustion section

Combustor with tangential fuel and air flow

Combustor with helix air and fuel mixing passage

Fuel injector manifold having trim device therein