TURBOMACHINE IMPINGEMENT COOLING MODULES

ROTATING DETONATION ENGINE FOR POWER GENERATION

SOLID OXIDE FUEL CELL ASSEMBLY

DESIGN METHOD FOR AXIAL MULTI-STAGE COMBUSTOR AND AXIAL MULTI-STAGE COMBUSTOR APPLYING THE SAME METHOD

Gas Turbine System

System and Method of Air-Augmented Gas turbine Turbojet Engines

GAS TURBINE ENGINE COMBUSTOR HAVING CERAMIC MATRIX COMPOSITE (CMC) LINERS AND CMC DOME

GAS TURBINE ENGINE HAVING A COMBUSTION SECTION WITH STEAM PROVIDED TO SECOND COMBSUTOR PLENUM

THERMOPHOTOVOLTAIC ENERGY CONVERSION IN GAS TURBINE ENGINE

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

ADDITIVELY MANUFACTURED TAPERED TRANSITION PORTION AND AFT FRAME FOR REPLACEMENT OF EXISTING COMBUSTOR PARTS

ARTICLE AND METHOD FOR MANUFACTURING AN EXPANDED COMBUSTOR LINER

SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR

ROTATING DETONATION COMBUSTOR SYSTEM AND METHOD OF OPERATING THE ROTATING DETONATION COMBUSTOR SYSTEM

COMBUSTOR FOR A GAS TURBINE ENGINE

High Entropy Alloy Repair of Nickel and Cobalt Superalloys

COMBUSTOR APPARATUS

ANNULAR DOME ASSEMBLY FOR A COMBUSTOR

MONOLITHIC SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION

HIGH SHEAR FUEL DISTRIBUTOR

Aircraft power plant with detonation combustion tube

Gas turbine

GAS TURBINE

Gas turbine engine centrifugal compressor with impeller load and cooling control

Aircraft system with gas turbine engine powered compressor

Augmented drive of compressors via differential and multistage turbine

Impingement cooling apparatus support structure and method of manufacture

Pressure drag jet engine

Combustion device having a flameless combustion chamber, use of such a device and electricity production or energy cogeneration apparatus comprising such a device

