FLAMEHOLDER FOR A REHEAT ASSEMBLY

INJECTOR ASSEMBLY FOR AN ENGINE, AND AIRCRAFT

PROPULSION SYSTEM FOR JET NOISE REDUCTION

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

COMBUSTOR AND GAS TURBINE

ROTATING DETONATION-ENABLED AUGMENTOR SYSTEMS

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

Fuel injection device for a turbojet engine afterburner

Diffusion cone for the rear part of a jet engine incorporating a flame-holder ring at the trailing edge

Gas turbine combustor structure

MULTITUBE PILOT INJECTION INTO TRAPPED VORTICES IN A GAS TURBINE ENGINE

MULTITUBE PILOT INJECTOR HAVING AN INSULATED MANIFOLD FOR A GAS TURBINE COMBUSTOR

Trailing edge fuel injection enhancement for flame holding mitigation

Afterburner structure with self-excited sweeping oscillating fuel injection nozzles

PROPULSION SYSTEM FOR JET NOISE REDUCTION

REHEAT ASSEMBLY FOR GAS TURBINE ENGINE

Reheat assembly

Hydrogen and oxygen supplemental firing for combined-cycle facility

FUEL NOZZLE WITH RESTRICTED CORE AIR PASSAGE

Multitube pilot injector having a split airflow for a gas turbine engine

Systems and methods for spraying fuel in an augmented gas turbine engine

Swirl preburner system and method

Systems and methods for spraying fuel in an augmented gas turbine engine

Fuel nozzle and combustor and gas turbine including the same

Afterburner strut with integrated fuel feed lines

BURNER AND COMBUSTION METHOD FOR A BURNER

Fuel injector for hypersonic jet engine operation

Hydrogen and oxygen supplemental firing for combined cycle facility

Combustor having inner and outer tubular oxygen nozzles about a tubular fuel supply unit

Premixer for low emissions gas turbine combustor

FUEL DELIVERY SYSTEM WITH A CAVITY COUPLED FUEL INJECTOR

FUEL TESTER FOR CHARACTERIZATION OF THE SUSCEPTIBILITY TO THERMOACOUSTIC INSTABILITIES AND METHOD

Swirl preburner system and method

Gas turbine engine with a unitary structure and method for manufacturing the same

Thrust chamber device and method for operating a thrust chamber device

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

FUEL INJECTOR

Fuel nozzle and combustor and gas turbine including the same

Aerospace turbofan engines

GAS TURBINE COMBUSTOR AND GAS TURBINE

Burner assembly, combustor, and gas turbine

TRAILING EDGE BOX AND FUEL SPRAYBAR WITH INTERNAL PASSAGES

Jet engine, flying object, and operation method of jet engine

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

FUEL NOZZLE ASSEMBLY FOR REDUCING MULTIPLE TONE COMBUSTION DYNAMICS

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

Flight vehicle air breathing engine with isolator having bulged section

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

Combustion chamber of a turbine, in particular a thermodynamic cycle turbine with recuperator, for producing energy, in particular electrical energy

FUEL INJECTOR

FUEL INJECTOR

FUEL INJECTOR

Burner for a gas turbine

Combustor with axially staged fuel injection

Vortex generating device

Gas turbine combustor

Sequential combustion with dilution gas mixer

METHOD FOR OPERATING A COMBUSTION SYSTEM

Combustion chamber

Augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane

Additively manufactured augmentor vane of a gas turbine engine with additively manufactured fuel line extending therethrough

SYSTEMS AND METHODS FOR CONTROLLING FLAME INSTABILITY

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

Gas turbine engine afterburner

Closed trapped vortex cavity pilot for a gas turbine engine augmentor

High G-field Combustion

Burner for a can combustor

Burner for a can combustor

Staged fuel and air injection in combustion systems of gas turbines

Afterburner and aircraft engine

Combustor assembly for use in a gas turbine engine and method of assembling

FUEL INJECTOR

Sequential combustor and method for operating the same

Gas turbine fuel components

Fuel injection locations based on combustor flow path

In-stream burner module

Afterburner and aircraft engine

Fuel injector device

Combustor and gas turbine

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

Cooled fuel injector system for a gas turbine engine

Injector apparatus with reheat combustor and turbomachine

Injector apparatus and reheat combustor

Injecting apparatus with reheat combustor and turbomachine

Pivoting stowable spray bar

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

COMBUSTOR LINER

Lobe lance for a gas turbine combustor

Variable orifice jet for a turbine engine

Method and an apparatus for producing cooling apertures in a combustion chamber head

