MITIGATION STRATEGY FOR AIRFOIL CRACKS FOR INTEGRALLY BLADED ROTORS

INTEGRAL COMPOSITE STATOR LABYRINTH SEAL

Turbocharger

Front frame and deflection grid of a thrust reverser of an aircraft nacelle

Monolithic rotor and compressor wheel

Additively Manufactured Component Including an Impingement Structure

Method of assembly for gear system with rotating carrier

Sacrificial plug system

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

Method of assembly for fan drive gear system with rotating carrier

Hybrid rocket motor with integral oxidizer tank

Method of manufacturing a component of a rotary machine and component manufactured using said method

TURBOCHARGER

Turbomachine vane with integrated metal leading edge and method for obtaining it

METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PART PROVIDED WITH A SENSOR

Stress reduction structure, gas turbine casing, and gas turbine

Turbine blade cooling hole arrangement

Turbine vane assembly with ceramic matrix composite components mounted to case

Air intake scoop for an aircraft

Unitary flow path structure

Turbine nozzle with CMC aft band

Reduced stress boss geometry for a gas turbine engine

Potted stator vane with metal fillet

Diffuser for compressor

Methods and features for positioning a flow path inner boundary within a flow path assembly

Additively manufactured tube array

Method of assembly for fan drive gear system with rotating carrier

Recuperator for gas turbine engine

TURBINE BLISK AND METHOD OF MANUFACTURING THEREOF

Method for manufacturing centrifugal rotary machine and method for manufacturing impeller thereof

Sump housing for a gas turbine engine

CONTOURED CASE BOSSES FOR A GAS TURBINE ENGINE

Rotary machine and impeller

Process of making integrally bladed rotor

BLADE OF A TURBOMACHINE, INCLUDING A COOLING CHANNEL AND A DISPLACEMENT BODY SITUATED THEREIN, AS WELL AS A METHOD FOR MANUFACTURING

Turbine engine with single wall cantilevered architecture

Inlet frame for a gas turbine engine

Radial compressor and exhaust gas recirculation system

TURBOMACHINE SEALING ELEMENT

GEARED TURBOFAN WITH INTEGRALLY BLADED ROTOR

Rotor with zirconia-toughened alumina coating

Additively manufactured heat exchanger

Additively manufactured component including an impingement structure

Turbine nozzle with CMC aft Band

Method for manufacturing blisk, and blisk intermediate product

Flow path assembly with pin supported nozzle airfoils

Methods and features for positioning a flow path inner boundary within a flow path assembly

Cooled blisk with dual wall blades for gas turbine engine

Unitary flow path structure

Unitary flow path structure

Unitary flow path structure

Planetary gear system and gas turbine engine with a planetary gear system

HOLLOW-WALL HEAT SHIELD FOR FUEL INJECTOR COMPONENT

Radial compressor and turbocharger

Turbocharger having a nozzle ring centered by a guiding projection

Reduction gear having an epicyclic gear train for a turbine engine

Diagonal or radial fan having a guide device

Coated turbomachinery component

Method for machining an attachment flange of an aircraft turbomachine case

Blade equipped with platforms comprising a retaining leg

Intermediate casing for a turbomachine turbine

Stator with adjustable vanes for the compressor of an axial turbine engine

Augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane

Rotary friction welding

Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct

Turbine engine and method of assembling

Method of manufacturing a component of a rotary machine and component manufactured using said method

Sump assembly for a gas turbine engine

ADJUSTABLE GUIDE VANE FOR TURBOMACHINE

Sump housing for a gas turbine engine

Hybrid rocket motor with integral oxidizer tank

Turbine blade attachment curved rib stiffeners

Device for attaching an air inlet onto a fan casing of an aircraft turbojet nacelle

Gas turbine engine with one piece acoustic treatment

High pressure exhaust muffling device with multiple sources

Compliant shaft with a recursive configuration for turbine engines

Segmented turbine blade squealer tip and cooling method

Rear frame for a thrust reverser structure with diversion grids

Reversible spiral groove journal bearing for use on standard and reverse rotation turbochargers

