COMBUSTOR LINER V-BAND WITH DIRECTED AIR FLOW

COMBUSTION LINER

COMBUSTOR DEFLECTOR ASSEMBLY

Turbine engine combustor having a combustion chamber heat shield

COMBUSTOR DILUTION WITH VORTEX GENERATING TURBULATORS

Combustor deflector assembly

Combustor liner having cooling dispersing member for localized liner cooling

Combustor nozzle, combustor, and gas turbine including same

Unit cell resonator networks for gas turbine combustor tone damping

Combustion liner having a dilution passage

Flange cooling structure for gas turbine engine

Dilution air inlets with notched tip and slotted tail for combustor

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE

ENGINE COMPONENT ASSEMBLY

Panel burn through tolerant shell design

Combustion chamber with particle separator

Combustor bulkhead with circular impingement hole pattern

Impingement cooling with impingement cells on impinged surface

COMBUSTOR LINER PANEL WITH MICRO-CIRCUIT CORE COOLING

Liner cooling structure with reduced pressure losses and gas turbine combustor having same

HGP component with effusion cooling element having coolant swirling chamber

Backside features with intermitted pin fins

Combustor panel stud cooling effusion through heat transfer augmentors

Gas turbine combustor liner with integral chute made by additive manufacturing process

Fin-pin flow guide for efficient transition piece cooling

Turbulator geometry for a combustion liner

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Turbulators for cooling heat shield of a combustor

Combustor quench aperture cooling

Internally cooled dilution hole bosses for gas turbine engine combustors

Combustor heat shield edge cooling

Combustor panel standoff pin

Panel burn through tolerant shell design

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

APPARATUS AND METHOD FOR MITIGATING PARTICULATE ACCUMULATION ON A COMPONENT OF A GAS TURBINE ENGINE

Heat shield panels with overlap joints for a turbine engine combustor

Float wall combustor panels having airflow distribution features

Turbulence generating structure for liner cooling enhancement and gas turbine combustor having the same

Cooling structure with ribs for gas turbine engine

Combustor with particle collection panel having a plurality of particle collection chambers

Duct assembly including helicoidal structure and gas turbine combustor including the same

Float wall combustor panels having airflow distribution features

Engine component with hollow turbulators

Combustor panel standoffs with cooling holes

COMBUSTOR BASKET COOLING RING

Hybrid dimple-and-void auxetic structures with engineered patterns for customized NPR behavior

Combustor pipe, combustor, and gas turbine

Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor

Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor

ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT

Engine component with flow enhancer

Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor

Wall panel assembly for a gas turbine engine

Cooling mechanism of combustion chamber, rocket engine having cooling mechanism, and method of manufacturing cooling mechanism

Engine component assembly

Combustor thermal shield fabrication method

Combustor arrangement including flow control vanes

Staged fuel and air injection in combustion systems of gas turbines

Gas turbine engine wall assembly with enhanced flow architecture

Engine components with impingement cooling features

Fastback turbulator

SINGLE SKIN COMBUSTOR HEAT TRANSFER AUGMENTERS

Single skin combustor with heat transfer enhancement

Cooling apparatus for a fuel injector

Article and method of forming an article

Internally cooled dilution hole bosses for gas turbine engine combustors

Combustor heat shield with carbon avoidance feature

Article and manifold for thermal adjustment of a turbine component

Trapped vortex fuel injector and method for manufacture

Cooling device with small structured rib-dimple hybrid structures

CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGINE COMBUSTOR

Angled impingement inserts with cooling features

Gas turbine engine component cooling circuit with respirating pedestal

Cooling flow for leading panel in a gas turbine engine combustor

Cooling an igniter body of a combustor wall

Combustor panels and configurations for a gas turbine engine

Combustor quench aperture cooling

Turbine engine multi-walled structure with internal cooling element(s)

Turbine engine multi-walled structure with cooling element(s)

Turbine engine combustor heat shield with one or more cooling elements

Passage geometry for gas turbine engine combustor

Heat shield panels with overlap joints for a turbine engine combustor

Combustion chamber having axially extending and annular coolant manifolds

Turbulator structure on combustor liner

Wall for a hot gas channel in a gas turbine

Sealed combustor liner panel for a gas turbine engine

Fuel injector guide(s) for a turbine engine combustor

Cooled wall assembly for a combustor and method of design

Heat transfer pedestals with flow guide features

Impingement film-cooled floatwall with backside feature

Combustor wall aperture body with cooling circuit

Gas turbine engine combustor liner panel

Gas turbine engine combustor liner panel

Gas turbine combustor

Gas turbine system with a transition duct having axially extending cooling channels

