Blade tip

Fan rotor with thickened blade root

Gas turbine engine airfoil

Gas turbine engine

Gas turbine engine airfoil

Gas turbine engine airfoil

Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion

Gas turbine engine including vane structure and seal to control fluid leakage

Gas turbine engine with distributed fans

Fan drive gear system module and inlet guide vane coupling mechanism

Fan rotor, in particular for a turbine engine

Cylindrical case and manufacturing method of cylindrical case

Gas turbine engine

Leading edge protector

Attachment of structures having different physical characteristics

Fan blade with variable thickness composite cover

Sliding nozzle flap assembly

Turbomachine vane having an airfoil designed to provide improved aerodynamic and mechanical properties

Metal leading edge protective strips for airfoil components and method therefor

Geared turbofan with a gearbox upstream of a fan drive turbine

Joint between components

Fan having a variable setting by means of differential rotation of the fan disks

Airplane turbojet fan blade of cambered profile in its root sections

Low noise compressor rotor for geared turbofan engine

Gas turbine engine

Geared turbofan engine gearbox arrangement

Pivoting fan track liner for blade retainment

Injection molded composite fan platform

Low profile fan platform attachment

Turbofan engine main bearing arrangement

Gas turbine engine inlet wall design

Fan nozzle drive systems that lock thrust reversers

Turbomachine rotor blade

GAS TURBINE ENGINE BUSHING

Hollow component manufacture

Wear pad to prevent cracking of fan blade

Fan rotor blade of aircraft jet engine

Fan rotor blade of aircraft jet engine

Fan blade root integrated sealing solution

Fan casing arrangement for a gas turbine engine and related method

Turbine engine vane with asymmetrical profile

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

ACOUSTIC LINER

Turbojet fan blade

Method for repairing a blade

Gas turbine engine and electric machine

Fiber structure woven as a single piece by 3D weaving and application to the manufacturing of composite material part

Thrust efficient turbofan engine

Steam turbine bearing support structure and steam turbine thereof

Thrust efficient turbofan engine

Gas turbine engine fan blade airfoil profile

Hybrid turbine blade including multiple insert sections

Gas turbine engine geared architecture axial retention arrangement

Integral fan blade wear pad and platform seal

Exhaust nozzle for an elongated gear turbofan with high bypass ratio

Elongated geared turbofan with high bypass ratio

Thrust efficient turbofan engine

Fan blades for gas turbine engines with reduced stress concentration at leading edge

Fan spacer having unitary over molded feature

Hybrid spinner support

Dual rotor blades having a metal leading airfoil and a trailing airfoil of a composite material for gas turbine engines

Fan track liner designed to yield next to fan case hook

Bifurcated inlet scoop for gas turbine engine

Under-root spacer for gas turbine engine fan blade

System for changing the pitch of the blades of a propeller

Gas turbine engine nose cone attachment configuration

Method of making protective reinforcement for the leading edge of a blade

Hydraulic system for controlling the orientation of fan blades

Non-integral fan blade platform

Adhesive pattern for fan case conformable liner

Rotor blade root spacer for arranging between a rotor disk and a root of a rotor blade

