VARIABLE PITCH FAN BLADE RETENTION SYSTEM

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

FAN WITH VARIABLE DEPTH GROOVE CASING TREATMENT

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

DAMPED FAIRING ASSEMBLY

GAS TURBINE ENGINE HAVING A SENSOR ASSEMBLY FOR MONITORING PROPELLER WHIRL

GEARED TURBOMACHINE FAN AND COMPRESSOR ROTATION

MULTIPLE LOADS PATHS FOR VIBRATION MITIGATION AND IMPROVED TIP CLEARANCE IN TURBOFAN ENGINE

ADDITIVE FAN EXIT GUIDE VANE STRUCTURE WITH ACOUSTIC CAPABILITY

BOOSTER ROTORS AND METHODS OF OPERATING GAS TURBINE ENGINES

GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO

GAS TURBINE ENGINE HAVING COMPOSITE FAN BLADES

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

GAS TURBINE ENGINE

TURBINE ENGINE HAVING A FAN SPEED SENSOR SYSTEM

LIFT FAN ASSEMBLY FOR AN AIRCRAFT

EFFICIENT AIRCRAFT ENGINE

TURBINE ENGINE HAVING A VARIABLE ENGINE INTAKE SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

AIRFOIL ASSEMBLY

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

BLADE WITH COMPOSITE STRUCTURE HAVING IMPROVED PLY DROP ORIENTATION

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

GAS TURBINE ENGINE

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

Containment Case for Gas Turbine Engine

TURBINE ENGINE HAVING A PLURALITY OF LUBRICANT STRUTS, EACH DEFINING A LUBRICANT STRUT FLOWPATH

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

FAN EXIT GUIDE VANE LOAD CARRYING TENSION MEMBER WITH DAMPER

Reinforced Fan Inter-Blade Platforms

TURBINE ENGINE INCLUDING A FAN BLADE SENSOR SYSTEM

COWL ASSEMBLY FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINE HAVING COMPOSITE FAN BLADES

NOSECONE FOR A DUCTED FAN GAS TURBINE ENGINE

VARIABLE PITCH FAN BLADE RETENTION SYSTEM

AIRFOILS HAVING INTERNAL VIBRATIONAL DAMPERS

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

PUMP SYSTEMS HAVING DUAL-FUNCTION HEAT EXCHANGERS AND RELATED METHODS

SENSOR ASSEMBLY TO DETECT PROPELLER WHIRL IN A TURBINE ENGINE

CRUSHABLE BEARING RING FOR A FAN ASSEMBLY

TURBINE ENGINE AIRFOIL WITH A WOVEN CORE

TURBINE ENGINE WITH COMPOSITE AIRFOILS

FAN EXIT GUIDE VANE WITH LOAD CARRYING TENSION MEMBER

PARTIAL EXIT CENTRIFUGAL COMPRESSOR

FIBROUS TEXTURE FOR A CASING MADE OF COMPOSITE MATERIAL WITH REINFORCED FLANGES

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

AIRCRAFT ENGINE

TURBINE ENGINE WITH COMPOSITE AIRFOILS

GAS TURBINE ENGINE

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

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

GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES

PREVENTING ABNORMAL FAN BLADE DEFLECTION OR FAN FLUTTER WITH RETROREFLECTORS

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

ELONGATED JOURNAL BEARING FOR HIGH GEAR RATIO EPICYCLIC FAN DRIVE GEAR SYSTEM

ENGINE SYSTEM FOR AN AIRCRAFT

SINGLE SPOOL GEARED TURBOFAN

GAS TURBINE ENGINE WITH THIRD STREAM

COST-EFFECTIVE SOLID-STATE DEPOSITION OF FUNCTIONALLY GRADED TITANIUM HOLLOW FAN BLADE SHEATH FOR IMPROVED GALVANIC CORROSION RESISTANCE

