SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERY

Cooling Nozzle Vanes of a Turbine Engine

TURBINE ENGINE SUPPORT STRUCTURE WITH AIRFLOW PORTS

COMBUSTION MODULE FOR A TURBOMACHINE

BURNER WITH A BILAMINAR COUNTERDIRECTIONAL VORTEX FLOW

Combustion module for a turbomachine

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

Gas turbine engine injector module with thermally coupled fuel lines having respective outlets

FUEL NOZZLE WITH RESTRICTED CORE AIR PASSAGE

TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE

TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE

Reverse flow combustor

Gas turbine engine

Ring assembly for double-skin combustor liner

Involute trapped vortex combustor assembly

Combustor assembly for a turbo machine

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

Systems and methods for establishing message routing paths through a computer network

Inner cooling shroud for transition zone of annular combustor liner

Cooling configurations for combustor attachment features

Reverse flow combustor

Fuel nozzle assembly and gas turbine having the same

Ring-shaped combustion chamber for a turbine engine

Particle-trapping device for a turbomachine and turbomachine with such a device

BURNERS HAVING FUEL PLENUMS

Staged dual fuel radial nozzle with radial liquid fuel distributor

Combustor assemblies for use in turbine engines and methods of assembling same

Small exit duct for a reverse flow combustor with integrated fastening elements

Small exit duct for a reverse flow combustor with integrated cooling elements

Combustor arrangement including flow control vanes

Gas turbine combustion acoustic damping system

Combustor for gas turbine engine

Annular turbomachine combustion chamber

System and method having annular flow path architecture

Apparatus and method for air extraction at a gas turbine engine combustor

AIRCRAFT ENGINE COMPRISING AZIMUTH SETTING OF THE DIFFUSER WITH RESPECT TO THE COMBUSTION CHAMBER

Gas turbine engine combustor and method of forming same

Gas turbine fuel components

Fuel injection locations based on combustor flow path

GAS TURBINE COMBUSTOR

D5/D5A DF-42 integrated exit cone and splash plate

Combustor and gas turbine

Combustion chamber having axially extending and annular coolant manifolds

COMBUSTOR LINER

D5/D5A DF-42 double walled exit cone and splash plate

Liner retaining feature for a combustor

Combustor arrangement with fastening system for combustor parts

Combustor front panel

Combustor cap assembly

Combustor with ring part having protrusions and gas turbine including the combustor

Heat-transfer device and gas turbine combustor with same

Combustor liners with U-shaped cooling channels

MULTI-FUEL TURBINE COMBUSTOR, MULTI-FUEL TURBINE COMPRISING SUCH A COMBUSTOR AND CORRESPONDING METHOD

Gas turbine combustion acoustic damping system

Combustor with fuel injector pegs for reducing combustion pressure oscillations

Liner, flow sleeve and gas turbine combustor each having cooling sleeve

Combustor dome heat shield

Gas turbine combustion liner with triangular heat transfer element

Gas turbine engines having fuel injector shrouds with interior ribs

Cooling structure for gas turbine combustor liner

Combustor heat-shield cooling via integrated channel

Burners having fuel plenums

Flamesheet combustor contoured liner

Asymmetric combustor heat shield panels

Combustor apparatus in a gas turbine engine

Low calorific fuel combustor for gas turbine

Reverse flow ceramic matrix composite combustor

Multi-zone combustor

System for providing a working fluid to a combustor

Flow conditioner in a combustor of a gas turbine engine

Rich burn, quick mix, lean burn combustor

Gas turbine combustor equipped with heat-transfer device

Flow sleeve inlet assembly in a gas turbine engine

Combustor and rotating machine

Combustion arrangement and turbine comprising a damping facility

Combustor and method of supplying fuel to the combustor

Combustor and method of supplying fuel to the combustor

Assemblies and apparatus related to combustor cooling in turbine engines

Reverse-flow annular combustor for reduced emissions

Ducting arrangement for cooling a gas turbine structure

Air management arrangement for a late lean injection combustor system and method of routing an airflow

Flamesheet combustor dome

Variable length combustor dome extension for improved operability

Burner arrangement including an air supply with two flow passages

LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM

Combustor heat shield

System and method for reducing combustion dynamics in a combustor

FUEL NOZZLE ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME

Gas turbine combustor and method for operating same

Micromixer of turbine system

COMBUSTOR ASSEMBLY WITH IMPINGEMENT SLEEVE HOLES AND TURBULATORS

System and method for supplying a working fluid to a combustor

Symmetric fuel injection for turbine combustor

Flowsleeve of a turbomachine component

Combustor of a turbomachine including multiple tubular radial pathways arranged at multiple circumferential and axial locations

