Method to strip coatings off of an aluminum alloy fan blade

Planetary gearbox

Rotor blade retention system for a gas turbine engine

Blade for a turbomachine fan, comprising an identification medium, and method for reading such an identification medium

Variable pitch fans for turbomachinery engines

Platform for an airfoil of a gas turbine engine

Efficient aircraft engine

Ice accumulation and shedding mitigation for sensor probe

Geared turbofan engine with targeted modular efficiency

Blower vane

Structural assembly for a gas turbine engine

Rotor blade for a turbomachine, associated turbine module, and use thereof

Stator apparatus for a gas turbine engine

Thrust efficient gas turbine engine

Direct drive electrically-geared turbofan

Method for producing a casing for an aircraft turbine engine

Epicyclic gear train

Integrated hybrid propulsion system

Turbomachine assembly having a damper

Assembly for a turbomachine

HEAT EXCHANGER

Aircraft

Gas turbine engine fan

Lean burn combustor

GAS TURBINE FOR TWIN-ROTOR AIRCRAFT

LOW PRESSURE GENERATOR FOR GAS TURBINE ENGINE

Turbomachine fan

Electrically geared turbofan

Geared turbofan engine gearbox arrangement

Method for coating an aircraft turbomachine component

Multi-cover gas turbine engine component

Assembly of an outlet guide vane for an aircraft turbine engine using a reduced-size vacuum sheet

Turbomachine and gear assembly

HIGH PURITY ALUMINUM COATING WITH ZINC SACRIFICIAL UNDERLAYER FOR ALUMINUM ALLOY FAN BLADE PROTECTION

Gas turbine engine compression system with core compressor pressure ratio

Turbofan gas turbine engine

Aircraft with a single fluid inlet aperture

Heat exchanger

Heat exchanger

Gas turbine engine airfoil

Aircraft turbofan having a cowl articulated in rotation and a system for deploying said cowl

Geared turbine engine with relatively lightweight propulsor module

Turbojet engine fan casing

Stiffened rotor shaft for a gas turbine engine

Exhaust duct of gas turbine engine

Gas turbine engine with airflow measurement system

Device for driving a shaft of a jet engine for inspection purposes

AIRCRAFT ENGINE WITH IMPROVED HANDLING OF VIBRATIONAL MODES

Plain bearing for a planetary gear box, planetary gear box for a gas turbine engine, and a gas turbine engine

