TURBINE BLADE, IN PARTICULAR FOR A GAS TURBINE ENGINE

HEAT EXCHANGER FOR A GAS TURBINE ENGINE

TURBINE ENGINE FOR AN AIRCRAFT

TURBOMACHINE VANE PROVIDED WITH A COOLING CIRCUIT AND METHOD FOR LOST-WAX MANUFACTURING OF SUCH A VANE

Turbine blade and gas turbine

TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

COOLING PASSAGE EXIT OPENING CROSS-SECTIONAL AREA REDUCTION FOR TURBINE SYSTEM COMPONENT

Turbine engine having a compressor with an inducer

PLATFORM FOR STATOR VANE

Guide vanes in a gas turbine engine

Turbine engine combustor having a combustion chamber heat shield

Turbine blade and gas turbine

COOLING ASSEMBLY FOR A TURBINE ASSEMBLY

Cooling passage exit opening cross-sectional area reduction for turbine system component

Heat exchanger for a gas turbine engine

Combustor nozzle, combustor, and gas turbine including same

Ceramic matrix composite airfoil with heat transfer augmentation

Blade intake

Cooling air delivery assembly

TURBINE COMPONENT WITH A THIN INTERIOR PARTITION

Radial turbine rotor with complex cooling channels and method of making same

Heat exchanger comprising a baffle wall with hollow turbulence generators

Turbine airfoil and turbine including same

Blade component, method for manufacture of same, and gas turbine

De-icing device for an air intake of an aircraft turbojet engine nacelle

ENGINE COMPONENT ASSEMBLY

Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air

Turbine shroud cooling

Turbine blades including aero-brake features and methods for using the same

Inserts for airfoils of gas turbine engines

Airfoil tip pocket with augmentation features

Method, system and apparatus for reducing fluid drag

Cooling assembly for a turbine assembly

Gas turbine engine components having interlaced trip strip arrays

Modular casing manifold for cooling fluids of gas turbine engine

Turbine vane with dust tolerant cooling system

Turbine vane with dust tolerant cooling system

Cooling assembly for a turbine assembly

Device for cooling a component of a gas turbine/turbo machine by means of impingement cooling

Turbine component with dust tolerant cooling system

Fuel injector and gas turbine

Turbine blade and gas turbine

Engine component with set of cooling holes

Turbine blade with dust tolerant cooling system

Boas flow directing arrangement

Gas turbine engines with improved airfoil dust removal

Turbomachine blade with trailing edge having improved cooling

A TURBOMACHINE BLADE OR VANE HAVING A VORTEX GENERATING ELEMENT

Assembly for particle removal

Airfoil tip pocket with augmentation features

Trailing edge pressure and flow regulator

Film-cooled multi-walled structure with one or more indentations

APPARATUS AND METHOD FOR USING PLASMA TO ASSIST WITH THE COMBUSTION OF FUEL

Turbine engine component and method of cooling

Ceramic matrix composite component cooling

Turbine engine component including an axially aligned skin core passage interrupted by a pedestal

Impingement cooling for a gas turbine engine component

TURBINE BLADE

Vane platform leading edge recessed pocket with cover

Turbine blade including pin-fin array

Internally cooled airfoil

Turbine engine with annular cavity

Airfoil leading edge cooling channels

Cooling hole with shaped meter

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Airfoil cooling circuits

Turbine blade cooling system with channel transition

Splayed tip features for gas turbine engine airfoil

Cooling structure for turbine airfoil

Turbine blade with dust tolerant cooling system

Turbine vane with dust tolerant cooling system

Leading edge hybrid cavities for airfoils of gas turbine engine

Cooling structure for turbine airfoil

Airfoil with leading edge convective cooling system

GAS TURBINE ENGINE COMPONENT COOLING CAVITY WITH VORTEX PROMOTING FEATURES

Engine component

Cooling circuit with shaped cooling pins

Article having ceramic wall with flow turbulators

Trip strips for augmented boundary layer mixing

Trip strip configuration for gaspath component in a gas turbine engine

Turbomachine blade with optimised cooling

Variably skewed trip strips in internally cooled components

Cooling System

Platform cooling core for a gas turbine engine rotor blade

Trailing edge cooling for a turbine blade

Turbine component with a thin interior partition

Turbine airfoils with micro cooling features

Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air

Hybrid cooling schemes for airfoils of gas turbine engines

ENGINE COMPONENT WITH SET OF COOLING HOLES

Segregated cooling air passages for turbine vane

Gas turbine engine components having internal hybrid cooling cavities

Double wall turbine gas turbine engine vane platform cooling configuration with main core resupply

