SYSTEMS AND METHODS FOR FACILITATING SUBSTANTIALLY UNIFORM VENTILATION AIRFLOW INSIDE AN ENGINE ENCLOSURE OF A GAS TURBINE ENGINE

Three-dimensional printing process, swirling device and thermal management process

Turbine blade with sectioned pins

Augmented cooling system

Cooled wall

Pin-fin array

Method and apparatus for cooling gas turbine and rotor blades

Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly

Turbine blade

Impingement cooling mechanism, turbine blade and cumbustor

Impingement cooling mechanism, turbine blade and combustor

Dust mitigation for turbine blade tip turns

Turbine blade

Method of mixing between a primary flow and a secondary flow in a turbine engine, corresponding device and turbine engine

Gas turbine combustor equipped with heat-transfer device

Film-cooled turbine blade for a turbomachine

Fluid mixer and heat exchange system using same

Trailing edge and tip cooling

Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles

Airfoil with variable trip strip height

Internally cooled gas turbine engine airfoil

Turbine blade of a gas turbine with swirl-generating element and method for its manufacture

Flow inducer for a gas turbine system

Gas turbine engine airfoil cooling circuit arrangement

Gas turbine engine airfoil internal cooling features

Trailing edge cooling configuration for a gas turbine engine airfoil

Cooled blade for a gas turbine

Plate-like air-cooled engine surface cooler with fluid channel and varying fin geometry

Airfoil cooling circuits

Blade outer air seal with cored passages

TURBINE COOLING APPARATUS

Mixing element for gas turbine units with flue gas recirculation

Airfoil cooling enhancement and method of making the same

Trailing edge cooling

Gas turbine engine airfoil cooling circuit

Surface area augmentation of hot-section turbomachine component

Gas turbine engine component with converging/diverging cooling passage

Compressor and a turbine engine with optimized efficiency

Air fuel premixer having arrayed mixing vanes for gas turbine combustor

Gas turbine engine component having wavy cooling channels with pedestals

Methods and systems for use in regulating a temperature of components

PIN-FIN ARRAY

Turbine blade cooling system with bifurcated mid-chord cooling chamber

TURBINE AIRFOIL AND METHOD OF CONTROLLING A TEMPERATURE OF A TURBINE AIRFOIL

Blade or vane for a turbomachine

FLOW EVACUATION SYSTEM FOR AN AIRCRAFT ENGINE

TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING

Serpentine cooling circuit with T-shaped partitions in a turbine airfoil

Integrated axial and tangential serpentine cooling circuit in a turbine airfoil

Cooling system having reduced mass pin fins for components in a gas turbine engine

Platform with cooling circuit

Cooled turbine blades for a gas-turbine engine

Turbine blade tip with vortex generators

Endwall component for a turbine stage of a gas turbine engine

Turbine component cooling channel mesh with intersection chambers

TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY OF IMPINGEMENT NOZZLES

Turbine blade platform cooling systems

Combustor liner assembly with enhanced cooling system

COMBUSTOR TRANSITION PIECE WITH DILUTION SLEEVES AND RELATED METHOD

Cooled blade for a gas turbine

Gas turbine

Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine

Cooled blade for a gas turbine, method for producing such a blade, and gas turbine having such a blade

Interior cooling channels

Airfoil cooling hole flag region

Aircraft gas turbine engine

Turbine vane for a gas turbine and casting core for the production of such

Heat transfer enhancement in internal cavities of turbine engine airfoils

RECUPERATOR FOR GAS TURBINE ENGINES

Gas turbine having an improved cooling architecture

Stator blade for a gas turbine and gas turbine having same

Blade for a gas turbine

Compound cooling flow turbulator for turbine component

Turbine Airfoil Cooling System with Pin Fin Cooling Chambers

Cooling structure of turbine airfoil

Heat transfer passage

Cooling arrangements

High pressure single crystal turbine blade tip repair with laser cladding

Microcircuit cooling for blades

Film-cooling augmentation device and turbine airfoil incorporating the same

Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil

WALL OF A ROCKET ENGINE

Combustion chamber comprising a cooling unit and method for producing said combustion chamber

Blade cooling structure of gas turbine

Turbomachine

Heat transfer augmentation in a compact heat exchanger pedestal array

Gas turbine engine with fluid mixing arrangement

Cavity ventilation

Heat exchanging hollow passages with helicoidal grooves

Castings, casting cores, and methods

Cooling arrangement

Methods and apparatus involving shroud cooling

Arrangement for a gas turbine engine

Trailing edge cooling for turbine blade airfoil

SYSTEM AND METHOD FOR GENERATING MODULATED PULSED FLOW

Gas turbine engine component having dual flow passage cooling chamber formed by single core

Gas turbine engine assemblies with vortex suppression and cooling film replenishment