Planetary gearbox

Woven fibrous texture

Modeling method for a fan assembly of an aero engine

Turbomachine assembly comprising fan blades with an extended trailing edge

Generator cooling system for turbo-fan engine

COMPOSITE AIRFOIL WITH METAL STRENGTH

Fan blade comprising a thin shield and a stiffener

Systems and methods of power allocation for turboprop and turboshaft aircraft

Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub

Geared turbofan with over-speed protection

Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features

Turbomachine blade having a maximum thickness law with high flutter margin

Double-flow turbojet engine assembly with epicycloidal or planetary gearbox

Acoustically treated panels

Fan track liner

Low speed fan up camber

Fan module comprising variable-pitch blades

Electric module for an aircraft fan comprising blades with improved attachment

Hybridization of fibers of the fibrous reinforcement of a fan blade

COMPOSITE FAN CONTAINMENT CASE

Aircraft gas turbine engine with improved response to rotor unbalance

Aircraft engine

HYBRIDIZATION OF THE FIBRES OF THE FIBROUS REINFORCEMENT OF A BLADE

Engine mount system for a gas turbine engine

Geared gas turbine engine with reduced fan noise

Gas turbine engine with blade channel variations

EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES

Turbomachine with electric machine comprising a rotor ring attached to the fan

Methods and apparatus for gas turbine bending isolation

Turbojet with step-down mechanism

Gas turbine engine with speed sensor

Method for manufacturing a turbomachine composite part

Housing less front bearing compartment for gas turbine engine

Methods and apparatus to detect air flow separation of an engine

Electrically geared turbofan

Manufacture of a fan track liner

OGV electroformed heat exchangers

Mechanical reduction gear of an aircraft turbomachine

Airfoil with integral platform for gas turbine engines

Gearboxes for aircraft gas turbine engines

Gearboxes for aircraft gas turbine engines

Methods and systems for assessing engine health

Turbine section of high bypass turbofan

Cooling device for a turbine of a turbomachine

Turbofan engine front section

Turbine blade having a structural reinforcement with enhanced adherence

Blade cutback distribution in rotor for noise reduction

Variable pitch bladed disc

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

Gas turbine engine with axial movable fan variable area nozzle

Inlet guide vane draw heat exchanger system

FAN CASE FOR A GAS TURBINE ENGINE

Turbofan engine

High bypass ratio engine bypass duct nozzle with controlled nozzle area

Reliable gearbox for gas turbine engine

WALL DEPOSITION

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

Thermal management system

Fan blade platform seal and method for forming same

VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR

Fan and low pressure compressor geared to low speed spool of gas turbine engine

Epicyclic gear train

Turbine fan fairing platform with protective surface

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

Trunnion retention for a turbine engine

Turbofan comprising a system comprising flexible screens for closing off the bypass duct

Turbofan comprising a system comprising a screen for closing off the bypass duct

Fan blade having closed metal sheath

Shaft bearings for gas turbine engine

Exhaust nozzle of a gas turbine engine

Turbmachine fan disc

Dual density abradable panels

Shroud for splitter and rotor airfoils of a fan for a gas turbine engine

Reliable gearbox for gas turbine engine

High power epicyclic gearbox and operation thereof

Integral gutter and front center body

Turbofan engine, nacelle thereof, and associated method of operation

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

GAS TURBINE ENGINE FAN

Impeller with hub sweep

Mechanical attachment scheme for isogrid ducts

Airfoil-mounted platforms of gas turbine engines

SYSTEM FOR AN IMPROVED STATOR ASSEMBLY

Gas turbine engine with reversible heat exchanger

Gas turbine engine

Containment case having ceramic coated fibers

Oil baffles in carrier for a fan drive gear system

Damping device

EFFICIENT JET

GAS TURBINE ENGINE FOR AN AIRCRAFT COMPRISING AN AIR INTAKE

Seal ring assembly for a gas turbine engine

Method and system for detecting damage to the mobile blades of an aircraft

LOW POWER HYBRID TURBOFAN DRAG REDUCTION

Self retained linkage and system including the self retained linkage for a gas turbine engine

Ring gear mounting arrangement with oil scavenge scheme

Turbofan comprising a cam actuating a set of rotatable blades for blocking off the bypass flow duct

