SYSTEM AND METHOD FOR ADAPTIVE IMPINGEMENT COOLING

COMBUSTOR HAVING A PRESSURE FEED

COMBUSTION LINER HAVING TURBULATORS

Injection system for a turbomachine combustion chamber, including air injection means improving the air-fuel mixture

Combustor

Stoichiometric exhaust gas recirculation combustor with extraction port for cooling air

Apparatus and method for cooling a combustor

Thermally isolated wall assembly

System and method for injecting fuel

GAS TURBINE FUEL SYSTEM FOR LOW DYNAMICS

Gas turbine combustion chamber

Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor

Low calorific fuel combustor for gas turbine

SUBSTRATE WITH SHAPED COOLING HOLES AND METHODS OF MANUFACTURE

Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece

Apparatus and method for cooling a combustor

Burner arrangement with deflection elements for deflecting cooling air flow

COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME

Fuel nozzle and assembly and gas turbine comprising the same

Apparatus and filtering systems relating to combustors in combustion turbine engines

Apparatus and filtering systems relating to combustors in combustion turbine engines

Diffuser/rectifier assembly for a turbine engine with corrugated downstream walls

Flame tolerant secondary fuel nozzle

Replaceable orifice for combustion tuning and related method

Method for operating a burner and burner, in particular for a gas turbine

Component having a film cooling hole

Combustor head plate assembly with impingement

Combustor liner cooling at transition duct interface and related method

Method and system for providing a splitter to improve the recovery of compressor discharge casing

IMPINGEMENT STRUCTURES FOR COOLING SYSTEMS

Angled vanes in combustor flow sleeve

Gas turbine combustion device

Combustor liner segment seal member

Combustor liner segment seal member

Gas turbine, method of controlling air supply and computer program product for controlling air supply

Gas turbine, method of controlling air supply and computer program product for controlling air supply

Turbulated aft-end liner assembly and cooling method

Impingement cooling plate for a hot gas duct of a thermal machine

Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement

Integrated Ion Transport Membrane and Combustion Turbine System

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

Cooling arrangement for a combustion chamber

Combustion chamber head of a gas turbine

System and method for cooling a wall of a gas turbine combustor

Turbine air flow conditioner

Anti-flashback features in gas turbine engine combustors

APPARATUS AND METHOD FOR COOLING GAS TURBINE ENGINE COMBUSTORS

Systems and methods for reintroducing gas turbine combustion bypass flow

PATTERN COOLED COMBUSTOR LINER

INJECTION DEVICE FOR A TURBOMACHINE

Burner for a Turbo Machine, Baffle plate for Such a Burner and a Turbo Machine Having Such a Burner

TURBULATED AFT-END LINER ASSEMBLY AND RELATED COOLING METHOD

Modular serpentine cooling systems for turbine engine components

Combustor assembly and cap for a turbine engine

COOLING APPARATUS FOR COMBUSTOR TRANSITION PIECE

COOLING A ONE-PIECE CAN COMBUSTOR AND RELATED METHOD

Ring cooling for a combustion liner and related method

Plasma flow controlled diffuser system

Toroidal boundary layer gas turbine

Method and apparatus for introducing diluent flow into a combustor

METHOD AND APPARATUS OF FUEL NOZZLE DILUENT INTRODUCTION

METERING OF DILUENT FLOW IN COMBUSTOR

Structures with adaptive cooling

Segmented combustor cap

Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor

Casing of a gas turbine engine having a radial spoke with a flow guiding element

Turbomachine with a diffuser

Counter-vortex film cooling hole design

Counter-vortex paired film cooling hole design

Combustor wall with improved cooling

Diffuser having distribution element for providing part-flow

Replaceable orifice for combustion tuning and related method

Re-heat combustor for a gas turbine engine

Airflow distribution to a low emissions combustor

Turbulated aft-end liner assembly and cooling method

Extended impingement cooling device and method

Component having a film cooling hole

Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters

LEAKAGE REDUCING VENTURI FOR DRY LOW NITRIC OXIDES (NOx) COMBUSTORS

Dirt separator for compressor diffuser in gas turbine engine

CHAMBER-BOTTOM BAFFLE, COMBUSTION CHAMBER COMPRISING SAME AND GAS TURBINE ENGINE FITTED THEREWITH

System for reducing combustor dynamics

Gas turbine engine diffuser and combustion chamber and gas turbine engine comprising same

Methods of forming fan-shaped effusion holes in combustors

Airfoil, sleeve, and method for assembling a combustor assembly

Annular combustion chamber for a turbomachine

Wall elements for gas turbine engine components

Chamber endwall, method of producing it, combustion chamber comprising it, and turbine engine equipped therewith

Combustor assembly for gas turbine engine

Methods and system for reducing pressure losses in gas turbine engines

Combustor

Air flow conditioner for a combustor can of a gas turbine engine

Combustor

Combustor

Combustor

Wall elements for gas turbine engine combustors

Gas turbine engine transitions comprising closed cooled transition cooling channels

Gas turbine combustor

Dirt separator for compressor diffuser in gas turbine engine

System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines

Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber

Diffuser for a gas turbine, and gas turbine for power generation

Burner, gas turbine combustor, burner cooling method, and burner modifying method

Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air

Gas turbine, method of controlling air supply and computer program product for controlling air supply

Combi-Supersonic-Adjusting-Nozzle

Diffuser for an annular combustion chamber, in particular for an airplane turbine engine

Aerodynamic trip for a combustion system

Combustor flow sleeve with optimized cooling and airflow distribution

High thrust gas turbine engine with improved core system

Cooling aft end of a combustion liner

Combustion apparatus

Gas turbine combustor and a gas turbine equipped therewith

Extended impingement cooling device and method

Flow sleeve for a low NOx combustor

Methods and apparatus for film cooling gas turbine engine combustors

Cooling jets

Combustor inlet plenum and baffle

CMC component with cooling cavity

Separating airflows within a turbine engine

Apparatus and process for gas turbine air filtration and fuel vaporization

Nozzle set

Acoustic damper for combustor

Dome structure providing a dome-deflector cavity with counter-swirled airflow

Valve with valve member cooling

Tangential annular combustor with premixed fuel and air for use on gas turbine engines

Tangential and flameless annular combustor for use on gas turbine engines

Pistonless, rotary internal combustion engine and associated support systems