Impingement cooling apparatus for turbomachine

Annular dome assembly for a combustor

SOLID OXIDE FUEL CELL ASSEMBLY

TURBOFAN ENGINE

Combustor panels for gas turbine engines

Turbofan with offset gas generator and auxiliary power core

System and method for installation or removal of one or more combustion cans

ANTI-BACK-TRANSFER INTAKE STRUCTURE FOR ROTATING DETONATION COMBUSTION CHAMBER

Combustor for a gas turbine engine

Combustor for a gas turbine engine including a liner having a looped feature

Combustor for a gas turbine engine

Active boundary layer control in diffuser

Augmented drive of compressors via differential and multistage turbine

Combustor dilution hole

Gas turbine engine

Combined cooling heating and power micro gas turbine device

Turbine vane and gas turbine comprising same

Aircraft propulsion system with inter-turbine burner

Piloted rotating detonation engine

SYSTEM AND METHOD FOR TREATING WASTEWATER

Integral superstructure for load path optimization

Centrifical compressor assembly for a gas turbine engine

Article and method for manufacturing an expanded combustor liner

COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE

Two-stage combustor for gas turbine engine

Co-axial dual swirler nozzle

Combustor and gas turbine including the same

Assembly for a turbomachine

Volute trapped vortex combustor assembly

Ultra compact combustor

Method for operating a power plant

Combustion engine having a rotary compressor-combustor array

Microturbine and Combustor thereof

Multistage gas turbine engine with differential drive of compressor

Augmented drive of compressors via differential and multistage turbine

Combined heat and power system and method of operation

Combustor panels for gas turbine engines

COMBUSTOR MOUNTING STRUCTURES FOR GAS TURBINE ENGINES

VARIABLE GEOMETRY ROTATING DETONATION COMBUSTOR

Combustor

HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

Manufacturing thin-walled castings utilizing adaptive machining

NON-AXISYMMETRIC COMBUSTOR FOR IMPROVED DURABILITY

Constant volume combustion chamber with counter rotating shutter valve

LIQUID FUEL LEAK DETECTION SYSTEM AND RELATED METHOD

VEHICLE MICROTURBINE SYSTEM AND METHOD OF OPERATING THE SAME

Retention hardware

GAS TURBINE ENGINE

Combustor liner attachment assembly for gas turbine engine

Dilution/effusion hole pattern for thick combustor panels

Gas turbine including first-stage stator vanes

Additive integral combustor expansion spring

Combustor having honeycomb seal ring

Igniter for gas turbine engine

Premix fuel nozzle for a gas turbine and combustor

Gas turbine engine

Combustor Systems

Gas turbine engine heaters

Combustor nozzle, combustor, and gas turbine

Cooled grommet for a combustor wall assembly

Unitary flow path structure

Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor

Offset cores for gas turbine engines

Gas turbine engine architecture with nested concentric combustor

Airfoil fluid curtain to mitigate or prevent flow path leakage

Flow path assembly with airfoils inserted through flow path boundary

Combustor shell attachment

Non-contact seal with progressive radial stop(s)

Gas turbine engine and combustor having air inlets and pilot burner

Fuel nozzle manifold systems for turbomachines

Radial flow turbine heat engine

Turbine Engine With Rotating Detonation Combustion System

Ultra compact combustor

Methods and features for positioning a flow path inner boundary within a flow path assembly

Seal retention assembly for gas turbine engine

Support ring with fluid flow metering

Co-axial dual swirler nozzle

Burner with variable port area

Involute trapped vortex combustor assembly

Fuel and air injection handling system for a combustor of a rotating detonation engine

Volute trapped vortex combustor assembly

Combustor and gas turbine including the same

Combustor and gas turbine including the same

REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM

Gas turbine engine airfoil

Non-contact seal with progressive radial stop(s)

Parallel combustor configuration for unmanned underwater vehicle propulsion turbine

Non-contact seal assembly for rotational equipment

Metering hole geometry for cooling holes in gas turbine engine

Method and system for controlling a sequential gas turbine engine

Airfoil fluid curtain to mitigate or prevent flow path leakage

System and method for transition piece seal

NON-AXIALLY SYMMETRIC TRANSITION DUCTS FOR COMBUSTORS

Methods for assembling a unitary flow path structure

Methods and features for positioning a flow path inner boundary within a flow path assembly

Flow path assembly with airfoils inserted through flow path boundary

Unitary flow path structure

Unitary flow path structure

Unitary flow path structure

Power generation system and method for activating fuel cell in power generation system

Rotor shaft cooling

Portable jig and fixture for precision machining

Components having channels for impingement cooling

Combustor for rotating detonation engine and method of operating same

Components having separable outer wall plugs for modulated film cooling

Gas turbine engine including a re-heat combustor and a shaft power transfer arrangement for transferring power between low and high pressure shafts

Monolithic superstructure for load path optimization

Turbine

Component assembly for a gas turbine engine

SYSTEMS, APPARATUSES AND METHODS FOR IMPROVED ROTATING DETONATION ENGINES

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

Combustor finger seal

METHOD OF CONTROLLING A GAS TURBINE ASSEMBLY

Slinger combustor having main combustion chamber and sub-combustion chamber, and gas turbine engine system having the same

Transition part assembly and combustor including the same

COpower generation system

INSTALLATION TOOL AND SYSTEM FOR ASSEMBLING A GAS TURBINE COMBUSTOR

HYBRID COMPRESSED AIR ENERGY STORAGE SYSTEM AND PROCESS

Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine

Retention hardware

Diffuser of a thermal energy machine and thermal energy machine

Regulation of the oil flow in a cooling circuit of a turbomachine

GAS TURBINE WITH SEQUENTIAL COMBUSTION ARRANGEMENT

GAS TURBINE ENGINE

COMPRESSOR SECONDARY FLOW AFT CONE COOLING SCHEME

Turboengine, and vane carrier unit for turboengine

Secondary airflow passage for adjusting airflow distortion in gas turbine engine

METHODS AND SYSTEMS FOR MONITORING HEALTH OF A COMBUSTOR

FUEL INJECTOR COVERS AND METHODS OF FABRICATING SAME

Slotted injector for axial fuel staging

Staged fuel and air injection in combustion systems of gas turbines

CONTINUOUS ROTATING DETONATION ENGINES AND ASSOCIATED SYSTEMS AND METHODS

TRANSITION DUCT SYSTEM WITH A ROBUST CONVERGING FLOW JOINT AT AN INTERSECTION BETWEEN ADJACENT TRANSITIONS EXTENDING BETWEEN A COMBUSTOR AND A TURBINE ASSEMBLY IN A GAS TURBINE ENGINE

