THERMOPHOTOVOLTAIC ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

AIRFOIL, TURBINE BLADE INCLUDING THE AIRFOIL, AND GAS TURBINE INCLUDING THE TURBINE BLADE

Skin Passageway Trip Strips

Turbine Blade And Gas Turbine Including Same

TURBINE VANE FOR A GAS TURBINE ENGINE

INTERNALLY DIFFUSING HEAT EXCHANGER FOR A GAS TURBINE ENGINE

HEAT-EXCHANGING PARTITION WALL

HEAT EXCHANGER WITH CURVED CORE AREA AND INTENDED FOR USE WITH AN AGRICULTURAL PUMPER TRUCK

TURBINE VANE FOR A GAS TURBINE ENGINE

Matrix for an Air-Oil Heat Exchanger of a Jet Engine

System and Method of Air-Augmented Gas turbine Turbojet Engines

TURBINE COMPONENT HAVING AIR-JET COOLING STRUCTURE, AND GAS TURBINE INCLUDING SAME

TURBINE COMPONENT HAVING PIN-FIN COOLING STRUCTURE, AND GAS TURBINE INCLUDING SAME

TURBINE BLADE WITH BOOMERANG SHAPED WALL COOLING PASSAGES

INJECTOR HEAD FOR FUEL INJECTOR

TURBINE ENGINE FOR AN AIRCRAFT

Turbine blade with boomerang shaped wall cooling passages

REINFORCED FILM FLOATWALL FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT

ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM

Skin passageway trip strips

THERMAL MANAGEMENT SYSTEM

BEAD PROTRUSIONS HEAT TRANSFER SURFACE STRUCTURE OF FLUID CONDUITS AND MANIFOLDS

TANDEM SEAL PUMP

HEAT EXCHANGER SYSTEMS AND DEVICES FOR INCREASED DURABILITY

Method for Manufacturing Heat Exchanger and Heat Exchanger

Method and apparatus for constructing a ringed airfoil

AIRFOIL WITH RIBS DEFINING SHAPED COOLING CHANNEL

Heat Exchanger With Curved Core Area And Intended For Use With An Agricultural Pumper Truck

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

Fluid ducts including a rib

AIRFOIL FOR A TURBINE ENGINE

BEARING CHAMBER WITH THERMAL HEAT EXCHANGE FINS

BEARING CHAMBER WITH MAPPED THERMAL HEAT EXCHANGE FINS

COOLING SCHEMES FOR AIRFOILS FOR GAS TURBINE ENGINES

Internally cooled turbine blade

PLATFORM FOR STATOR VANE

ASYMMETRIC HEAT TRANSFER MEMBER FILLET TO DIRECT COOLING FLOW

Heat exchanger for a hydrogen fuel delivery system

Flow guides for internal cooling of a CMC airfoil

Ring segment assembly in gas turbine engine

Turbine engine combustor having a combustion chamber heat shield

Combined TCA cooler and FGH for power plants

Turbine blade and gas turbine

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

Turbine arrangement including a turbine outlet stator vane arrangement

Device to shift structural resonance in a vertical long shaft pump

Internally cooled turbine blade

Components for gas turbine engines

Cooling schemes for airfoils for gas turbine engines

Turbine blade comprising ribs between cooling outlets with cooling holes

Thermal management system for gas turbine engine

HYBRID SUPPLY CONFIGURATION FOR AXIALLY FLOWING HIGH INTERNAL MACH NUMBER BAFFLES

Integrated oil tank with passive thermal modulation

Surface cooler assembly

Gas turbine engine airfoil fairing with rib having radial notch

Cooling structure and method of trailing-edge cutback of turbine blade, and turbine blade

Optimized heat exchange system for a turbomachine

Cooling device for turbine nozzle guide vane by liquid metal with low melting point

Turbine airfoil and turbine including same

Optimised heat exchange system of a turbomachine

Method and system of monitoring a component of an aircraft

ENGINE COMPONENT ASSEMBLY

Fin for internal cooling of vane wall

Cooling structure for trailing edge of turbine blade

Turbine blade repair method using additive manufacturing

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

Matrix for an Air/Oil Heat Exchanger of a Jet Engine

Impingement panel support structure and method of manufacture

Flared central cavity aft of airfoil leading edge

Airfoil tip pocket with augmentation features

Cast turbine nozzle having heat transfer protrusions on inner surface of leading edge

Apparatus for controlling turbine blade tip clearance and gas turbine including the same

Heat exchanger for a turbomachine and manufacturing thereof

Printing-enhanced casting cores

Gas turbine engine components having interlaced trip strip arrays

Turbomachine rotor blade with a cooling circuit having an offset rib

Turbine blade repair method using additive manufacturing

Impingement insert for a gas turbine engine

INTEGRATED OIL TANK WITH PASSIVE THERMAL MODULATION

Turbine rotor blade with platform with non-linear cooling passages by additive manufacture

