Composite fan blade with leading edge sheath and energy absorbing insert

Blade and method for reloading an abradable coating

Pitch actuation system for a turbomachine propeller

Gas turbine engine with geared architecture

Gearbox for a gas turbine engine

Annulus filler

Hollow fan blade constrained layer damper

Mistuned fan for gas turbine engine

Gas turbine engine with axial movable fan variable area nozzle

Geared turbine engine with relatively lightweight propulsor module

Air flow straightening assembly and turbomachine including such an assembly

Method for manufacturing a composite casing for a turbomachine compressor

BLADE OR VANE FOR A GAS TURBINE ENGINE

Assembly consisting of a bearing support and bearings of a rotor shaft in a turbomachine

Axial retention of a fan shaft in a gas turbine engine

Trunnion retention for a turbine engine

Mistuned compressor rotor with hub scoops

LAMINATED HYBRID COMPOSITE-METALLIC CONTAINMENT SYSTEM FOR GAS TURBINE ENGINES

Gas turbine engine with minimal tolerance between the fan and the fan casing

Method of providing turbine engines with different thrust ratings

Rotor with non-uniform blade tip clearance

Fan blade tip with frangible strip

Composite material casing of stiffening shape

Fan exit stator assembly

Fan Containment case for gas turbine engines

Fan stress tracking for turbofan gas turbine engines

GAS TURBINE ENGINE

Gas turbine engine

Gas turbine engine airfoil

Blade platform and a fan disk for an aviation turbine engine

Rotating airfoil with tip pocket

Hub for propeller having variable-pitch blades, with radial and axial dimensioning variation

FAN DISC APPARATUS

Turbine fan system and method

Vane assembly of a gas turbine engine

Low-noise airfoil for an open rotor

Geared turbofan engine with high compressor exit temperature

Power beam welded cavity-back titanium hollow fan blade

Processes and tooling associated with diffusion bonding

Axially-partitioned oil-distribution wheel, and planetary reduction gear comprising such a wheel

Methods of customizing, manufacturing, and repairing a rotor blade using additive manufacturing processes

Fan module with variable-pitch blades for a turbine engine

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Geared gas turbine engine with reduced fan noise

Leading edge shield

Method to strip and recoat erosion coatings applied to fan blades and structural guide vanes

Turbine section of high bypass turbofan

Turbomachine vane comprising an electroacoustic source with improved assembly mode, row of outlet guide vanes and turbomachine comprising such a vane

Gas turbine engine with gearbox health features

Aircraft gas turbine engine variable fan blade mechanism

Gas turbine engine fan blade, design, and fabrication

Apparatus for airfoil leading edge protection

Gas turbine engine hollow fan blade rib orientation

Blade, associated fan and turbojet engine

System for controlling the pitch of fan blades of a turbine engine, the system having a feathering-locking peg

Fan module having variable-pitch blades for a turbine engine

Non-contact seal assembly for rotational equipment

Fluid cooling systems for a gas turbine engine

Method for altering the law of twist of the aerodynamic surface of a gas turbine engine fan blade

Leading edge shield

Inlet pre-swirl gas turbine engine

Method of manufacturing a fan blade

Variable pitch change control method

Self-latching nacelle

TURBINE WITH FLOW INDUCED BY CRYOGENIC HELIUM

Distributed fan lubrication system

Electrical bus arrangement for ice protection systems

Following blade impact load support

Fan module with variable pitch blades

Aircraft turbomachine assembly having an improved decoupling system in the event of a fan blade loss

Softwall containment systems

Turbomachine module comprising a rotor supporting pitchable blades

Method of manufacturing a composite aircraft blade

Blade made of composite material with integrated platform for an aircraft turbine engine

System and method for manufacture of abrasive coating

OPEN-CELL RETICULATED FOAM

Three dimensional auxetic structure, manufacturing method and tooling

Variable pitch fan blade system

Nacelle

Systems and methods for electronic measurement of propeller blade angle

Variable pitch fan blade system

LOW NOISE COMPRESSOR AND TURBINE FOR GEARED TURBOFAN ENGINE

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

Tapered composite backsheet for use in a turbine engine containment assembly

Airfoil structure and method of manufacture

Aircraft propulsion assembly equipped with a main fan and with at least one offset fan

Mitigation of effects of fan blade off in a gas turbine engine

Turbine engine airfoil with a modified leading edge

Gas turbine engine

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

Aircraft propulsion assembly equipped with a main fan and with a least one offset fan

Epicyclic gear train

Asymmetric multi degree of freedom flutter damper

Variable displacement flutter damper for a turbofan engine

Acoustic panel of turbine engine and method of arranging the acoustic panel

Flutter damper for a turbofan engine

Airfoil containment structure including a notched and tapered inner shell

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

Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan

GEARED TURBOFAN

Fan casing and mount bracket for oil cooler

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Turbine engine and method of manufacturing