Chevron trip strip

Flow control in modulated air systems

Turbine blade cooling system with tip flag transition

Turbine blade cooling system with tip diffuser

Turbine blade cooling system with lower turning vane bank

Turbine blade cooling system with upper turning vane bank

Turbine component with rail coolant directing chamber

Double wall turbine gas turbine engine blade cooling configuration

Double wall turbine gas turbine engine blade cooling configuration

Double wall turbine gas turbine engine blade cooling configuration

Double wall turbine gas turbine engine blade cooling configuration

Gas turbine engines with improved airfoil dust removal

Modified J type cantilevered vane and gas turbine having the same

Film cooling hole arrangement for gas turbine engine component

Metal trailing edge for laminated CMC turbine vanes and blades

Cooling structure with ribs for gas turbine engine

Trip strip and film cooling hole for gas turbine engine component

Turbine airfoil with internal cooling channels having flow splitter feature

AIRFOIL HAVING INTERNAL HYBRID COOLING CAVITIES

Airfoil having internal hybrid cooling cavities

Airfoil having internal hybrid cooling cavities

Turbine airfoil with turbulating feature on a cold wall

Swirling flow eductor system and method

Gas turbine blade

Airfoil having forward flowing serpentine flow

Airfoil having forward flowing serpentine flow

Engine component with non-uniform chevron pins

Engine component with hollow turbulators

Airfoil edge cooling channels

COMBUSTION CHAMBER AND A COMBUSTION CHAMBER FUEL INJECTOR SEAL

Turbomachine airfoil

Cooling configuration for a gas turbine engine airfoil

Welding process with an arc welder and beam welder for a weld turbulator

Passive flow modulation of cooling flow into a cavity

Turbomachine blade cooling structure and related methods

Air bearing and thermal management nozzle arrangement for interdigitated turbine engine

Impingement insert

Turbine vane and gas turbine including the same

Engine component with flow enhancer

Turbine engine airfoil having a cooling circuit

Turbine component with shaped cooling pins

Blockage-resistant vane impingement tubes and turbine nozzles containing the same

Airfoil tip pocket with augmentation features

Turbine blades and gas turbine having the same

Turbine airfoil with trailing edge cooling featuring axial partition walls

Actively cooled component

Combustor pipe, combustor, and gas turbine

METHOD OF CONVERTING THE ENERGY OF A GASEOUS WORKING FLUID AND APPARATUS FOR THE IMPLEMENTATION THEREOF

Gas turbine engine component with flow separating rib

Gas turbine ring segment having serially connected cooling holes and gas turbine including the same

Turbomachine Blade Cooling Cavity

TURBINE ENGINE WITH AN EXTENSION INTO A BUFFER CAVITY

Trailing edge pressure and flow regulator

Nacelle inner lip skin with heat transfer augmentation features

Exhaust stream mixer

ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT

Platform cooling core for a gas turbine engine rotor blade

Cooling structure for vane

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Turbine blade and gas turbine

Turbine assembly

Article having ceramic wall with flow turbulators

Airfoil cooling circuits

Additively manufactured component for a gas powered turbine

Dual walled component for a gas turbine engine

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

Engine component with porous section

Systems for removing heat from turbine components

Assembly for a gas turbine engine

Cooling hole with shaped meter

TURBINE AIRFOIL COOLING SYSTEM WITH CHORDWISE EXTENDING SQUEALER TIP COOLING CHANNEL

Ceramic matrix composite component cooling

Cooling passage for gas turbine rotor blade

Rocket propulsion system and method for operating a rocket propulsion system

Method for operating a rocket propulsion system and rocket propulsion system

Engine component assembly

AIRFLOW MANIPULATION DEVICE FOR COMPRESSOR

Turbomachine including clearance control system

Airfoil with variable slot decoupling

COMPRESSOR SECONDARY FLOW AFT CONE COOLING SCHEME

Thermal lifting member for blade outer air seal support

Apparatus, turbine nozzle and turbine shroud

Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil

Airfoil

System and method for mixing tempering air with flue gas for hot SCR catalyst

Apparatus, turbine nozzle and turbine shroud

Cooled turbine vane platform comprising forward, midchord and aft cooling chambers in the platform

Air shredder insert

Airfoil having impingement openings

Accelerator insert for a gas turbine engine airfoil

Airfoil for a gas turbine engine

Chevron trip strip

Core component having toroidal structures

Flow exchange baffle insert for a gas turbine engine component

PASSIVE FLOW MODULATION OF COOLING FLOW INTO A CAVITY

Turbine blade comprising a central cooling duct and two side cavities connected downstream from the central duct

Gas turbine engine airfoil cooling circuit arrangement

Turbine airfoil with trailing edge cooling circuit

Article and method of forming an article

Engine component with film cooling

Gas turbine engine wall assembly with enhanced flow architecture

Baffle insert for a gas turbine engine component and method of cooling

Baffle insert for a gas turbine engine component and component with baffle insert

