AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN IMPROVED COWLING PANEL

FIRE RETARDANT ENGINE CASING APPARATUS

Containment assembly for an aircraft engine

TURBORAMJET ENGINE

Connecting arrangement between components of an aircraft engine

Impeller for aircraft engine

Fire retardant engine casing apparatus

Bi-material joint for engine

Turbo charger with compressor wheel

Turbine blade having a structural reinforcement with enhanced adherence

Guide vane for a gas turbine engine and method for testing a bond seal of a guide vane for a gas turbine engine

Hybrid airfoil for gas turbine engines

Fan blade having closed metal sheath

Rotor assembly for in-machine grinding of shroud member and methods of using the same

Nozzle-to-engine mount reinforcement through which mounting fasteners are visible

Wear resistant turbine blade tip

Wear resistant airfoil tip

Fan blade with composite cover

Method for adhesive bonding of titanium components using a fiber laser system

Multi-material leading edge protector

FAN CONTAINMENT

Hybrid airfoil for gas turbine engines

Erosion protection coating with screen

Fan blade having closed metal sheath

Anti-fire device for closing spaces at joints of a nacelle and nacelle comprising such a device

Turbo molecular pump for mass spectrometer

Erosion resistant steam valve

Systems and methods for fan blade de-icing

Aircraft fan with low part-span solidity

Vane stages

Compressor rotor with coated blades

BLADE CONTAINMENT STRUCTURE

Method for inserting septum into acoustic liner

COMPOSITE COATING LAYER HAVING IMPROVED EROSION RESISTANCE AND TURBINE COMPONENT INCLUDING THE SAME

Manufacture of a hollow aerofoil

Turbine blade with abradable tip

Method of producing a gas turbine engine component

Fan spacer for a gas turbine engine

Wear resistant turbine blade tip

Turbine engine blade with leading edge strip

ADDITIVELY MANUFACTURED INTEGRATED VALVE AND ACTUATOR FOR A GAS TURBINE ENGINE

Resin transfer molded rocket motor nozzle

Fairings for power generation machines

Devices and methods for exhaust vectoring in tilt rotor aircraft

Compressor rotor with coated blades

Entrance and exit chip rings for balancing broach forces

Sintered non-porous cathode and sputter ion vacuum pump containing the same

Power beam welded cavity-back titanium hollow fan blade

Processes and tooling associated with diffusion bonding

Gas turbine engine fan blade, design, and fabrication

Actuation via surface chemistry induced surface stress

Hollow titanium airfoil with titanium coating

Peening Method for Turbine Engine Component

Hybrid turbine blade for improved engine performance or architecture

Apparatus and method for non-destructive detection of fan blade electrical isolation

Blade comprising a folded leading edge shield and method of manufacturing the blade

Blade comprising a leading edge shield and method for producing the blade

Fan

ALUMINUM BRAZING OF HOLLOW TITANIUM FAN BLADES

FAN BLADE WITH ANODE AND METHOD FOR GALVANIC CORROSION MITIGATION

Systems and methods for making blade sheaths

Sync ring assembly and associated clevis including a rib

Composite blade, comprising a leading-edge reinforcement made of another material

Three-spring ram air turbine actuator

Reinforcement for the leading edge of a turbine engine blade

Aircraft fan with low part-span solidity

Composite panel and aircraft turbojet engine nacelle comprising such a panel

Multi-piece non-linear airfoil

Air foil with galvanic protection

Micro lattice hybrid composite fan blade

Flame-holder device

Blade shield removal and replacement

Method for repairing a fan casing

Method of manufacturing a leading edge shield

FRICTION WELDING

Load absorption systems and methods

Turbine blade attachment curved rib stiffeners

Turbine blade attachment rails for attachment fillet stress reduction

Method for producing an especially large aeronautical part

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

Fan blade with adhesive fabric stackup

Acoustic measurement system incorporating a temperature controlled waveguide

Compressor blade or vane having an erosion-resistant hard material coating

Pump housing of a magnetic and a non-magnetic material

Erosion and wear protection for composites and plated polymers

Nose cone assembly

Abrasive tip for composite fan blades

Gas turbine engine rotor mistuning

Aircraft blade lock retainer

HIGH TEMPERATURE, LOW OXIDATION, AMORPHOUS SILICON-COATED TITANIUM

Composite compressor blade for an axial-flow turbomachine

Vane stages

ALUMINUM AIRFOIL WITH TITANIUM COATING

Fan blade assembly

Electric conduction structure for jet engine

Method to immobilize an entrapped contaminant within a honeycomb structure

Turbine engine casing and manufacturing method

Erosion resistant material and turbine blade

GAS TURBINE BLADE AND METHOD OF PROTECTING SAME

High-modulus coating for local stiffening of airfoil trailing edges

Tooling for fastening metal reinforcement on the leading edge of a turbine engine blade, and a method using such tooling

Method of forming an inflated aerofoil

Composite Fan Blade

Turbine engine hybrid rotor

COMPOSITE AIRFOIL METAL LEADING EDGE ASSEMBLY

Method of making a Ni—based single crystal superalloy and turbine blade incorporating same