Fan

Core-protecting fan modules and turbofan engines containing the same

Fan platform with stiffening feature

Fan

Apparatus including heat exchanger and sound attenuator for gas turbine engine

Airflow straightening assembly having improved aerodynamic performances

Thrust-ring and rotor fan system

High compressor build clearance reduction

Gas turbine engine with geared architecture

Apparatus including heat exchanger and sound attenuator for gas turbine engine

Turbine engine lubrication system with wash flow filter

Propulsion system for an aircraft

ALUMINUM BRAZING OF HOLLOW TITANIUM FAN BLADES

COOL CORE GAS TURBINE ENGINE

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

Turbofan case for controlling blade deflection

Rotary assembly of an aeronautical turbomachine comprising an added-on fan blade platform

Lock for threaded in place nosecone or spinner

Unsymmetrical turbofan abradable grind for reduced rub loads

DISPOSABLE FAN PLATFORM FAIRING

Turbofan nacelle assembly with flow disruptor

Steel soft wall fan case

Components having vibration dampers enclosed therein and methods of forming such components

Method for manufacturing a turbomachine fan having a reduced noise level at multiple rotational frequencies of said turbomachine

Systems and methods for making airfoils

Systems and methods for making blade sheaths

Fan blade having a tip assembly

Assembly of turbine engine parts comprising a fan blade having an integrated platform, and corresponding turbine engine

Geared low fan pressure ratio fan exit guide vane stagger angle

Method of fabricating an airfoil element out of composite material and having metal reinforcement fastened by riveting

Guide vane assembly with compensation device

Fan drive gear system module and inlet guide vane coupling mechanism

Airfoil structure having a shape memory alloy actuator

Integrated fan heat exchanger

Thrust ring and rotor fan system with passive leading edge slats

Geared turbofan gas turbine engine architecture

Reinforcement for the leading edge of a turbine engine blade

Blade comprising lands with a stiffener

Fan module with rotatable vane ring power system

Method and system for elastic bearing support

Rotary assembly of a turbomachine equipped with an axial retention system of a blade

Methods and systems for bonding

Supersonic single-stage turbofan engine

Vane comprising an assembled platform and blade

Blade equipped with platforms comprising a retaining leg

Integrally bladed fan rotor

Gas turbine engine with graphene heat pipe

Blisk comprising a hub having a recessed face on which a filling member is mounted

Gas turbine engine with a geared turbofan arrangement

Gas turbine engine with a geared turbofan arrangement

Turbomachine stator travelling wave inhibitor

Fan blade with structural spar and integrated leading edge

Aircraft fan with low part-span solidity

ROTOR STAGE

Damping characteristic determination for turbomachine airfoils

METHOD FOR SETTING A GEAR RATIO OF A FAN DRIVE GEAR SYSTEM OF A GAS TURBINE ENGINE

Real time aerodamping measurement of turbomachine

Method of fabricating a reference blade for calibrating tomographic inspection, and a resulting reference blade

Method for detecting a fluid leak in a turbomachine and fluid distribution system

Multi-piece non-linear airfoil

Gas turbine engine with cold turbine and multiple core flowpaths

Anti-rotation feature for wear liners

Gas-turbine engine composite components with integral 3-D woven off-axis reinforcement

Fiber composite material and preform and fan blade made therefrom

Gas turbine engine with axial movable fan variable area nozzle

Aluminum fan blade tip prepared for thermal spray deposition of abrasive by laser ablation

Method for high temperature forging of a preformed metal part, and shaping equipment suitable for forging

Micro lattice hybrid composite fan blade

Mistuned laminate airfoil

Turbine engine air guide assembly with improved aerodynamic performance

Annular heatshield

Fan blade with composite cover

Gas turbine engine with axial movable fan variable area nozzle

Assembly and method for influencing flow through a fan of a gas turbine engine

Nacelle

Nose cone attachment for turbofan engine

Method for release of fan blisk airfoil with external shaped charge

Aircraft engine power generator disposed inside of a stationary nose cone

Method of releasing a fan blade and assembly for releasing a fan blade from a turbofan engine

