Dual alloy blade

ROTOR ASSEMBLY FOR A TURBOMACHINE AND A METHOD OF MANUFACTURING THE SAME

Moving Blade and Turbine Using Moving Blade

TURBINE AIRFOIL COOLING SYSTEM WITH INTEGRATED AIRFOIL AND PLATFORM COOLING SYSTEM

Systems and Methods for Monitoring Components

Lockwire Tab Backcut For Blade Stress Reduction (9E.04)

Method of mounting rotor blades on a rotor disk, and clamping device for performing such a method

Margin bucket dovetail radial support feature for axial entry buckets

Method for determining vibratory contact stress at a blade attachment

Low profile fan platform attachment

Fan blade pitch setting

Gas turbine engine having a vane assembly

Vane with spoiler

Blade

Turbine rotor assembly, turbine, and rotor blade

Fan blade removal feature for a gas turbine engine

Blade with a platform and a hollow bumper

Removal tool

Rotor, axial compressor, installation method

Blade positioning

Ultrasonic flaw-detection method and apparatus for blade groove in turbine rotor disc

Turbine rotor blade

Turbine bucket lockwire anti-rotation device for gas turbine engine

Mobile vane for a turbine engine, comprising a lug engaging in a locking notch of a rotor disk

Curved blade retention slot for turbine blade in a turbine disk

Gas turbine engine airfoil

Load absorption systems and methods

MODULAR TURBINE BLADE WITH SEPARATE PLATFORM SUPPORT SYSTEM

Rotary assembly for a turbomachine

Rotor for turbine engine comprising blades with added platforms

Turbine blade attachment curved rib stiffeners

Turbine blade attachment rails for attachment fillet stress reduction

BLADE OF A TURBOMACHINE HAVING BLADE ROOT THERMAL INSULATION

Compressor aft rotor rim cooling for high OPR (T3) engine

METHODS FOR MOUNTING A TURBINE SUBCOMPONENT TO A TURBINE COMPONENT

THERMAL SHIELDING IN A GAS TURBINE

Tool and method for installing turbomachine component

Seal-plate anti-rotation in a stage of a gas turbine engine

Gas turbine engine with short inlet and mistuned fan blades

Damper seal installation features

Disk assembly and turbine including the same

Mounting of vanes at the periphery of a turbine engine disc

Airfoil platform having dual pin apertures and a vertical stiffener

Platform for an airfoil having bowed sidewalls

Ductile compensation layer for brittle components

Rotationally symmetrical part for a turbine engine rotor, and related turbine engine rotor, turbine engine module, and turbine engine

Blade for a turbomachine impeller and method for modelling the same

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

Rotating structure and a method of producing the rotating structure

Turbine blade

LOW MODULUS INSERT FOR A COMPONENT OF A GAS TURBINE ENGINE

Variable pitch fan blade retention system

Fan platform for a gas turbine engine

Aviation turbine engine fan assembly including a fitted platform

RETAINING DEVICE FOR AXIALLY RETAINING A BLADE AND ROTOR DEVICE WITH SUCH A RETAINING DEVICE

Integrated strut and turbine vane nozzle arrangement

BLADE/DISK DOVETAIL BACKCUT FOR BLADE DISK STRESS REDUCTION (9E.04, STAGE 2)

Compliant layer for ceramic components and methods of forming the same

Flow control device for rotating flow supply system

Blade provided with platforms possessing attachment portions

Gas turbine cooling systems and methods

Turbine engine rotor lock

Assembling method of a bucket and a fixture for a bucket for a turbine blade

Underplatform damping members and methods for turbocharger assemblies

Rotor device of an aircraft engine with a damping device between turbines blades

Cooled turbine runner for an aircraft engine

Method and system for repairing turbomachine dovetail slots

Trunnion retention for a turbine engine

METHOD FOR COOLING A TURBOENGINE ROTOR, AND TURBOENGINE ROTOR

Ducted thrust producing system with asynchronous fan blade pitching

Rotary machines including a hybrid rotor with an integrally bladed rotor portion

Composite disk

Fan blade attachment root with improved strain response

Disk lug cooling flow trenches

Composite airfoil metal patch

Composite blade root stress reducing shim

TURBO ENGINE ROTOR COMPRISING A BLADE-SHAFT CONNECTION MEANS, AND BLADE FOR SAID ROTOR

Turbomachine component displacement apparatus and method of use

Fan blade with root through holes

Additive manufacturing system utilizing an epitaxy process and method of operation

Turbine dovetail slot heat shield

BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION FOR A SECOND STAGE OF A TURBOMACHINE

Blade, bladed wheel, turbomachine, and a method of manufacturing the blade

APPARATUS FOR MOUNTING A BLADE ON A TURBINE DISK

TURBINE BLADE RETENTION CONFIGURATION

Fan, in particular for a turbine engine

Airfoil device for a gas turbine and corresponding arrangement

Bladed rotor

Gas turbine engine damping device

GAS TURBINE ENGINE COMPONENT COOLING PASSAGE WITH ASYMMETRICAL PEDESTALS

Article of manufacture for turbomachine

Retaining rings for turbomachine disk and coverplate assemblies

METHOD OF ATTACHING A CERAMIC MATRIX COMPOSITE ARTICLE

Method for electro-chemical machining turbine wheel in-situ

Fixture for electro-chemical machining electrode

Faceted turbine blade damper-seal

Turbomachine bucket displacement apparatus and method of use

Sealing system and gas turbine

Chocking and retaining device

Chocking and retaining device

TURBINE BLADE

AIRFOIL AND METHOD FOR MANAGING PRESSURE AT TIP OF AIRFOIL

ROOT SPRING REMOVAL TOOL AND METHOD OF REMOVING A BLADE ROOT SPRING

Retention device

Ceramic attachment configuration and method for manufacturing same

Rotor blade vibration damper

Bucket mounted multi-stage turbine interstage seal and method of assembly

Locking element and turbomachine

Blade wedge attachment lay-up

Hybrid metal and composite spool for rotating machinery

Compressible fan blade with root spacer

Turbine blade, set of turbine blades, and fir tree root for a turbine blade

Gas turbine engine airfoil component platform seal cooling

Fan blade root

Rotary assembly for a turbomachine

CMC blade with monolithic ceramic platform and dovetail

Ply architecture for integral platform and damper retaining features in CMC turbine blades