BLADE WITH COMPOSITE STRUCTURE HAVING IMPROVED PLY DROP ORIENTATION

MOUNTING ASSEMBLY FOR A GEARBOX ASSEMBLY

GAS TURBINE ENGINE HAVING COOLING SYSTEMS

MODULATED AIR-COOLED HEAT EXCHANGER FOR HYBRID ELECTRIC THERMAL MANAGEMENT SYSTEMS

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

CONTAINMENT RING FOR GAS TURBINE ENGINE

GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES

GAS TURBINE ENGINE HAVING COOLING SYSTEMS

AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENT

FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY

HIGH POWER EPICYCLIC GEARBOX AND OPERATION THEREOF

GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO

GAS TURBINE ENGINE HAVING COMPOSITE FAN BLADES

METALLIC BLADE SPAR RETENTION SYSTEM

TURBINE ENGINE WITH COMPOSITE AIRFOILS

HYDROGEN LIQUID OXYGEN COMBINED CYCLE ENGINE

Vane Assembly For Open Fan Engine

GAS TURBINE ENGINE

GEARBOXES FOR AIRCRAFT GAS TURBINE ENGINES

AIRFOIL-MOUNTED ACOUSTIC RESONATOR ARRAY FOR GAS TURBINE ENGINE COMPONENT

AERONAUTICAL PROPULSION SYSTEM COMPRISING AN OPTIMIZED FAN SECTION

COMPONENT MOUNTING AND DRIVE IN A GEARED TURBOFAN ARCHITECTURE

COMPRESSION IN A GAS TURBINE ENGINE

OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE

AIRCRAFT PROPULSION SYSTEM WITH ASYMMETRIC EXHAUST ASSEMBLY

SENSOR ASSEMBLY TO DETECT PROPELLER WHIRL IN A TURBINE ENGINE

GUIDE VANE ASSEMBLY WITH FIXED AND VARIABLE PITCH INLET GUIDE VANES

AIRFOIL VIBRATION DAMPING APPARATUS

TURBINE ENGINE HAVING A FIRE BOX

TURBINE-POWERED SYSTEM WITH THERMOELECTRIC COOLING

BLADE CONFIGURED FOR IMPACT TOLERANCE

GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES

GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES

ONCE PER REVOLUTION SIGNAL OPTICAL INSPECTION SYSTEM

TURBOFAN ENGINE HAVING A LOW-PRESSURE TURBINE

UNBALANCED ROTOR FOR UNBALANCE TESTING OF AIRCRAFT POWER PLANT

AIRCRAFT ENGINE

HEAT EXCHANGER

GAS TURBINE ENGINE FRONT SECTION

COMPOSITE AIRFOIL ASSEMBLY FOR A TURBINE ENGINE

Fan drive gear system rotating oil baffle

AIRCRAFT

SYSTEM AND METHOD FOR DETECTING AND REDUCING TORQUE IN A TURBINE ENGINE

TOWER SHAFT DRIVEN PLANETARY FAN DRIVE GEAR LUBRICATION SYSTEM

TURBOMACHINE MODULE EQUIPPED WITH VARIABLE PITCH VANES AND AN ANNULAR INTERFACE SHROUD

OPTICAL DEFECT DETECTION SYSTEM

GEARBOXES FOR AIRCRAFT GAS TURBINE ENGINES

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

ELONGATED JOURNAL BEARING FOR HIGH GEAR RATIO EPICYCLIC FAN DRIVE GEAR SYSTEM

Fan assembly for an engine having redundant trunnion retention

EPICYCLIC GEAR TRAIN

TURBINE ENGINE WITH COMPOSITE AIRFOILS

GAS TURBINE ENGINE HAVING A SENSOR ASSEMBLY FOR MONITORING PROPELLER WHIRL

Vane assembly for open fan engine

MOUNTING ASSEMBLY FOR A GEARBOX ASSEMBLY

BLADE FOR A DUCTED FAN OF A TURBOMACHINE

Module for mounting a turbomachine fan blade

Hydrogen liquid oxygen combined cycle engine

HIGH POWER EPICYCLIC GEARBOX AND OPERATION THEREOF

OBJECT DIRECTION MECHANISM FOR TURBOFAN ENGINE

BLADE SPACER

GAS TURBINE ENGINE

FAN ASSEMBLIES WITH FAN DISK INSERTS AND METHODS OF ASSEMBLING THE SAME

LIGHT WEIGHT FAN CASING CONFIGURATIONS FOR ENERGY ABSORPTION

Turbine engine having an airfoil assembly with a trunnion and a spar

Differentiated shortening of strands of the fibrous reinforcement of a fan blade

GAS TURBINE AIRFOIL NOISE REDUCTION

TURBINE ENGINE WITH COMPOSITE AIRFOILS

ANNULUS FILLER FOR A GAS TURBINE ENGINE

ROTOR BLADE INSPECTION SYSTEM

GAS TURBINE ENGINE

TURBINE ENGINE WITH COMPOSITE AIRFOILS

Compressor with anti-ice inlet

VARIABLE PITCH FAN

GAS TURBINE ENGINE COMPRESSION SYSTEM WITH CORE COMPRESSOR PRESSURE RATIO

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH SEGMENT INTERFACE COMPONENTS