Gas turbine combuster

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

AXIAL STAGE COMBUSTION SYSTEM WITH EXHAUST GAS RECIRCULATION

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

System for sealing between combustors and turbine of gas turbine engine

Combustor

SYSTEM AND METHOD HAVING ANNULAR FLOW PATH ARCHITECTURE

GASIFICATION APPARATUS WITH SUPERCRITICAL FLUID

Combustor assembly for a turbine engine

System for suppressing acoustic noise within a gas turbine combustor

Combustor cooling system

Combustion engine

Non-contact seal assembly for rotational equipment

Combustor cooling structure

PRE-DIFFUSER WITH HIGH CANT ANGLE

ENGINE JETTING OUT COMBUSTION GAS AS DRIVING FORCE

COMBUSTOR FOR A GAS TURBINE ENGINE

High pressure compressor diffuser for an industrial gas turbine engine

Sequential combustor and method for operating the same

Turbomachine sparkplug fixing assembly

GAS TURBINE ENGINE

Turbine engine with a turbo-compressor

Cooling flow for leading panel in a gas turbine engine combustor

Cooled grommet for a combustor wall assembly

TWO-STAGE COMBUSTOR FOR GAS TURBINE ENGINE

Meter plate for blade outer air seal

SERVICE-FRIENDLY CROSS FLAME TUBE WITH TWIST LOCK ATTACHMENT FOR CAN-ANNULAR GAS TURBINES

METHOD FOR CONTROLLING THE OPERATION OF A GAS TURBINE WITH SEQUENTIAL COMBUSTION

Combustor aft mount assembly

Wave rotors with temperature control features

Automatic control of turbine blade temperature during gas turbine engine operation

GAS TURBINE ENGINE AND TURBINE CONFIGURATIONS

Gas turbine engine airfoil

Exhaust mixer for wave rotor assembly

Method for the monitoring of a degree of coking at seals by a gas generator shaft

Bearing compartment seal

GAS TURBINE COMBUSTOR AND GAS TURBINE ENGINE EQUIPPED WITH SAME

Gas turbine engine wall assembly with support shell contour regions

Hybrid diffuser case for a gas turbine engine combustor

Recuperated gas turbine engine

Systems and methods to respond to grid overfrequency events for a stoichiometric exhaust recirculation gas turbine

Turbine engine with guide vanes forward of its fan blades

Gas turbine engine combustor bulkhead assembly

Geared turbofan engine with low pressure environmental control system for aircraft

Inner diffuser case cone and skirt

DISCOURAGER SEAL FOR A TURBINE ENGINE

METHOD FOR PRODUCING A METAL UNDERCOAT MADE FROM PLATINUM ON A METAL SUBSTRATE

Angled Core Engine

Offset cores for gas turbine engines

Liner retaining feature for a combustor

APPARATUS FOR AN ASSEMBLY TOOL FOR MOUNTING OR DISMANTLING, REPLACEMENT AND MAINTENANCE OF A COMPONENT OF AN ENGINE

Ultra-High Efficiency Gas Turbine (UHEGT) with Stator Internal Combustion

Decoupled gas turbine engine

ENGINE PROPULSION SYSTEM

Joint for sealing a gap between casing segments of an industrial gas turbine engine combustor

Gas turbine engine architecture with nested concentric combustor

GAS TURBINE ENGINE WITH SUPERSONIC COMPRESSOR

Serrated outer surface for vortex initiation within the compressor stage of a gas turbine

Reverse-flow core gas turbine engine with a pulse detonation system

Exhaust liner flange cooling

Annular combustion chamber of a gas turbine and gas turbine with such a combustion chamber