Lightweight shrouded fan blade

Redundant airfoil attachment

Grounding for fan blades on an underblade spacer

Bi-directional compression fan rotor for a gas turbine engine

Airfoil with galvanic corrosion preventive shim

Reduced trim flow gas turbine engine oil system

METHOD AND SYSTEM FOR FABRICATING COMPOSITE CONTAINMENT CASINGS

Composite flange from braided preform

Turbomachine rotor with a means for axial retention of the blades

Hollow fan blade with honeycomb filler

Electrical grounding for blades

Electrical grounding for blade sheath

Compressor blade of a gas turbine as well as method for manufacturing said blade

Composite turbine engine blade with structural reinforcement

Axial retention for fasteners in fan joint

Method of Manufacturing Fan Blade Shields

Fairing assembly

Fan blade platform

System for attaching a turbojet engine spinner

Front bearing support for a fan drive gear system

Airfoil cover system

Fan rotor and associated turbojet engine

Blade dovetail bottom

Hollow fan bladed with braided fabric tubes

Gas turbine engine geared architecture axial retention arrangement

Geared turbofan with three co-rotating turbines

Fan blade and method of manufacturing same

Diffuser seal for geared turbofan or turboprop engines

COMPOSITE AIRFOIL WITH LOCAL TAILORING OF MATERIAL PROPERTIES

Gas turbine engine driving multiple fans

METHOD OF APPLYING LIQUID ADHESIVE TO A SURFACE OF A METALLIC FAN BLADE

GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE

Fastening system for fan and shaft interconnection

Fan and boost joint

CONFORMAL LINER FOR GAS TURBINE ENGINE FAN SECTION

Clearance control for gas turbine engine section

Hydraulic device for changing the pitch of a propeller

Hollow airfoil construction utilizing functionally graded materials

Fan blade attachment of gas turbine engine

Gas turbine rotary blade with tip insert

Fan case rub system, components, and their manufacture

Nacelle

Internally cooled spoke

SPEED SENSOR PROBE LOCATION IN GAS TURBINE ENGINE

COMPRESSOR FLOWPATH

GEARED TURBOMACHINE FAN AND COMPRESSOR ROTATION

Air recovery system for precooler heat-exchanger

Aluminum fan blade construction with welded cover

Airfoils for wake desensitization and method for fabricating same

Fan blade with composite core and wavy wall trailing edge cladding

Airfoils including tip profile for noise reduction and method for fabricating same

Method for Reducing Stress on Blade Tips

Gas turbine engine with fan variable area nozzle to reduce fan instability

Fan rotor blade and fan

Blade for a gas turbine engine

GAS TURBINE ENGINE WITH VARIABLE PITCH FIRST STAGE FAN SECTION

Gas turbine engine with two-spool fan and variable vane turbine

Airfoil devices, leading edge components, and methods of making

Hollow fan blade channel configuration to reduce stress

Fan blade channel termination

Fan blade having internal rib break-edge

HOLLOW FAN BLADE RIB GEOMETRY

ABRADABLE PANEL AND METHOD OF FORMING THE SAME

Fan case thrust reverser

Metallic fan blade platform

STRUCTURAL COMPOSITE FAN EXIT GUIDE VANE FOR A TURBOMACHINE

Torque frame and asymmetric journal bearing for fan drive gear system

Gas turbine engine fan variable area nozzle with swivable insert system

Method of treating an aerofoil

Gas turbine engine with low stage count low pressure turbine

Subsonic swept fan blade

Fan blade protection system

INNER PERIPHERAL SURFACE SHAPE OF CASING OF AXIAL-FLOW COMPRESSOR

Journal pin for gear system

Hybrid metal fan blade

Turbine engine fan disk

Gas turbine engine module adapter to a carrier

Gas turbine engine lubrication

Turbomachine rotor with anti-wear shim between a disk and an annulus

Coupling shaft for gas turbine fan drive gear system

ROTOR HAVING AN ANNULUS FILLER

EPICYCLIC GEAR TRAIN

Epicyclic gear train

GAS TURBINE ENGINE GEAR TRAIN

Gas turbine engine with geared architecture

Gas turbine engine gear train

GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO

GAS TURBINE ENGINE WITH GEARED ARCHITECTURE

Gas turbine engine with low fan pressure ratio

GAS TURBINE ENGINE WITH GEARED ARCHITECTURE

Prestressing device having circumferential activity

GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY

Annulus filler

Twelve-hour structure for thrust reverser, in particular with grids

INTERDEPENDENT LUBRICATION SYSTEMS

Gas turbine engine with axial movable fan variable area nozzle

Fan blade with winglet

Gas turbine engine having fan blades of adjustable pitch with cyclic setting

Composite vane mounting

Composite vane mounting

Fan case assembly and method

Rotor blade of a gas turbine engine made of composite material comprising a connecting yoke, method for manufacturing the blade

AUXILIARY HYDRAULIC POWER GENERATION SYSTEM

Thrust reverser for a turbofan engine nacelle

Non-integral platform and damper for an airfoil

COMPOSITE LEADING EDGE SHEATH AND DOVETAIL ROOT UNDERCUT

Composite fan blade dovetail root

PANELLED ASSEMBLY

Method and system for a leakage controlled fan housing

CO-CURED SHEATH FOR COMPOSITE BLADE

Annulus filler assembly for a rotor of a turbomachine

GAS TURBINE ENGINE WITH AN ARRANGEMENT FOR MEASURING THE SHAFT ROTATION SPEED

Annulus filler for a gas turbine engine

Composite load-bearing rotating ring and process therefor

Annulus filler element for a rotor of a turbomachine

Fan

Containment casing for an aero engine

Aerofoil blade assembly

Rotor blade with reduced rub loading

Annulus filler for a gas turbine engine

Air intake for aircraft nacelle, and propulsion assembly including such air intake

Reinforced composite fan blade

Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing

METHOD OF MANUFACTURING A COMPONENT COMPRISING AN INTERNAL STRUCTURE

Variable drive gas turbine engine

Linear telescopic actuator for moving a first and a second element relative to a stationary element

