OPEN ROTOR NOSE CONE RAM AIR HEAT EXCHANGER WITH EXHAUST OF COOLING AIR THROUGH STATIC STRUCTURE

INTERMEDIATE SHAFT COVER, AND GAS TURBINE PROVIDED WITH SAME

COOLING FLUID GUIDE FOR GAS TURBINE AND GAS TURBINE

BEARING ASSEMBLY HOUSING FOR AN AIRCRAFT PROPULSION SYSTEM

GAS TURBINE ENGINE VANE OUTER DIAMETER PLATFORM INTEGRATED WITH BLADE OUTER AIR SEAL

FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR CONVENTIONAL GAS TURBINE ENGINES

FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR HYBRID ELECTRICS

SUPERCHARGED COMBUSTOR COOLING USING TURBOMACHINERY

INDUCER ASSEMBLY FOR A TURBINE ENGINE

AIR-OIL HEAT EXCHANGER COMPRISING DIVERGENT PARIETAL CHANNELS

CONNECTION STRUCTURE FOR A GENERATOR ASSEMBLY

GAS TURBINE STATIONARY BLADE AND GAS TURBINE

Cooling Nozzle Vanes of a Turbine Engine

HEAT EXCHANGER

METHOD OF RESTORING ALLOY DEPLETION IN AN AIRFOIL AROUND COOLING HOLES

OPEN ROTOR NOSE CONE RAM AIR HEAT EXCHANGER WITH EXHAUST OF COOLING AIR THROUGH STATIC STRUCTURE

TURBINE ENGINE FOR AN AIRCRAFT

GAS TURBINE ENGINE VANE OUTER DIAMETER PLATFORM INTEGRATED WITH BLADE OUTER AIR SEAL

GUIDE VANE ASSEMBLY

TURBOMACHINE COMPRISING AN OUTLET CONE INCORPORATING COMPONENTS COOLED BY CIRCULATION OF A COOLING FLOW

AIRCRAFT

INSTRUMENTED STATOR WITH EXTENDED INTERNAL PASSAGES

GAS TURBINE ENGINE POWER CABLE COOLING

INDUCER ASSEMBLY FOR A TURBINE ENGINE

AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF

TURBINE VANE BAFFLE CHIMNEY

TURBINE ENGINE ELEMENT COMPRISING AT LEAST ONE BLADE OBTAINED BY ADDITIVE MANUFACTURING

Axially offset vane arrays in turbine engine bypass

AIR-HEATED GUIDE VANE WITH TIP HEATING

Device for sealing and reinjecting a bypass flow for a turbine nozzle

Cooling jacket of a hollow blade of a distributor

TWO PIECE HOLLOW-VANE ASSEMBLY JOINED VIA BRAZING

Component for a turbine engine with a cooling hole

AIRFOIL WITH THICK WISHBONE FIBER STRUCTURE

Compressor bleed pressure recovery

BLEED PASSAGE ARRANGEMENT FOR A GAS TURBINE ENGINE SHROUD

System and method for insulating components in an exhaust gas flow from a gas turbine

STRUCTURE OF COOLING TURBINE VANE SHROUD AND MANUFACTURING METHOD THEREOF

Conduit bushing with cellular material

Bleed passage arrangement for a gas turbine engine shroud

PLATFORM FOR STATOR VANE

Guide vanes in a gas turbine engine

AIRFOIL WITH BAFFLE HAVING FLANGE RING AFFIXED TO PLATFORM

Flow guides for internal cooling of a CMC airfoil

Turbine component with heated structure to reduce thermal stress

Turbine engine with TOBI supporting vanes

STATIC FLUID PASSAGEWAYS FOR GAS TURBINE ENGINES HAVING A GRAPHENE PORTION

Connection structure for a generator assembly

Diffuser ring with air manifold

Cooling system for power cables in a gas turbine engine

Turbine nozzle having blading made of ceramic matrix composite through which a metal ventilation circuit passes