COOLED AIRFOIL AND METHOD FOR MAKING AN AIRFOIL HAVING REDUCED TRAIL EDGE SLOT FLOW

Impingement cooling arrangement

Fastener assembly with cyclone cooling

Counter-vortex film cooling hole design

Counter-vortex paired film cooling hole design

Cooled Turbine Rotor Blade

Airfoil for nozzle and a method of forming the machined contoured passage therein

Blade for a gas turbine

Blades for gas turbine engines

Apparatus and method for a gas turbine entrainment system

TURBINE AIRFOIL CASTING METHOD

Dust hole dome blade

Cooling structure

Turbine blade tip cooling system

Air sealing element

Advanced turbulator arrangements for microcircuits

Component to be arranged in the flow channel of a turbomachine and spraying method for producing the coating

Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method

Gas turbine component with reduced cooling air requirement

Nozzles for use with gasifiers and methods of assembling the same

Angled tripped airfoil peanut cavity

TURBINE BLADE WITH INTERNAL COOLING STRUCTURE

Cooled turbine blade for a gas turbine and use of such a turbine blade

Impingement cooled structure

Airfoil with improved cooling slot arrangement

Method and apparatus to facilitate cooling turbine engines

Enhanced turbine airfoil cooling

Vane wheel of turbine comprising a vane and at least one cooling channel

COOLANT FLOW SWIRLER FOR A ROCKET ENGINE

Local indented trailing edge heat transfer devices

Turbine blade trip strip orientation

Cooling arrangement for a tapered turbine blade

Airfoil cooling with staggered refractory metal core microcircuits

Core for use in a casting mould

Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade

Refractory metal core main body trench

Turbine airfoil cooling system with spanwise equalizer rib

Turbine component with tip flagged pedestal cooling

Turbine airfoil with submerged endwall cooling channel

Cooling arrangement for a component of a gas turbine engine

High effectiveness cooled turbine blade

Turbine airfoil cooling system with near wall vortex cooling chambers

Leading edge cooling using chevron trip strips

Leading edge cooling using wrapped staggered-chevron trip strips

Turbine airfoil with integral chordal support ribs

Gas turbine engine component suction side trailing edge cooling scheme

Turbine element

Manufacturable and inspectable microcircuits

Advanced turbulator arrangements for microcircuits

Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages

Turbine blade with radial cooling channels

Turbine airfoil with improved cooling

Turbomachine blade with fluidically cooled shroud

Turbine airfoil with counter-flow serpentine channels

Air deflector for a cooling circuit for a gas turbine blade

Manufacturable and inspectable microcircuit cooling for blades

Turbine blade including revised trailing edge cooling

Combustion chamber comprising a cooling unit and method for producing said combustion chamber

Cooled component of a fluid-flow machine, method of casting a cooled component, and a gas turbine

Turbine bucket tip cap

Turbine component

Bipedal damper turbine blade

Turbine airfoil with integrated impingement and serpentine cooling circuit

Gas turbine moving blade having a platform, a method of forming the moving blade, a sealing plate, and a gas turbine having these elements

Turbulator on the underside of a turbine blade tip turn and related method

Device for effecting heat transfer to rotating equipment, in particular gas turbines

Airfoil trailing edge cooling

Heat transfer enhancement features for a tubular wall combustion chamber

Gas turbine stationary blade

Vortex dissipation device for a cooling system within a turbine blade of a turbine engine

Blade outer seal with micro axial flow cooling system

Method for providing turbulation on the inner surface of holes in an article, and related articles

Methods and apparatus for maintaining rotor assembly tip clearances

Aspherical dimples for heat transfer surfaces and method

Airfoil with large fillet and micro-circuit cooling

Heat transfer augmentation in a compact heat exchanger pedestal array

Vortex cooling system for a turbine blade

Combustor cooling with angled segmented surfaces

Drillable super blades

Cooled rotor blade

Cooled turbine airfoil

Turbine nozzle trailing edge cooling configuration

Turbulator on the underside of a turbine blade tip turn and related method

Turbulated hole configurations for turbine blades

Tailored turbulation for turbine blades

Gas turbine stationary blade

Airfoil with shaped trailing edge pedestals

Airfoil cooling holes

Component and turbine assembly with film cooling

Hot gas path component with mesh and impingement cooling

Hot gas path component with mesh and dimpled cooling

Hot gas path component with mesh and turbulated cooling

Spanwisely variable density pedestal array

Gas turbine vane with integral cooling flow control system

Split flow turbine nozzle

Microcircuit cooling for a turbine airfoil

Cooling system for a turbine blade

Turbine bucket airfoil cooling hole location, style and configuration

Microcircuit cooling for a turbine blade

Cooling circuits for a gas turbine blade

Asonic aerospike engine

High blowing ratio high effectiveness film cooling configurations

Rim seal arrangement having pumping feature

Shaped recess flow control