Turbine rotor blade root with hollow mount with lattice support structure by additive manufacture

Double walled stator housing

Component having a dirt tolerant passage turn

Turbine vane with dust tolerant cooling system

Turbine vane with dust tolerant cooling system

Unitary body turbine shrouds including shot peen screens integrally formed therein and turbine systems thereof

Airfoil for a turbine engine incorporating pins

Compressor with thermal expansion reducing structure

Airfoil with connecting rib

Airfoil rib with thermal conductance element

Airfoil with ribs defining shaped cooling channel

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

Impingement cooling with impingement cells on impinged surface

Turbine component with dust tolerant cooling system

Turbine vane assembly incorporating ceramic matrix composite materials and cooling

Method for fan blade heating using coanda effect

Airfoil with ribs having connector arms and apertures defining a cooling circuit

Tandem seal pump

AIRFOIL WITH TUNABLE COOLING CONFIGURATION

System for a combined turbine and bearing case for a turbocharger

Turbine blade and gas turbine

Engine component with set of cooling holes

Brazed in heat transfer feature for cooled turbine components

Components for gas turbine engines

Turbine blade with dust tolerant cooling system

Turbine blade with serpentine channels

Turbomachine blade with trailing edge having improved cooling

Shroud interlock

Cooling schemes for airfoils for gas turbine engines

Inter-compressor cross-over pipe heat exchanger

Turbine stator outer shroud cooling fins

COMPONENTS FOR GAS TURBINE ENGINES

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

Internally-cooled turbomachine component

A TURBOMACHINE BLADE OR VANE HAVING A VORTEX GENERATING ELEMENT

Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger

Turbomachine vane, including deflectors in an inner cooling cavity

Gas turbine blade

Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly

Airfoil tip pocket with augmentation features

Turbine airfoil with trailing edge framing features

Coolant channel

Turbine shroud cooling

AIRFOIL FOR A TURBINE ENGINE

Blade for a turbine blade

Blade/vane cooling passages

Acoustic resonance excited heat exchange

Backside features with intermitted pin fins

Air-oil heat exchanger

Airfoil having dead-end tip flag cavity

Surface modifications for improved film cooling

Heat exchanger and methods of forming

Air-oil heat exchanger

Surface cooler and method of forming

Airfoil with cooling passage network having flow guides

Turbine blade with a coupled serpentine channel

Turbine scroll assembly for gas turbine engine

Dirt tolerant pins for combustor panels

Axial flow cooling scheme with castable structural rib for a gas turbine engine

AXIAL FLOW COOLING SCHEME WITH STRUCTURAL RIB FOR A GAS TURBINE ENGINE

Thermal management system for gas turbine engine

Fin-pin flow guide for efficient transition piece cooling

Airfoil with arced pedestal row

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

Structure for improving performance of cooling blade, and blade and gas turbine having the same

Cooling systems for gas turbine engines

Impingement cooling for a gas turbine engine component

Airfoil cooling circuit

Turbine stator blade

Method and apparatus for improving cooling of a turbine shroud

Blade outer air seal fin cooling assembly and method

Ribbed pin fins

Vane platform leading edge recessed pocket with cover

Turbine blade including pin-fin array

Turbine rotor blade with airfoil cooling integrated with impingement platform cooling

Airfoil leading edge cooling channels

ADDITIVE MANUFACTURING METHOD FOR THE ADDITION OF FEATURES WITHIN COOLING HOLES

Flared central cavity aft of airfoil leading edge

Turbine blade cooling system with channel transition

AIRFOIL HAVING ANGLED TRAILING EDGE SLOTS

Airfoil with tunable cooling configuration

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

TURBINE ELEMENT FOR HIGH PRESSURE DROP AND HEAT TRANSFER

Cooling circuit with shaped cooling pins

Article having ceramic wall with flow turbulators

Casting plug with flow control features

Electronics assembly having a heat sink and an electrical insulator directly bonded to the heat sink