Buffer fluid delivery system and method for a shaft seal of a gas turbine engine

Vane forward rail for gas turbine engine assembly

Service tube locking device

TURBINE ENGINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANES SUPPORTED BY RETAINING MEANS AND CORRESPONDING TURBINE ENGINE

Components for gas turbine engines

STATOR PLENUM WITH COLLET SEAL

Inducer assembly for a turbine engine

Intermediate casing for a gas turbine engine

Exhaust frame differential cooling system

Additively manufactured intermediate duct for disposition between a low-pressure compressor and a high-pressure compressor, and corresponding manufacturing method

Aircraft having a single fluid inlet aperture

Turbine engine fan track liner with tip injection air recirculation passage

Ceramic matrix composite turbine vane assembly having minimalistic support spars

FABRICATION OF COOLING HOLES USING LASER MACHINING AND ULTRASONIC MACHINING

Turbomachine hollow blade

Edge detection via window grid normalization

Nozzle blade for a turbine engine, nozzle, turbine engine and method for manufacturing same

FILLING AN AIRCRAFT TURBINE ENGINE LUBRICANT TANK

Two-piece baffle

Turbomachine with device for cooling and pressurising a turbine

System for cooling turbine shaft coupling

Cooling air delivery assembly

Module for turbomachine

HEAT EXCHANGER COMPRISING AN INTER-VANE WALL PROVIDED WITH HOLLOW TURBULENCE GENERATORS

Seal air buffer and oil scupper system and method

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

DEVICE FOR CONNECTING PARTS OF AN AIRCRAFT ENGINE AND METHOD FOR USING SAME

Gas turbine engine with fluid circuit and ejector

Manufacturing methods for multi-lobed cooling holes

Gas turbine engine forward bearing compartment architecture

Vane assembly with integrated nozzle tube

FLOW DIVERTER FOR MID-TURBINE FRAME COOLING AIR DELIVERY

Turbine vane and gas turbine comprising same

Buffer fluid delivery system and method for a shaft seal of a gas turbine engine

Embedded electric machine

Turbine airfoil

HEAT EXCHANGER

Aircraft

Turbine vane, and turbine and gas turbine including the same

Blade for a turbine engine, associated turbine engine distributor and turbine engine

Method for manufacturing an engine component with a cooling duct arrangement and engine component

Turbomachine comprising a heat exchanger in the secondary path

Technique for cooling inner shroud of a gas turbine vane

Component for a turbine engine with a cooling hole

Seal air buffer and oil scupper system and method

CMC vane arc segment with cantilevered spar

Turbofan gas turbine engine

Aircraft with a single fluid inlet aperture

Gas Turbine Nozzle

Turbine engine with metered cooling system

Tube assembly for a gas turbine engine

Connection structure for a generator assembly

Turbine vane and gas turbine including the same

Air turbine starter with primary and secondary air flow paths

Turbofan engine comprising an outlet cone cooled by its secondary flow

GAS TURBINE FACILITY

Turbine rotor and axial flow turbine

Monolithic diffuser and deswirl flow structure for gas turbine engine

Turbine module

Airfoil having internally cooled wall with liner and shell

Housing less front bearing compartment for gas turbine engine

OGV electroformed heat exchangers

System for cooling turbine shaft coupling

Gas turbine engine forward bearing compartment architecture

Method for extracting a foreign body lodged in a high-pressure distributor blade

Turbomachine component for a gas turbine, turbomachine assembly and gas turbine having the same

Inducer assembly for a turbine engine

Impingement insert for a gas turbine engine

Modular casing manifold for cooling fluids of gas turbine engine

METHOD OF CREATING HEAT TRANSFER FEATURES IN HIGH TEMPERATURE ALLOYS

Cooling system for power cables in a gas turbine engine

Aircraft pneumatic system

Engine components with cooling holes having tailored metering and diffuser portions

Thermal management of tail cone mounted generator

Gas turbine engine including squeeze film damper with reservoir

Fluid drain system for an aircraft propulsion system

Device and method for analyzing the surface of parts having cooling fluid openings