Fan blade anti-fretting insert

Fan blade platform

TURBOFAN ENGINE

Heat exchanger to cool turbine air cooling flow

Transonic airfoil and axial flow rotary machine

Gas turbine engine fan variable area nozzle with swivalable insert system

Variable fan nozzle using shape memory material

Fan rotor blade support structure and turbofan engine having the same

Fan casing for a gas turbine engine

PROPULSOR DEVICES HAVING VARIABLE PITCH FAN BLADES WITH SPHERICAL SUPPORT AND DAMPING SURFACES

Fan blade retention and variable pitch system

Fan rotor for a turbomachine or a test engine

FAN BLADE

FAN VARIABLE AREA NOZZLE WITH ADAPTIVE STRUCTURE

AXIAL FLOW FLUID DEVICE

Systems and methods involving localized stiffening of blades

Gas turbine engine systems involving tip fans

Thrust reverser for a turbofan gas turbine engine

Thrust reverser door

Gas turbine engine with variable geometry fan exit guide vane system

Aircraft turbomachine fan comprising a balancing flange concealed by the inlet cone

Damping device for composite blade

Component with a damping filler

Component with a damping filler and method

Method of forming an aerofoil with a damping filler

FAN BLADE RETAINING STRUCTURE

FAN BLADE RETAINING STRUCTURE

Method and system for cooling fluid in a turbine engine

Airfoil acoustic impedance control

BLADE ATTACHMENT RETENTION DEVICE

Variable rotor blade for gas turbine engine

Linkage system with wear reduction

Turbomachine with a deflector system

Turbomachine fan

Fan blade made of a textile composite material

Methods and apparatus for fabricating a fan assembly for use with turbine engines

Guide Vane and Method of Fabricating the Same

Fan blade for a gas-turbine engine

Interdependent lubrication systems in a turbine engine

Turbomachine blade

Tip cambered swept blade

Aircraft engine

Hollow fan blade for gas turbine engine

Turbofan gas turbine engine with variable fan outlet guide vanes

Systems and methods for monitoring thermal growth and controlling clearances, and maintaining health of turbo machinery applications

Compressor comprising a plurality of cells reconstituting an annular volume of separation of flows in a turbine engine

Hollow fan blade for gas turbine engine

Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes

Nonlinearly stacked low noise turbofan stator

Fan driven emergency generator

Universal Carnot propulsion systems for turbo rocketry

Damped assembly

Coated journals

Hollow fan blade for gas turbine engine

Hollow fan blade for gas turbine engine

Hollow fan blade for gas turbine engine

Hollow fan blade for gas turbine engine

Method for making a hollow fan blade with machined internal cavities

Variable stator vane arrangement for a compressor

Variable cam exhaust nozzle

Noise attenuator arrangement

Casing, a compressor, a turbine, and a combustion turbine engine including such a casing

Reinforced fan blade

Gas turbine engines including splittered airfoils

Trunnions having multiple fan blades for use with an aircraft engine

Fan blade assembly with leading edge fillet

Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes

Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes

Fibrous texture for a casing made of composite material with reinforced flanges

Epicyclic gear reduction carrier and torque frame connection

Fan with variable depth groove casing treatment

Turbine engine having a variable engine intake system

Compliant dampening wedge mount

Variable pitch fan blade retention system

Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance

Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes

Preventing abnormal fan blade deflection or fan flutter with retroreflectors

Root block design for composite fan blade

Gas turbine engine with hybrid fan exit guide vanes

Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance

Containment ring for gas turbine engine

Gas turbine engine having cooling systems

Distributed electrical generators for turbofan engines

Outer nacelle with inlet guide vanes and acoustic treatment

Turbine engine fan case with bleed air for tip injection and heat exchanger cooling

Variable pitch airfoil assembly for an open fan rotor of an engine having a damping element

Guide vane assembly with fixed and variable pitch inlet guide vanes

Gas turbine engine with forward swept outlet guide vanes

Gas turbine engine with fan track liner having triply periodic minimal surface reinforcement

Turbine engine with fan bypass water injection to augment thrust

Airfoil-mounted acoustic resonator array for gas turbine engine component

Component mounting and drive in a geared turbofan architecture

Fan drive gear system gutter ejector system

Rotating carrier oil manifold

Airfoil assembly with a trunnion and spar

Nose cone/spinner power takeoff

Adjustable depth tip treatment with axial member with pockets for a fan of a gas turbine engine

Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine

Adjustable depth tip treatment with rotatable ring with pockets for a fan of a gas turbine engine

Adjustable air flow plenum with sliding doors for a fan of a gas turbine engine

Blade spacer

Rotor blade inspection system

Rotor blade inspection system