Turbofan gas turbine engine with gearbox

Turbofan gas turbine engine with gearbox

Containment case active clearance control structure

Geared turbofan engine with targeted modular efficiency

Damping device

GEARED TURBOFAN WITH FOUR STAR/PLANETARY GEAR REDUCTION

Gas turbine engine fan

Thermal management system using shape memory alloy actuator

Fan blade attachment root with improved strain response

Variable area fan nozzle for turbofan aircraft engine

Geared turbofan engine gearbox arrangement

Compressor rotor for supersonic flutter and/or resonant stress mitigation

Turbofan engine with acoustic treatment

Turbine assembly

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

AIRCRAFT ENGINE AND METHOD OF OPERATION THEREOF

AIRCRAFT ENGINE AND METHOD OF OPERATING SAME

Hybrid turbofan with differential electrical and mechanical power transfer

Geared gas turbine engine with reduced fan noise

Geared turbine engine with relatively lightweight propulsor module

Disengageable speed-reducing unit

Fan module with variable-pitch blades for a turbomachine

Geared gas turbine engine

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

Multi-cover gas turbine engine component

Guide vane for a turbomachine fan

Hybrid transmission turbojet engine

THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT

After-fan system for a gas turbine engine

Rotor blade of a turbomachine

Method of forming gas turbine engine components

Systems and methods for dry fog inlet particle separator

Multiple layer structure

Gas turbine engine compression system

Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

Internally damped airfoiled component

Fan blade with composite cover

Gas turbine engine with geared architecture

Abradable turbomachine element provided with visual wear indicators

Turbine exhaust case cooling

Compressor flowpath

Ventilation and extinguishing device for a gas turbine engine

Electric machine

Thrust efficient turbofan engine

Geared turbomachine fan and compressor rotation

Inter-blade platform seal

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

GAS TURBINE ENGINE JET

Outlet guide vanes

Fan and low pressure compressor geared to low speed spool of gas turbine engine

Turbomachine rotor rotating system and turbomachine rotor

Fan blade for a gas turbine engine

OIL SUPPLY ARRANGEMENT FOR BEARING

Fan comprising an inter-blade platform attached upstream by a ferrule

LOW NOISE COMPRESSOR AND TURBINE FOR GEARED TURBOFAN ENGINE

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

Thermal management system

Fan assembly having flow recirculation circuit with guide vanes

Fan assembly having flow recirculation circuit with rotating airfoils

STRUCTURAL ASSEMBLY FOR A GAS TURBINE ENGINE

Gas turbine engine airfoil

Hydraulic system

Deployable fairing for door reversers systems and methods

Turbomachine assembly

Noise reducing gas turbine engine airfoil

Platform apparatus for propulsion rotor

Frangible gas turbine engine airfoil with layup change

Frangible gas turbine engine airfoil

WINDAGE SHIELD SYSTEM FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINE

Gas turbine engine

Concentric turbomachine with electric machine

Turbofan arrangement with blade channel variations

HIGH THRUST GEARED GAS TURBINE ENGINE

Method for producing a shielding cartridge for a turbomachine element and corresponding shielding cartridge and turbomachine element

Containment case active clearance control structure

Low-pitch variable-setting fan of a turbine engine

Variable bypass ratio fan with variable pitch aft stage rotor blading

Fan blade having closed metal sheath

Attachment of piloting feature

Fan blade refurbishment training device

Stabilization bearing system for geared turbofan engines

Abrasive tip blade manufacture methods

Casing having a non-axisymmetric composite wall

Turbomachinery transition duct for wide bypass ratio ranges

Superconducting ultra power efficient radial fan augmented nano-aerodrive (superfan)

Turbine blade, turbocharger, and method of producing turbine blade

Shape memory alloy variable stiffness airfoil

Method and system for elastic bearing support

Aircraft fan with low part-span solidity

Fan blade attachment root with improved strain response

Gas turbine engine with geared architecture

Split sleeve hidden door thrust reverser

GEARED TURBOFAN WITH HIGH GEAR RATIO AND HIGH TEMPERATURE CAPABILITY

Stator configuration for gas turbine engine

Offset cores for gas turbine engines

Fan case with interleaved layers

Variable pitch fan actuator

Short inlet with low solidity fan exit guide vane arrangements

Stiffened platform

Attachment of structures having different physical characteristics

Fan case assembly for gas turbine engine

Fan platform wedge seal

AIRCRAFT ENGINE FAN

Gas turbine engine nose cone assembly

Relative position measurement

Nacelle

Efficient, low pressure ratio propulsor for gas turbine engines

Fan drive gear system mechanical controller

NON-SYMMETRIC FAN BLADE TIP CLADDING

Geared turbofan engine with targeted modular efficiency

System and method for fan blade rotor disk and gear inspection

Gear and gas turbine engine

Single ply having plurality of fiber angles

Fan blade repair fixture and method of repair

Noise reduction apparatus and jet fan

Gas turbine engine fan platform

Fan spacer for a gas turbine engine

Elongated geared turbofan with high bypass ratio

Fan for a turbomachine

Oil baffles in carrier for a fan drive gear system

Turbine engine blade with leading edge strip

Reinforced composite blade and method of making a blade

High efficiency centrifugal impeller with balancing weights

Wear liner installation tool

Composite nosecone

Geared architecture turbofan engine thermal management system and method

FAN DISC ASSEMBLY

FAN DISC ASSEMBLY

FAN DISC ASSEMBLY

Method and system for improving turbine blade performance

Apparatus and method for selective bonding to form hollow components

Fan blade with filled pocket

Assembly for releasable locking of a spinner or nosecone to an engine structure

Integral stiffening rail for braided composite gas turbine engine component

Heat dissipation system for electric aircraft engine

Power takeoff transmission

Damping device

Fan track liner

Modulation of vane end serrations

Turbomachinery blade and method of fabricating

Turbine engine assembly comprising a nose cone and a front shroud

Composite fan platform lug reinforcement

Fairing ring for a bladed wheel

Turbofan engine's fan blade and setting method thereof

Pylon of a propulsion unit

THREE SPOOL TURBOFAN ENGINE WITH LOW NOISE INTERMEDIATE TURBINE ROTOR

Geared turbofan with four star/planetary gear reduction

Partially shrouded gas turbine engine fan

Fan assembly of a gas turbine engine with a tip shroud

Annulus filler

OGV electroformed heat exchangers

CORE FOR HIGH-TEMPERATURE SHAPING OF A METAL PART AND MANUFACTURING PROCESS

Fan casing with annular shell