Segmented variable fan outlet guide vane with cam assembly and unique actuation mechanisms

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH UNIQUE ACTUATION MECHANISMS

SEGMENTED VARIABLE FAN OUTLET GUIDE VANE WITH CAM ASSEMBLY AND PASS THROUGH ACTUATION MECHANISMS

TURBINE ENGINE AIRFOIL WITH A WOVEN CORE

HOUSING FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR HOUSING MANUFACTURE

Method for manufacturing a composite blade for a turbine engine, the blade comprising a reinforcing shield for balancing the blade

Turbine engine with composite airfoils

FAN ASSEMBLY HAVING A FAN RETENTION MEMBER FOR SUPPORTING A BLADE PLATFORM

VARIABLE PITCH FANS FOR TURBOMACHINERY ENGINES

PLATFORM FOR A FAN ASSEMBLY

VARIABLE PITCH FAN OF A GAS TURBINE ENGINE

ASSEMBLY FOR A TURBOMACHINE BLADE, COMPRISING A FASTENER, DEFINING A POCKET, AND A SHIM ADAPTED TO BE RECEIVED IN THE POCKET AT THE SAME TIME AS A ROOT OF THE BLADE

Aircraft propulsion system having a nacelle equipped with an improved articulation system

Direct drive electrically-geared turbofan

OUTLET GUIDE VANES AND AN ACCESSORY DRIVE GEARBOX FOR A GAS TURBINE ENGINE

Turbofan provided with a fastening assembly arranged on a fan casing

Object direction mechanism for turbofan engine

Outlet guide vane assembly for a turbofan engine

Aeronautical propulsion system

Gearboxes for aircraft gas turbine engines

ASSEMBLY FOR A TURBINE ENGINE FAN CASE AND AN AIR INLET, METHOD FOR USING SUCH AN ASSEMBLY

Efficient aircraft engine

Fan module equipped with an oil-transfer device

Compression in a gas turbine engine

Vane comprising a structure made of composite material, and associated manufacturing method

FAN CASE ASSEMBLY OF TURBO FAN ENGINE

Fan module equipped with an oil transfer device

GAS TURBINE ENGINE WITH THIRD STREAM

Fan module provided with an oil transfer device

Engine backbone bending reduction

Fan blade for a gas turbine engine

ASSEMBLY FOR A TURBOMACHINE BLADE, COMPRISING A FASTENER, DEFINING A POCKET, AND A SHIM ADAPTED TO BE RECEIVED IN THE POCKET AT THE SAME TIME AS A ROOT OF THE BLADE

PUMP SYSTEMS HAVING DUAL-FUNCTION HEAT EXCHANGERS AND RELATED METHODS

Platform for an airfoil of a gas turbine engine

Aviation turbofan engine and fan duct nozzle

Air bottoming cycle driven propulsor

Bypass turbofan including a system for blocking the secondary flow including veils

GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM

Sealing device for a discharge valve of a turbomachine

Gearboxes for aircraft gas turbine engines

Hybrid Composite Components

Engine mount system for a gas turbine engine

Method for manufacturing a composite platform for a fan of an aircraft turbine engine

Selective power distribution for an aircraft propulsion system

Integrated hybrid propulsion system

DUCTED TURBOMACHINERY ENGINES

Stator configuration for gas turbine engine

Stator assembly

FAN BLADE OR VANE WITH IMPROVED BIRD IMPACT CAPABILITY

Fan for a turbine engine

Geared turbine engine with relatively lightweight propulsor module

Composite vane for an aircraft turbine engine

GAS TURBINE ENGINE

GAS TURBINE ENGINE

Hydrogen electric hybrid power plant for hovercar and control method

THERMAL TRANSPORT BUS CAPACITY FOR A THERMAL TRANSPORT BUS IN A TURBOFAN ENGINE

Blade comprising a shield having a defrosting air passage duct

Cowl assembly for a gas turbine engine

Rotating airfoil assembly for an aircraft engine

Rotating airfoil with a spring damper system

Blade made of composite material comprising a leading edge shield, turbine engine comprising the blade

POLYMERIC FOAMS FOR HOLLOW CAVITIES

Gas turbine engine fan

PORTABLE AND WEARABLE HAND-GRASP NEURO-ORTHOSIS

Actuation assembly for a fan of a gas turbine engine

Assembly for an aircraft turbine engine, comprising means for the axial and radial retention of a fan