Self-cooled orifice structure

Jet burner with cooling duct in the base plate

Gas turbine engine component having shaped pedestals

Annular combustion chamber wall arrangement

Finned ignitor grommet for a gas turbine engine

Heat-transfer device and gas turbine combustor with same

Combustor liners with U-shaped cooling channels

Combustor heat shield for a gas turbine engine

Fastback vorticor pin

Gas turbine engine combustor basket with inverted platefins

Trapped vortex fuel injector and method for manufacture

COMBUSTION CHAMBER WITH COOLING SLEEVE

Combustor with grommet having projecting lip

Interwoven channels for internal cooling of airfoil

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

Process for making a turbulator by additive manufacturing

Combustor dome heat shield

Gas turbine combustion liner with triangular heat transfer element

Hot gas path component with impingement and pedestal cooling

Cooling structure for gas turbine combustor liner

COMBUSTOR OF A GAS TURBINE WITH PRESSURE DROP OPTIMIZED LINER COOLING

Combustor with fuel staggering for flame holding mitigation

Turbine blade

Impingement cooling mechanism, turbine blade and cumbustor

Flow sleeve for a combustion module of a gas turbine

Combustor heat shield with carbon avoidance feature

Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes

Gas turbine combustor equipped with heat-transfer device

System and method for a multi-wall turbine combustor

Ducting arrangement for cooling a gas turbine structure

Cooling for combustor liners with accelerating channels

Gas turbine engine combustor liner

Combustor bulkhead assembly

Systems and methods for suppressing combustion driven pressure fluctuations with a premix combustor having multiple premix times

Near-wall roughness for damping devices reducing pressure oscillations in combustion systems

Combustor liner with improved film cooling

Combustor liner with decreased liner cooling

Combustor liner with reduced cooling dilution openings

Combustor liner with convergent cooling channel

COMBUSTOR ASSEMBLY WITH IMPINGEMENT SLEEVE HOLES AND TURBULATORS

Can annular combustion arrangement with flow tripping device

Combustor and method for supplying flow to a combustor

COMBUSTION CHAMBER HEAD OF A GAS TURBINE WITH COOLING AND DAMPING FUNCTIONS

Distributed cooling for gas turbine engine combustor

Turbomachine combustor assembly including a vortex modification system

Methods and systems for transferring heat from a transition nozzle

COMBUSTION LINER HAVING TURBULATORS

COOLING STRUCTURE, GAS TURBINE COMBUSTOR AND MANUFACTURING METHOD OF COOLING STRUCTURE

Apparatus and method for cooling a combustor

Combustor with fuel staggering for flame holding mitigation

Gas turbine combustor having contraction member on inner wall surface

Apparatus and method for cooling a combustor

Combustor liner assembly with enhanced cooling system

Burner arrangement with deflection elements for deflecting cooling air flow

Cooling arrangement for a turbine component

Mesh cooled conduit for conveying combustion gases

Combustor head plate assembly with impingement

Combustor liner helical cooling apparatus

Angled vanes in combustor flow sleeve

HYBRID VENTURI COOLING SYSTEM

Fuel injection system for a combustion chamber of a turbomachine

Combustor liner for a turbine engine with venturi and air deflector

Turbulated aft-end liner assembly and cooling method

Gas turbine having an improved cooling architecture

Heat exchange bulkhead

Cooling structure for gas turbine combustor

GAS TURBINE ENGINE AND METHOD OF OPERATION

Combustor liner

PATTERN COOLED COMBUSTOR LINER

Flow conditioner for use in gas turbine component in which combustion occurs

TURBULATED AFT-END LINER ASSEMBLY AND RELATED COOLING METHOD

Modular serpentine cooling systems for turbine engine components

Cooled component with a featured surface and related manufacturing method

Gas turbine transition duct

Combustor dynamic attenuation and cooling arrangement

Turbulated aft-end liner assembly and cooling method

Combustor heat shield with variable cooling

Combustor liner and heat shield assembly

Cooling arrangement for a component of a gas turbine engine

Wall elements for gas turbine engine combustors

Tile and exo-skeleton tile structure

Combustion apparatus

Combustor with additively manufactured combustor body having aft frame with heat transfer augmentation