Component having a dirt tolerant passage turn

Modular components for gas turbine engines and methods of manufacturing the same

Turbomachine blade comprising an internal fluid flow passage equipped with a plurality of optimally arranged disruptive elements

Heat shield for gas turbine fluid tubes

System and method for transporting lubricant through a vane

Mid-turbine frame for gas turbine engine

Ceramic airfoil with cooling air turn

Oil drainback arrangement for gas turbine engine

Sleeve for oil service tubes

Turbine engine comprising a heat exchanger in the secondary path

Engine with cooling passage circuit extending through blade, seal, and ceramic vane

Multi-flow cooling circuit for gas turbine engine flowpath component

Fire resistance device intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment

Integrated nozzle and diaphragm with optimized internal vane thickness

Methods and apparatuses using cast in core reference features

Gas turbine engine buffer system

Components for gas turbine engines

Tangential onboard injector inlet extender

Modulated turbine component cooling

Routing for electrical communication in gas turbine engines

Turbine engine airfoil

FLUID COOLING SYSTEMS FOR A GAS TURBINE ENGINE

Turbojet engine nacelle including a single movable frame of a cascade thrust reverser and passages of ancillaries

Engine component with set of cooling holes

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Assembly for a turbomachine

Airfoils and core assemblies for gas turbine engines and methods of manufacture

Turbine vane, and turbine and gas turbine including the same

Systems and methods for manufacturing film cooling hole diffuser portion

Cooled cooling air for blade air seal through outer chamber

Servitude passage arm for a turbo machine

Airfoil with baffle showerhead and cooling passage network having aft inlet

Oil pipe assembly

Tandem stators with flow recirculation conduit

Strut dampening assembly and method of making same

Turbine engine component and method of cooling

Diffuser case mixing chamber for a turbine engine

Airfoil having internal hybrid cooling cavities

Gas turbine engine with feed pipe for bearing housing

Coolant channel

Trailing edge pressure and flow regulator

Turbine exhaust case cooling

TURBINE VANE ASSEMBLY WITH COOLING FEATURE

Turbine blade and gas turbine

Fluid transfer assembly for rotational equipment

Feather seals with leakage metering

Method and device for adjusting the clearance between a rotor and a concentric stator of an aircraft turbine engine

Coverage cooling holes

Tie rod for a mid-turbine frame

Diffuser case support structure

Multiple injector holes for gas turbine engine vane

Wall of a hot gas component and hot gas component comprising a wall

Cooling circuit for gas turbine engine component

Device for holding a cooling tube for a turbomachine casing

Gas turbine engine forward bearing compartment architecture

Beveled coverplate

Air-film cooled component for a gas turbine engine

Method and apparatus for supplying cooling air to a turbine

Ceramic matrix composite component cooling

Article having cooling passage network with inter-row sub-passages

Dual-walled components for a gas turbine engine

Airfoil with baffle having flange ring affixed to platform

Turbine airfoil with multiple walls and internal thermal barrier coating

Gas turbine engine

Gas turbine engine and cooling air configuration for turbine section thereof

CUSTOMER BLEED AIR PRESSURE LOSS REDUCTION

Vane platform leading edge recessed pocket with cover

TURBINE EXHAUST STRUCTURE FOR A GAS TURBINE ENGINE

Airfoil leading edge cooling channels

Oil supply assembly for gas turbine engine

Steam turbine

ADDITIVE MANUFACTURING METHOD FOR THE ADDITION OF FEATURES WITHIN COOLING HOLES

Gas turbine engine with dove-tailed TOBI vane

Cooling hole with shaped meter

Dual-wall airfoil with leading edge cooling slot

Airfoil core inlets in a rotating vane

Airfoil with dual profile leading end

Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojet

Turbine distributor sector for an aircraft turbine engine

Sealing configuration to reduce air leakage

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

COOLING HOLE FOR A GAS TURBINE ENGINE COMPONENT

Gas turbine

Cooling structure for turbine airfoil

Cooling structure for turbine airfoil

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Turbine vane assembly with ceramic matrix composite components