Fan blades with protective sheaths and galvanic shields

Hollow fan blade with extended wing sheath

Locally extended leading edge sheath for fan airfoil

Low speed fan for gas turbine engines

Fibre pre-form manufacturing method

Hybrid turbine blade for improved engine performance or architecture

Forming a complexly curved metallic sandwich panel

Creep-resistant TiA1 alloy

Turbomachine blade comprising an insert protecting the blade tip

Hybrid turbine blade for improved engine performance or architecture

Hybrid spinner support

Airfoil with galvanic corrosion preventive shim

Composite turbine engine blade with structural reinforcement

TWO-PIECE DUCT ASSEMBLY

Thruster and spacecraft

Method of bonding a leading edge sheath to a blade body of a fan blade

Rotor

Method for producing a fibrous metal structure by means of weaving

Chromium alloy

COMPOSITE FILLED METAL AIRFOIL

ALUMINUM FAN BLADE ROOT

Steam turbine

Turbine engine support arms

Demisable fuel supply system

Demisable fuel supply system

FINAL-STAGE ROTOR BLADE OF A STEAM TURBINE

Nose cone assembly

Gas turbine blade and method of protecting same

Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE

METHOD AND APPARATUS FOR AIR FLOW CONTROL

Component for a gas turbine and a method for the production of the component

ANTI-EROSION COATING SYSTEM FOR GAS TURBINE COMPONENTS

Turbine Blade, Especially Rotor Blade for a Steam Engine, and Corresponding Method of Manufacture

METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED USING THIS METHOD

METHOD FOR MANUFACTURING A TITANIUM PART THROUGH INITIAL BETA FORGING

Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor

Pulse detonation system

METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED ACCORDING TO THIS METHOD

Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method

Fan airfoil sheath

Assembling titanium and steel parts by diffusion welding

Ring-shaped disk for gas turbine

Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor

COMPOSITE AIRFOILS HAVING LEADING EDGE PROTECTION MADE USING HIGH TEMPERATURE ADDITIVE MANUFACTURING METHODS

Hollow turbine blade

Steam turbine rotor and alloy therefor

Titanium sheath and airfoil assembly

CHARGING DEVICE, MORE PREFERABLY EXHAUST GAS TURBOCHARGER FOR A MOTOR VEHICLE

Process for manufacturing a single-piece blisk with a temporary blade support ring removed before a milling finishing step

Process for manufacturing a single-piece blisk by cutting with an abrasive water jet

Process for manufacturing a single-piece blisk with a temporary blade support ring arranged at a distance from blade tips

Method of manufacturing a turbine fan blade

HIGH TEMPERATURE ADDITIVE MANUFACTURING SYSTEMS FOR MAKING NEAR NET SHAPE AIRFOILS LEADING EDGE PROTECTION, AND TOOLING SYSTEMS THEREWITH

Heat transfer system and method for turbine engine using heat pipes

Fan blade platform

HEAT-RESISTANT COMPONENT

Method of protecting reactor components from fouling

Rotor assembly for an exhaust gas turbocharger

Intake cone for a gas-turbine engine

Vibration damping novel surface structures and methods of making the same

Method for the provision of fire protection for titanium components of an aircraft gas turbine and titanium components for an aircraft gas turbine

Erosions systems and components comprising the same

Methods allowing for visual inspection of coated components for erosion damage

Methods for making components having improved erosion resistance

Systems and methods involving localized stiffening of blades

Method of manufacturing a turbine fan blade

Annular component

Actuation via surface chemistry induced surface stress

Particulate mitigating propellant management tank device

Damping device for composite blade

Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon

Centerline compression turbine engine

Component with a damping filler

Component with a damping filler and method

Method of forming an aerofoil with a damping filler

Friction Welding Method and Components Produced From Steel and Metal Aluminide Using an Intermediary From an Ni Alloy

Turbocharger including cast titanium compressor wheel

TURBOMACHINE BLADE AND TURBOMACHINE COMPRISING THIS BLADE

Fan case reinforcement in a gas turbine jet engine

Fan case reinforcement in a gas turbine jet engine

Method for producing a titanium metallic composition having titanium boride particles dispersed therein

Treatment of turbine blades to increase hardness

METHODS AND ARTICLES RELATING TO HIGH STRENGTH EROSION RESISTANT TITANIUM ALLOY

Method and apparatus for gas turbine engines

Titanium foil as a structural heater element

Turbine engine system with shafts for improved weight and vibration characteristic

Turbine Vane for Turbo-Machines and Method for Fabricating

Surface treatment for a thin titanium foil

Composite turbomachine blade with metal reinforcement

Erosion-protective coatings on polymer-matrix composites and components incorporating such coated composites

Guide vane for a gas turbine engine

Turbomachine blade

Heat bridge between accessory casing and airplane engine accessory box

Rotor For A Turbo Machine And Method For The Manufacture Of Such A Rotor

Method of manufacturing a component

Method of fabricating a turbomachine rotor disk

Aerofoil

Side thruster module

Compressor, titanium-made rotor blade, jet engine and titanium-made rotor blade producing method

ANTI-WEAR DEVICE FOR A GUIDE PIVOT OF A VARIABLE-PITCH VANE OF A TURBOMACHINE COMPRESSOR

Variable stator vane assembly and bushing thereof

Gas turbine engine blade containment assembly

Turbomachine rotor including at least one disk reinforced by a composite ring

Generator for an engine

Tool for producing cast components, method for producing said tool, and method for producing cast components

Method of repairing a blade of a one-piece bladed disc of a turbomachine and test piece for implementing the method

Assembly and method for manufacture of component by hot isostatic pressing

Method of manufacturing a duct for a gas turbine engine

Erosion and wear resistant protective structures for turbine components

Backswept titanium turbocharger compressor wheel

Turbocharger with titanium component

Control lever for the angular setting of a stator blade in a turboshaft engine

Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine

Method for producing a titanium metallic composition having titanium boride particles dispersed therein

Application of high strength titanium alloys in last stage turbine buckets having longer vane lengths

Rotor blade containment assembly for a gas turbine engine

Gas turbine engine blade containment assembly

Compressor rotor and method for making

Compressor wheel joint

Blade for a turbine engine and method for production of said blade

Component with internal damping

Fan design