Heat-exchange and noise-reduction panel for a propulsion assembly

Cylindrical case

Axial turbomachine compressor casing

Combustion systems

Manufacture of a casing with a boss

Rotary machines including a hybrid rotor with an integrally bladed rotor portion

Reduced stress boss geometry for a gas turbine engine

Thermally compliant additively manufactured fuel injector

Thermally-coupled fuel manifold

Method for manufacturing a stage of a steam turbine

Combustor aft mount assembly

Structural honeycomb panel

Gas turbine engine truncated airfoil fillet

Integrally bladed rotor having axial arm and pocket

Ducted cowl support for a gas turbine engine

Variable shaft for hydraulic unit

Single-piece blisk for turbomachine fan comprising an upstream and/or downstream recess making its blades more flexible

Fuel/oil manifold

Additive manufactured ducted heat exchanger system with additively manufactured fairing

Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle

Turbine vane with platform pad

Instrumentation transfer strut

Hollow-wall heat shield for fuel injector component

Geared turbofan with integrally bladed rotor

TURBINE BLISK AND METHOD OF MANUFACTURING THEREOF

Method for producing an integral bent housing for an axial turbomachine compressor

Fan frame and assembling method thereof

Aircraft gas turbine having a core engine casing with cooling-air tubes

Method and device for manufacturing turbine blades

Monolithic shrouded impeller

Fuel manifold and fuel injector arrangement

Integrated frame structure of slim fan and manufacturing method thereof

Variable geometry turbo system

Method for manufacturing of a gas turbine engine component

Circulation pump

Web connected dual aerofoil members

Two-stage supercharging device

Turbomachine geared architecture support assembly

Impingement cooling of turbine blades or vanes

Combined hub, counterweight and crank arm with single piece steel body

Annular turbomachine seal and heat shield

Super polish masking of integrally bladed rotor

Turbocharger and engine cylinder head assembly

Combustion system including a transition piece and method of forming using a cast superalloy

Fan with metallic hub and plastic impeller and method for manufacturing such fan

Turbomachine geared architecture support assembly

Printed masking process

Integrated compressor housing and inlet

REDUCTION IN THERMAL STRESSES IN MONOLITHIC CERAMIC OR CERAMIC MATRIX COMPOSITE SHROUD

Integrated case and stator

Nozzled turbocharger turbine and associated engine and method

Support structure forming method

Turbocharger housing and tool device for machining the turbocharger housing

Turbocharger housing having a sealing device

APPLICATION OF TREATMENT FLUIDS TO COMPONENTS

One-piece manufacturing process

Multi-stage turbocharger arrangement

Multi-stage turbocharger arrangement

Supercharged internal combustion engine

Printed masking process

Impeller, compressor, and method for producing impeller

Diagonal fan

CO-CURED SHEATH FOR COMPOSITE BLADE

Exhaust-gas turbocharger

Heat dissipation system and fan thereof

Thrust Reversers Including Monolithic Components

Turbofan flow path trenches

Compact fan

Turbine nozzle assemblies

Vane for aircraft turbine engine receiver, provided with two hollow cores lodged in one another

COOLING APPARATUS FOR COMBUSTOR TRANSITION PIECE

Electric fluid pump and mold for insert-molding casing of electric fluid pump

Radial fan impeller

Pump

Method of producing a mini fan and a mini fan produced according to said method

Resinous shroud and manufacturing method of the same

Organic matrix composite integrally bladed rotor

Radial fan impeller

Blade and fan having the same

TURBOFAN AND MANUFACTURING METHOD THEREOF

BOX FAN GRILL WITH INTEGRAL MOTOR SUPPORT

Fan frame structure

Aeroengine thrust reverser

Flow-guiding member unit and its production method

Assembly of sectorized fixed stators for a turbomachine compressor

Centrifugal-fan impeller, and method of its manufacture

Injection molded centrifugal air impeller

Method of molding centrifugal impeller