Can annular combustion arrangement with flow tripping device

Gas turbine combustor with top hat nozzle arrangements

Combustor having wake air injection

Combustion system having a venturi for reducing wakes in an airflow

ANNULAR FLOW CONDITIONING MEMBER FOR GAS TURBOMACHINE COMBUSTOR ASSEMBLY

Multi-pierced combustion chamber with counter-rotating tangential flows

CONICAL REVERSE-FLOW COMBUSTION CHAMBER FOR A TURBOMACHINE

Gas turbine combustor having counterflow injection mechanism and method of use

Multipoint injectors with auxiliary stage

BURNER FOR STABILIZING THE COMBUSTION OF A GAS TURBINE

Reverse flow combustor duct attachment

TURBOMACHINE COMBUSTORS HAVING DIFFERENT FLOW PATHS

Reverse-flow annular combustor for reduced emissions

Burner system and method for damping such a burner system

Gas turbine engine combustor with lobed, three dimensional contouring

Apparatus and method for cooling a combustor

METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR

Stress reduction feature to improve fuel nozzle sheath durability

Combustor assemblies for use in turbine engines and methods of assembling same

Low calorific value fuel combustion systems for gas turbine engines

Low calorific fuel combustor for gas turbine

SYSTEM FOR DIRECTING AIR FLOW IN A FUEL NOZZLE ASSEMBLY

Ultra low emissions gas turbine combustor

Apparatus and method for cooling a combustor cap

Apparatus and method for cooling a combustor

APPARATUS AND METHOD FOR MIXING FUEL IN A GAS TURBINE NOZZLE

Apparatus and method for mixing fuel in a gas turbine nozzle

Combustor

LIQUID-FUELED PREMIXED REVERSE-FLOW ANNULAR COMBUSTOR FOR A GAS TURBINE ENGINE

Air biasing system in a gas turbine combustor

Method of repairing a gas turbine engine combustor

LOW EMISSION COMBUSTION SYSTEMS AND METHODS FOR GAS TURBINE ENGINES

Angled vanes in combustor flow sleeve

FUEL INJECTION IN SECONDARY FUEL NOZZLE

Combustor assembly for a turbine engine with enhanced cooling

Apparatus for conditioning airflow through a nozzle

Fuel injector and aerodynamic flow device

Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine

COMBUSTOR OF GAS TURBINE

Reverse flow ceramic matrix composite combustor

Combustor assembly and cap for a turbine engine

Combustor liner with integrated anti-rotation and removal feature

GAS TURBINE COMBUSTOR REPAIR USING A MAKE-UP RING

Combustor with improved cooling holes arrangement

Combustor assembly comprising a combustor device, a transition duct and a flow conditioner

Gas turbine engine reverse-flow combustor

Thermal machine

Flow sleeve impingement cooling using a plenum ring

INTEGRATED FUEL NOZZLE IFC

Airflow distribution to a low emissions combustor

Impingement cooled can combustor

Stress reduction feature to improve fuel nozzle sheath durability

Methods and systems to facilitate reducing combustor pressure drops

Turbine engine having folded annular jet combustor

Combustor construction

Combustor heat shield

Noise reducing combustor

Combustor with improved swirl

Method and apparatus for generating combustion products within a gas turbine engine

Optimized configuration of a reverse flow combustion system for a gas turbine engine

Gas turbine engine combustor with improved cooling

Combustor liner v-band design

Combustor

Method of fabricating a combustion chamber

Counterflow injection mechanism having coaxial fuel-air passages

Gas turbine combustor having counterflow injection mechanism

Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engine

Gas turbine engine combustor

Low smoke and emissions fuel nozzle

Gas turbine engine combustor with improved cooling

Exit duct of annular reverse flow combustor and method of making the same

Combustor exit duct

Combustor and method of improving manufacturing accuracy thereof

Combustor having means for directing air into the combustion chamber in a spiral pattern

Combustor heat shield and method of cooling

Stagnation point reverse flow combustor for a combustion system

Stagnation point reverse flow combustor

Lean-staged pyrospin combustor

Method and apparatus for reducing gas turbine engine emissions

Gas turbine combustor sliding joint

Auxiliary power unit having a rotary fuel slinger

Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine

Method and apparatus for reducing gas turbine engine emissions

Gas turbine can annular combustor

Turbine engine having a reverse flow annular vortex combustor

Cooling nozzle vanes of a turbine engine

Combustor with reverse dilution air introduction