Strut assembly for an aircraft engine

Non-Newtonian materials in aircraft engine airfoils

Fan blade

Geared gas turbine engine

Gas turbine engine with axial movable fan variable area nozzle

Fitted platform for a turbine engine fan, and a method of fabricating it

Blade shield removal and replacement

Method and system for metallic low pressure fan case heating

Conical load spreader for composite bolted joint

Condensation irradiation system

LOW NOISE COMPRESSOR AND TURBINE FOR GEARED TURBOFAN ENGINE

Compression system for a turbine engine

Mechanically retained fan blade cover

Fastener and method of restricting fluid flow using same

Low-cost epicyclic gear carrier and method of making the same

Liner system

Low profile fan platform attachment

Low pressure generator for gas turbine engine

GAS TURBINE ENGINES WITH FLUTTER CONTROL

Control of low pressure generator for gas turbine engine

System and method for nose cone edge delamination repair

Low pressure generator with electrical assembly for gas turbine engine

Apparatus and system for composite fan blade with fused metal lead edge

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

Abrasive blade tips with additive layer resistant to clogging

Organic matrix abradable coating resistant to clogging of abrasive blade tips

Gas turbine engine

Gas turbine engine with distributed fans

Sliding nozzle flap assembly

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Geared turbofan gas turbine engine architecture

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Gas turbine engine geared architecture axial retention arrangement

Cooling air architecture for compact size and performance improvement

Aerofoil body

Vane with spoiler

Electric propulsion engine for an aircraft

Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vane

Fan blade removal feature for a gas turbine engine

Fan blade and method of manufacturing a fan blade

Blade with a platform and a hollow bumper

Turbomachine guide vanes with improved vane profile

Repair of an assembly comprising a main body and a reinforcement

Method of manufacturing a leading edge shield

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Guide vane plate with a chamfered and a cylindrical edge region

Airfoil with multi-material reinforcement

Composite component

Fiber structure woven as a single piece by 3D weaving, and an application thereof to fabricating a composite material part

Shape memory alloy variable stiffness airfoil

Gas turbine engine gear train

Compressor rotor for supersonic flutter and/or resonant stress mitigation

Turbomachine blade, comprising a root with reduced stress concentrations

Gas turbine engine airfoil

Containment case trench filler layer and method of containing releasable components from rotatable machines

AIRCRAFT ENGINE WITH AN IMPACT PANEL

Actuation system for varying blade pitch

Load absorption systems and methods

NOSE CONE FOR A FAN OF AN AIRCRAFT ENGINE

Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function

Method and system for fiber reinforced composite panels

Method and system for controlling core cowl vent area

System and method of alleviating blade flutter

Stator-vane structure and turbofan engine employing the same

Fan track liner subassembly angled upturn joint

GRAPHENE ULTRA-CONDUCTIVE CASING WRAP

Gas turbine engine airfoil

Method and system for improving structural characteristics of composite component corners

Low noise compressor and turbine for geared turbofan engine

Aircraft engine and associated method for driving the fan with the low pressure shaft during taxi operations

Nacelle short inlet for fan blade removal

Gas turbine engine airfoil

Method and system for in-line distributed propulsion

Gas turbine engine with short inlet and blade removal feature

Gas turbine engine with short inlet and mistuned fan blades

Thrust efficient turbofan engine

Methods and apparatus for noise attenuation in an engine nacelle

Hybrid propulsion system including a chemically rechargeable ultra-capacitor

Fan for a turbomachine

Rotor assembly for use in a turbofan engine and method of assembling

Cascade assembly for a thrust reverser of an aircraft nacelle

Gas Turbine Engine

Method and system for improving turbine blade performance

Method of manufacturing a gas turbine engine

Fan blade apparatus

Casing for use in a turbofan engine and method of scavenging fluid therefrom

Geared turbofan with four star/planetary gear reduction

Gas turbine engine

Gas turbine engine

Compression cowl for jet engine exhaust

Gas turbine engine module adapter to a carrier

Method for balancing a turbofan engine or other rotating system

Airfoil platform having dual pin apertures and a vertical stiffener

Platform for an airfoil having bowed sidewalls

Pitch range for a variable pitch fan

Modular fan for a gas turbine engine

Variable pitch fan actuator

Geared turbomachine fan and compressor rotation

FUEL NOZZLE WALL SPACER FOR GAS TURBINE ENGINE

Gas turbine engine airfoil

Manhattan dual FDGS aux pump design

Differential gas bearing for aircraft engines

Nacelle fluid drain

Turbofan engine and method of reducing air flow separation therein

Nose cone and shaft balancing assembly

Propulsive assembly for aircraft comprising a turbojet fitted with a fan with removable blades

Fixed support and oil collector system for ring gear

Variable effective area fan nozzle

Engine having variable pitch outlet guide vanes

Fan platform for a gas turbine engine

Aviation turbine engine fan assembly including a fitted platform

Method and system for modulated turbine cooling

Gear system architecture for gas turbine engine

Trailing edge core compartment vent for an aircraft engine

Gas turbine engine uncontrolled high thrust detection system and method

Gas turbine engine with axial movable fan variable area nozzle