Thermally isolated turbine section for a gas turbine engine

Gas turbine engine airfoil

Combustion turbine with Siamesed wall paired combustor housings

Gas Turbine Engine Core Utilized in Both Commercial and Military Engines

Laser-charged high-speed propulsion system and method for production of high-powered laser

Ultra compact combustor having reduced air flow turns

CONTINUOUS DETONATION WAVE TURBINE ENGINE

Gas turbine engine

Power generation system and method for activating fuel cell in power generation system

Aircraft turbomachine combustion chamber module and method for designing same

Two-circuit injector for a turbine engine combustion chamber

System and method for generating electric energy

Offset core engine architecture

Turbine engine with a combustion chamber outer flange of sandwich type

Combustor with fuel injector pegs for reducing combustion pressure oscillations

System and method for reducing modal coupling of combustion dynamics

SYSTEMS AND METHODS FOR REDUCING MODAL COUPLING OF COMBUSTION DYNAMICS

Gas turbine engine with twin offset gas generators

Assembly for directing combustion gas

Bundled tube fuel injector with outer shroud and outer band connection

COMPRESSOR DISCHARGE CASING ASSEMBLY

Compressor arrangement

Continuous detonation combustion engine and system

Multiple motor gas turbine engine system with auxiliary gas utilization

Gas turbine with sequential combustion arrangement

Inductively coupled plasma arc device

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

Gas turbine engine with a fire wall and an off-take device

METHOD AND SYSTEM FOR AUGMENTING THE DETECTION RELIABILITY OF SECONDARY FLAME DETECTORS IN A GAS TURBINE

Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans

Burner arrangement and method for operating a burner arrangement

INNER BARREL MEMBER WITH INTEGRATED DIFFUSER FOR A GAS TURBOMACHINE

Damper for combustion oscillation damping in a gas turbine

System, method and apparatus for lean combustion with plasma from an electrical arc

Providing oxidation to a gas turbine engine

Slinger combustor

Compressor air provided to combustion chamber plenum and turbine guide vane

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

System, method and apparatus for lean combustion with plasma from an electrical arc

Cogen heat load matching through reheat and capacity match

Turbine engine including a continuous wave detonation chamber and cooling bypass flow and aircraft provided with such a turbine engine

Variable volume combustor with aerodynamic support struts

THE TESLA TWIN TURBINES COMBUSTION ENGINE MODULE

Fuel-cooled bladed rotor of a gas turbine engine

Power generation system and method of stopping power generation system

System and method for reheat in gas turbine with exhaust gas recirculation

Gas turbine centripetal annular combustion chamber and method for flow guidance

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

GAS TURBINE ASYMMETRIC FUEL NOZZLE COMBUSTOR

GAS TURBINE ASYMMETRIC NOZZLE GUIDE VANES

Combustor

COMBUSTOR

GAS TURBINE ENGINE WITH SHORTENED MID SECTION

Gas turbine engine with radial diffuser and shortened mid section

Gas turbine combustion system

Hot EGR driven by turbomachinery

Wave disc engine apparatus

Non-combustion energy source and configuration for brayton cycle heat engines

TANGENTIAL FLOW DUCT WITH FULL ANNULAR EXIT COMPONENT

Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section

Mid-section of a can-annular gas turbine engine to introduce a radial velocity component into an air flow discharged from a compressor of the mid-section

Mid-section of a can-annular gas turbine engine with a cooling system for the transition

Mid-section of a can-annular gas turbine engine with an improved rotation of air flow from the compressor to the turbine

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

Gas turbine engine with supersonic compressor

Radial inflow gas turbine engine with advanced transition duct

Gas turbine engine

Two-stage combustor for gas turbine engine

Full hoop casing for midframe of industrial gas turbine engine

Gas turbine combustion chamber arrangement of axial type of construction

AERO-DERIVATIVE GAS TURBINE ENGINE WITH AN ADVANCED TRANSITION DUCT COMBUSTION ASSEMBLY

Casing for a gas turbine engine

System and method for conditioning a working fluid in a combustor

Gas turbine engine with high and intermediate temperature compressed air zones

Support assembly for transition duct in turbine system

Support assembly for transition duct in turbine system

Corrosion resistant catalysts for decomposition of liquid monopropellants