Electrical connection of an electrical machine in an aircraft turbine engine

Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine

Heat transfer system for gas turbine engine

Gearboxes for aircraft gas turbine engines

Compressor flowpath

High and low spool configuration for a gas turbine engine

Epicyclic gear train

System and Method for Manufacture of Abrasive Coating

High power epicyclic gearbox and operation thereof

AIRCRAFT ENGINE

Levered counterweight feathering system

Metallic structures with additively manufactured metallic articles and methods for fabrication

SUPERCONDUCTING ULTRA POWER EFFICIENT RADIAL FAN AUGMENTED NANO-AERO DRIVE (SUPERFAN)

High fan tip speed engine

Composite fan case containment hook and improved forward debris capture

Gas turbine engine compression system with core compressor pressure ratio

Injection tooling for barrel-shaped rotating part

Compression in a gas turbine engine

Platform for a fan rotor of an aircraft turbomachine

Morphing structures for fan inlet variable vanes

Aircraft having a single fluid inlet aperture

Fan case assembly for a gas turbine engine

Turbine engine fan case with manifolded tip injection air recirculation passages

Part of a gas turbine engine and method for the manufacturing the part

AIRFOIL VIBRATION DAMPING APPARATUS

ROTATABLE AEROFOIL COMPONENT WITH Z-PINS

Aircraft engine attachment assembly

Geared turbomachine fan and compressor rotation

Gas turbine engine

Gas turbine engine

Gas turbine engine with a defined fan axis angle between a fan tip axis and a centerline

Geared turbofan engine with targeted modular efficiency

RADIAL STRUT FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE

Aircraft turbine engine with an off-axis propeller

Compressor flowpath

Gearbox configurations for clockwise and counterclockwise propeller rotation

Variable pitch fans for turbomachinery engines

Stator configuration for gas turbine engine

STRADDLE MOUNTED LOW PRESSURE COMPRESSOR

Fibrous texture for turbine engine blade made of composite material

Methods involving and apparatuses for a turbine engine fairing

Composite platform for a fan of an aircraft turbine engine

Turbomachine module equipped with an electric machine rotor

Method for manufacturing a composite platform for an aircraft turbine engine fan

FAN BLADE ASSEMBLY WITH MIDSPAN SHROUD

Automatic blade pitch control

Inlet for unducted propulsion system

Variable pitch fan assembly with remote counterweights

GAS TURBINE ENGINE WITH THIRD STREAM

Gearboxes for aircraft gas turbine engines

Retaining ejected gas turbine blades

Planetary gearbox

Object direction mechanism for turbofan engine

Composite fan blade airfoil, methods of manufacture thereof and articles comprising the same

STATOR APPARATUS FOR A GAS TURBINE ENGINE

Morphing structures for fan inlet variable vanes

Gas turbine engine front section

High fan up speed engine

Roller bearing arrangement for a gas turbine engine

GAS TURBINE ENGINE INLET

Fan icing detection system

High and low spool configuration for a gas turbine engine

TURBOFAN COMPRISING A SERIES OF ROTARY BLADES FOR CLOSING OFF THE DUCT FOR THE SECONDARY STREAM

FRANGIBLE AIRFOIL

Composite airfoils with frangible tips

Methods and apparatus to detect air flow separation of an engine

Levered counterweight feathering system

Turbomachines and epicyclic gear assemblies with lubrication channels

GEARBOX AND GAS TURBINE PROPULSION UNIT

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

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

Gearboxes for aircraft gas turbine engines

Hybridization of the fibers of the fibrous reinforcement of a fan blade

Deployable fairing for door reversers systems and methods

THREE-STREAM GAS TURBINE ENGINE WITH EMBEDDED ELECTRIC MACHINE

Light weight fan casing configurations for energy absorption

Preform for a composite blade

Airfoil for a gas turbine engine

Turbomachine polyspherical hub for variable pitch blades

Engine having variable pitch outlet guide vanes

Variable pitch fan assembly with remote counterweights

Shape memory alloy variable stiffness airfoil

High power epicyclic gearbox and operation thereof

HYBRID COMPOSITE COMPONENTS

Damping device

Gearboxes for aircraft gas turbine engines

Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contact

Gas turbine engine airfoil fairing with rib having radial notch

Method to strip coatings off of an aluminum alloy fan blade

Planetary gearbox