Turbine blade or a turbine vane for a gas turbine

Structure for cooling turbine blade

Cooling configuration for a cold gas turbine generator assembly

Heat exchanger with non-orthogonal perforations

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

Coolant channel

Blade outer air seal cooling fin

AXIAL STIFFENING RIBS/AUGMENTATION FINS

COOLANT CHANNEL WITH INTERLACED RIBS

AIRFOIL HAVING LEADING EDGE COOLING SCHEME WITH BACKSTRIKE COMPENSATION

Cooling and lubrication system for a turbocharger

Cooling passage with structural rib and film cooling slot

Impingement cooling features for gas turbines

Gas turbine

Keystoned blade track

Hybrid cooling schemes for airfoils of gas turbine engines

Dual-wall impingement cavity for components of gas turbine engines

Method and apparatus for cooling an rotor assembly

Gas turbine engine components having internal hybrid cooling cavities

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

Diffuser integrated heat exchanger

Heat dissipation system for electric aircraft engine

Gas turbine engine components having internal cooling features

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

Chevron trip strip

Turbine shroud cooling

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

Matrix for an air/oil heat exchanger of a jet engine

Turbo engine rotor disc

Modified structural truss for airfoils

Blade ring segment for turbine section, turbine section having the same, and gas turbine having the turbine section

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

Airfoil having internal hybrid cooling cavities

Airfoil having internal hybrid cooling cavities

Printing-enhanced casting cores

Woven skin cores for turbine airfoils

Hot section engine components having segment gap discharge holes

Airfoil having end wall contoured pedestals

Airfoil having forward flowing serpentine flow

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

Surface heat exchanger and acoustic treatment

Engine component with non-uniform chevron pins

System and method for converting turbine cooling nozzle

Endwall cooling system

Airfoil edge cooling channels

Turbine airfoil having flow displacement feature with partially sealed radial passages

Compressor bleed cooling system for mid-frame torque discs downstream from a compressor assembly in a gas turbine engine

Cooling configuration for a gas turbine engine airfoil

Fluid cooling systems for a gas turbine engine

Turbomachine rotor blade

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

Acoustic resonance excited heat exchange

Engine component with cooling passages

Cored airfoil platform with outlet slots

Turbomachine blade cooling structure and related methods

Engine component with insert

Adaptive cover for cooling pathway by additive manufacture

Heater apparatus and method for heating a component of a spacecraft, and spacecraft comprising a heater apparatus

Impingement insert

Gas turbine engine with a diffuser cavity cooled compressor

Airfoil turn caps in gas turbine engines

Combustor panel cooling arrangements

Method and system for cooling fluid distribution

Engine component with flow enhancer

Turbine component with shaped cooling pins

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

Airfoil tip pocket with augmentation features

Airfoil cooling

Actively cooled component

Combustor pipe, combustor, and gas turbine

Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function

Impingement jet strike channel system within internal cooling systems

Component having active cooling and method of fabricating

Gas turbine engines including channel-cooled hooks for retaining a part relative to an engine casing structure

Gas turbine engine component with flow separating rib

Blade tip cooling arrangement

Apparatus including heat exchanger and sound attenuator for gas turbine engine

Airfoil cooling structure

Turbomachine rotor blade

Internally cooled engine components

Turbine scroll assembly for gas turbine engine

Blade, cut-back of blade or vane and gas turbine having the same

Nacelle inner lip skin with heat transfer augmentation features

Gas turbine blade

COMPONENT HAVING IMPINGEMENT COOLED POCKETS FORMED BY RAISED RIBS AND A COVER SHEET DIFFUSION BONDED TO THE RAISED RIBS

Combustion chamber and a combustion chamber fuel injector seal

Plate-shaped structural component of a gas turbine

Cooling structure for vane

Turbine airfoil with trailing edge cooling circuit

Engine component with flow enhancer

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

Engine with chevron pin bank

Article having ceramic wall with flow turbulators

Airfoil with laterally insertable baffle

Airfoil having endwall panels

Additively manufactured component for a gas powered turbine

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

Bearing housing with impingement cooling system

GAS TURBINE ENGINE HAVING A CASING PROVIDED WITH COOLING FINS

Circular heatsink

Apparatus and systems for a surface cooler having pliant fins

GAS TURBINE ENGINE

GAS TURBINE ENGINE

TURBINE COMPONENT THERMAL BARRIER COATING WITH VERTICALLY ALIGNED, ENGINEERED SURFACE AND MULTIFURCATED GROOVE FEATURES

FAN CASING ASSEMBLY WITH COOLER AND METHOD OF MOVING

Turbine blade trailing edge with low flow framing channel

AIRFOIL FOR A TURBINE ENGINE WITH POROUS RIB

AIRFOIL FOR A TURBINE ENGINE WITH A POROUS TIP

GAS TURBINE ENGINE STATOR VANE BAFFLE ARRANGEMENT

Turbine blade with a non-constraint flow turning guide structure

Turbine vane with coupon having corrugated surface(s)

Forming cooling passages in thermal barrier coated, combustion turbine superalloy components

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Modular annular heat exchanger

Gas turbine blade

Combustor liner with dual wall cooling structure

Turbine shroud with abradable layer having dimpled forward zone

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

Impingement cooling system for a gas turbine engine