Baffle insert for a gas turbine engine component

Gas turbine engine component with a baffle insert

Trailing edge cooling for a turbine blade

Turbine blade with sectioned pins and method of making same

Engine component with film cooling

COOLING STRUCTURE AND GAS TURBINE

Cooled turbine runner, in particular for an aircraft engine

Cooling of turbine blades and method for turbine blade manufacture

Foreign substance removal apparatus for gas turbine

Fastback turbulator

Injector nozzle configuration for swirl anti-icing system

System and method for creating a fluidic barrier with vortices from the upstream splitter

Turbine band anti-chording flanges

Using inserts to balance heat transfer and stress in high temperature alloys

Integrated circuit cooled turbine blade

Cooling channels for gas turbine engine component

Article and manifold for thermal adjustment of a turbine component

Gas turbine cooling systems and methods

Cooling structure for hot-gas path components with methods of fabrication

Gas turbine

Article, airfoil component and method for forming article

Cooling device with small structured rib-dimple hybrid structures

Turbine airfoils with micro cooling features

METHOD FOR COOLING A TURBO-ENGINE COMPONENT AND TURBO-ENGINE COMPONENT

Turbine with cooled turbine guide vanes

TURBINE ROTORS INCLUDING TURBINE BLADES HAVING TURBULATOR-COOLED TIP POCKETS

Gas turbine engine component platform cooling

Rotor heat shield

Flow inducer for a gas turbine system

Angled impingement inserts with cooling features

Turbine bucket cooling

Turbine engine component including an axially aligned skin core passage interrupted by a pedestal

Blade outer air seal cooling passage

Turbine airfoil turbulator arrangement

Gas turbine engine component cooling cavity with vortex promoting features

Asymmetric diffuser opening for film cooling holes

Gas turbine engine component cooling passage turbulator

Film cooled multi-walled structure with one or more indentations

Internally cooled gas turbine engine airfoil

Integral metering feature, systems and methods

Gas turbine engine airfoil cooling configuration with pressure gradient separators

Gas turbine engine component with vascular cooling scheme

Exhaust mixer for wave rotor assembly

Trip strip restagger

Rotating turbine vane bearing cooling

Gas turbine engine with disk having periphery with protrusions

Hot part of gas turbine, gas turbine including the same, and manufacturing method of hot part of gas turbine

Turbulator structure on combustor liner

Cooling passages for a mid-turbine frame

GAS TURBINE ENGINE AIRFOIL TURBULATOR FOR AIRFOIL CREEP RESISTANCE

Gas turbine engine airfoil crossover and pedestal rib cooling arrangement

AIRFOIL FOR A TURBINE ENGINE

Engine component

Shroud assembly for a turbine engine

Engine component having platform with passageway

TURBINE BLADE HAVING HEAT SINKS THAT HAVE THE SHAPE OF AN AEROFOIL PROFILE

Gas turbine engine component with converging/diverging cooling passage

Leading edge cooling channel for airfoil

COOLING FOR TURBINE BLADE PLATFORM-AEROFOIL JOINTS

SHROUD ASSEMBLY FOR A TURBINE ENGINE

Turbine blade cooling structure

Film hole with protruding flow accumulator

Gas turbine engine combustor liner panel

Gas turbine engine component having trip strips

Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling

Internal cooling of engine components

Turbine blades and methods of forming turbine blades having lifted rib turbulator structures

Gas turbine engine airfoil cooling passage turbulator pedestal

Splayed tip features for gas turbine engine airfoil

Article and process for producing an article

Engine mid-turbine frame transfer tube for low pressure turbine case cooling

Airfoil cooling apparatus

Gas turbine engine component having shaped pedestals

Gas turbine engine component cooling with interleaved facing trip strips

Gas turbine engine component having curved turbulator

Rotor and gas turbine engine including same

Impingement cooled wall arrangement

Combustor liners with U-shaped cooling channels

Fastback vorticor pin

Rotor blade cooling

Airfoil cooling device and method of manufacture

Airfoil tip pocket with augmentation features

Gas turbine engine component arrangement

Method of reducing manufacturing variation related to blocked cooling holes

Blade outer air seal with cored passages

Gas turbine engine turbine vane platform cooling

Baffle with flow augmentation feature

Turbine blade having swirling cooling channel and cooling method thereof

Structural configurations and cooling circuits in turbine blades

Turbine airfoil with an internal cooling system having trip strips with reduced pressure drop

Structural configurations and cooling circuits in turbine blades

Structural configurations and cooling circuits in turbine blades

Flow outlet

Rotor blade and guide vane airfoil for a gas turbine engine

Exhaust stream mixer

Multi-orifice plate for cooling flow control in vane cooling passage

Cooling configuration for a gas turbine engine airfoil

Cooled airfoil trailing edge and method of cooling the airfoil trailing edge

Gas turbine blade

Gas turbine combustion liner with triangular heat transfer element

Coolant bridging line for a gas turbine, which coolant bridging line can be inserted into a hollow, cooled turbine blade

Thermal management article and method of forming the same, and method of thermal management of a substrate

Internally cooled airfoil

Internally cooled airfoil