Gas turbine engine systems and methods involving enhanced fuel dispersion

Carbureted fuel injection system for a gas turbine engine

CHANNEL DEFINING FUEL NOZZLE OF COMBUSTION SYSTEM

System for reducing combustion dynamics by varying fuel flow axial distances

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

Sequential combustion with dilution gas mixer

Combustor dome heat shield

Gas turbine engine afterburner

Sequential combustion with dilution gas mixer

Burner arrangement and method for operating a burner arrangement

Continuous ignition

AFTERBURNER AND AIRCRAFT ENGINE

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

Flow sleeve for a combustion module of a gas turbine

Flow sleeve assembly for a combustion module of a gas turbine combustor

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

Fuel efficient ultra-low emission and improved pattern factor colorless distributed combustion for stationary and propulsion gas turbine applications

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

System and method for reducing modal coupling of combustion dynamics

Duct burner of HRSG with liner film cooling

Injection device for a combustion chamber of a turbine engine

Fuel delivery system with a cavity coupled fuel injector

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

FLEXIBLE COMBUSTOR BRACKET

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

Apparatuses and systems with vertically and longitudinally offset mounting flanges

Fuel manifold with jumper tubes

Leaf spring damper for a turbine engine fuel delivery system

COMBUSTOR ASSEMBLY FOR A GAS TURBOMACHINE

Fuel injector

Cooling scheme for an increased gas turbine efficiency

Flow straightener and mixer

Reheat burner injection system with fuel lances

Reheat burner injection system

Reheat burner injection system

Igniter

THRUST AUGMENTED GAS TURBINE ENGINE

Trapped vortex combustor and method of operating thereof

Side-initiated augmentor for engine applications

Combustor having a first plurality of fuel nozzles having a first cross-sectional shape and a second plurality of fuel nozzles having a second cross-sectional shape different than the first cross-sectional shape

Reheat burner

Reheat burner

Controllable flameholder

Gas turbine system having premixed injector vanes

Coannular oil injection nozzle

AERODYNAMIC FLAME STABILIZER

Device for attaching a flame-holder arm to an afterburner housing

FLAME-HOLDER DEVICE COMPRISING AN ARM SUPPORT AND A HEAT-PROTECTION SCREEN THAT ARE IN ONE PIECE

Aerodynamic pylon fuel injector system for combustors

Fuel efficient ultra-low emission and improved pattern factor colorless distributed combustion for stationary and propulsion gas turbine applications

Convex Pilot Cone

Afterburner chamber for a turbomachine

Cooled flameholder swirl cup

Augmentor pilot

Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors

Gas turbine engine systems and methods involving enhanced fuel dispersion

Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct

Flame holder for minimizing combustor screech

Purged flameholder fuel shield

Augmentor with trapped vortex cavity pilot

Combustor and a fuel supply method for the combustor

GAS TURBINE GUIDE VANES WITH TANDEM AIRFOILS AND FUEL INJECTION AND METHOD OF USE

Two-stage hypersonic vehicle featuring advanced swirl combustion

Method and apparatus for assembling a flameholder for an augmenter

Fuel injector for a gas turbine engine

Secondary fuel injection from stage one nozzle

Augmentor variable vane flame stabilization

Flameholder arm for an afterburner

Augmentor radial fuel spray bar with counterswirling heat shield

Structural metering plate

Augmentor pilot nozzle

Structural track support of spraybars/tubing

Device for attaching a flame-arrestor arm to an afterburner casing and afterburner comprising such a device

Trapped vortex cavity afterburner

Gas turbine system and method of operation

Augmentor spray bars

Augmentor fuel conduit bushing

After-burner chamber with secure ignition

Compact swirl augmented afterburners for gas turbine engines

Augmenter swirler pilot

Method and apparatus for providing an afterburner fuel-feed arrangement

Device for fastening a fluid duct to a turbojet casing

Turbo-jet engine with a protective screen of the fuel manifold of a burner ring, the burner ring and the protective screen

Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojet

Method and apparatus for gas turbine engines

Device for feeding air and fuel to a burner ring in an after-burner chamber

Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine

Ablative afterburner

Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance

Afterburner arrangement

Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance

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