Platform cooling arrangement for a gas turbine engine

Shroud for gas turbine engine

Shroud for gas turbine engine

Method for controlling a turbomachine valve

Shroud and seal for gas turbine engine

TURBINE STATOR VANE WITH MULTIPLE OUTER DIAMETER PRESSURE FEEDS

Downstream turbine vane cooling for a gas turbine engine

Structure for cooling turbine blade

Multiple source impingement baffles for gas turbine engine components

Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved design

Spiral cavities for gas turbine engine components

Seal assembly with shield for gas turbine engines

Mid-turbine frame assembly

Tank assembly

Turbine vane having improved flexibility

Gas turbine engine case including bearing compartment

Bearing support assembly

Coolant airflow assembly particulate filter with panels in series

Case for gas turbine engine

Heat shield, systems and methods

METHODS AND APPARATUSES USING CAST IN CORE REFERENCE FEATURES

Integral turbine center frame

Outlet guide vane for turbomachine, made from several parts assembled together by attachment means outside the flow stream

Vane airfoil cooling air communication

Tail bearing housing

Hybrid cooling schemes for airfoils of gas turbine engines

TURBINE ENGINE SHROUD

Lubricated enclosure for an aircraft turbine engine, limiting the retention of lubricant during pitching

Turbine vane assembly and gas turbine including the same

Turbine rotor coolant supply system

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

Double wall turbine gas turbine engine vane platform cooling configuration with baffle impingement

Heat dissipation system for electric aircraft engine

Gas turbine engine thermal management system

Lightweight tierod

Airflow deflector and assembly

Gas turbine engine components having internal cooling features

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

Turbine module for a turbomachine

FAN DRIVE GEAR SYSTEM MANIFOLD RADIAL TUBE FILTERS

Gas turbine with separate cooling for turbine and exhaust casing

Outlet guide vane for aircraft turbomachine, comprising a lubricant cooling passage equipped with flow disturbance studs

Double wall turbine gas turbine engine vane with discrete opposing skin core cooling configuration

Cooling hole for a gas turbine engine component

Flow channel for a turbomachine

Vane air inlet with fillet

Fluid collection gutter for a geared turbine engine

Flow channel for a turbomachine

Shroud for a gas turbine engine

Pylon of a propulsion unit

OGV electroformed heat exchangers

Igniter cable conduit for gas turbine engine

Gas turbine engine having a flow-conducting assembly formed of nozzles to direct a cooling medium onto a surface

Wick structures for heat pipe-based cooling

Guide vane having a connecting tube

Sump housing for a gas turbine engine

Film cooling hole arrangement for gas turbine engine component

Aft frame assembly for gas turbine transition piece

AFT frame assembly for gas turbine transition piece

ENGINE COMPONENT

Conduit with damping fingers

Trip strip and film cooling hole for gas turbine engine component

METHOD FOR DETERMINING A LOCAL HOT GAS TEMPERATURE IN A HOT GAS DUCT, AND DEVICES FOR CARRYING OUT THE METHOD

Airfoil having internal hybrid cooling cavities

Airfoil having internal hybrid cooling cavities

Airfoil having internal hybrid cooling cavities

Airfoil having internal hybrid cooling cavities

Airfoil having fluidly connected hybrid cavities

ADDITIVE MANUFACTURING BAFFLES, COVERS, AND DIES

Seal assembly for a static structure of a gas turbine engine

Turbine frame assembly for gas turbine engines

Turbine vane having impingement plate for gas turbine and gas turbine including the same

Turbine vane, turbine, and gas turbine including the same

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

Outlet guide vane for turbomachine, comprising a lubricant cooling passage equipped with a thermal conducting matrix compressed between the intrados and extrados walls

Vane assembly for a gas turbine engine

Intersector sealing tab for an aircraft turbine engine

Turbine vane cluster including enhanced vane cooling

COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLE

Component for a turbine engine with a cooling hole

High thermal response exhaust diffuser strut collar

Segmented conduit with airfoil geometry

Damped fluid transfer tube for a gas turbine engine

Variable area turbine arrangement with secondary flow modulation

Engine component with hollow turbulators