Disk outer rim seal

Feature to provide cooling flow to disk

Blade attachment assembly

Metal leading edge on composite blade airfoil and shank

Fixture and method for installing turbine buckets

Turbine wheel with clamped blade attachment

Fan platform with leading edge tab

Flowpath boundary and rotor assemblies in gas turbines

FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES

FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES

Flowpath boundary and rotor assemblies in gas turbines

Gas turbine engine CMC airfoil assembly

Turbomachine rotor with optimised bearing surfaces

Turbine wheels with preloaded blade attachment

Radial lock for fan blade sheath

Blading member for a fluid flow machine

BLADING MEMBER FOR A FLUID FLOW MACHINE

Impeller having a radial seal for a turbine engine turbine

Turbine airfoil attachment with multi-radial serration profile

Dismantling device for blades and corresponding dismantling method

System and method for blade with protective layer

Apparatus having engineered surface feature and method to reduce wear and friction between CMC-to-metal attachment and interface

Abrasive flow media fixture with end contour

Platform of small hub-tip ratio

Turbine airfoil attachment with serration profile

Rotor disk assembly for a gas turbine engine

Snap in platform damper and seal assembly for a gas turbine engine

Turbine wheel cover-plate mounted gas turbine interstage seal

Composite blades for gas turbine engines

Composite components for gas turbine engines

Compliant layer for ceramic components and methods of forming the same

Turbomachine rotor assembly and method

Turbine wheel for a turbine engine

Bladed rotor disk including anti-vibratory feature

Apparatus and method for optimizing a test bed that is utilized for testing low cycle and high-cycle fatigue including modifying a support

Gas turbine engine with dove-tailed TOBI vane

Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method

Coating system including alternating layers of amorphous silica and amorphous silicon nitride

Coating system including oxide nanoparticles in oxide matrix

Slider for chocking a dovetail root of a blade of a gas turbine engine

Bladed rotor arrangement including axial projection

Bladed rotor arrangement and a lock plate for a bladed rotor arrangement

FAN BLADE WITH STATIC DISSIPATIVE COATING

GAS TURBINE ENGINE BLADE SLOT HEAT SHIELD

Gas turbine engine

Tangential blade root neck conic

Integrally bladed rotor

Repaired or remanufactured blade platform for a gas turbine engine

Gas turbine engine airfoil structure

Gas turbine engine rotor arrangement

Turbomachine blade assemblies

Fan blade grounding tab

Lightweight blade for gas turbine engine

Engine component having support with intermediate layer

Disk lug impingement for gas turbine engine airfoil

Reversible blade rotor seal

AXIAL FLOW COMPRESSOR AND GAS TURBINE EQUIPPED WITH AXIAL FLOW COMPRESSOR

FAN FOR A MULTI-FLOW TURBOSHAFT ENGINE, AND TURBOSHAFT ENGINE EQUIPPED WITH SUCH A FAN

Rotor blade with a conic spline fillet at an intersection between a platform and a neck

Blade wear pads and manufacture methods

ROTOR BLADE DOVETAIL WITH ROUND BEARING SURFACES

Turbine disk fatigue rejuvenation

Gas turbine engine rotor disk-seal arrangement

Fan blade dovetail and spacer

Co-formed element with low conductivity layer

Sealing features for a gas turbine engine

Aluminum Fan Blades with Root Wear Mitigation

HYBRID FAN BLADES FOR JET ENGINES

Fan disc

Damper mass distribution to prevent damper rotation

Turbine blade and damper retention

Rotor assembly for gas turbine

Rotor blade root spacer with grip element

Gas turbine engine nose cone attachment

Turbomachine rotor blade, turbomachine rotor disc, turbomachine rotor, and gas turbine engine with different root and slot contact face angles

FAN BLADE INCLUDING EXTERNAL CAVITIES

Fan blade positioning and support system for variable pitch, spherical tip fan blade engines

Turbine bucket assembly and turbine system

Developments in or relating to rotor balancing

Auxiliary device for welding spindle disks, having a damping belt, and friction welding method

Test blade

Variable dual spring blade root support for gas turbines

Turbomachine component displacement apparatus and method of use

Turbomachine bucket displacement apparatus and method of use

BLADE UNDERROOT SPACER WITH HOOK REMOVAL

Turbine rotor for a turbomachine

Method for manufacturing a turbine engine blade root of a composite material and blade root obtained by such a method

FIBER-REINFORCED TURBINE COMPONENT

Electrically grounding fan platforms

Root lightening holes with slot

Self-clamping fastener for CMC turbine blade

Propeller comprising a moveable dynamic scoop

Platform for ceramic matrix composite turbine blades

Fan rotor, in particular for a turbine engine

Composite turbine blade for high-temperature applications

Turbine engine blade removal apparatus and method

Turbine rotor assemblies with improved slot cavities

BLADE COMPRISING A SUPPORT, PROVIDED WITH A PORTION WITH A DEPRESSION

Turbine bucket closure assembly and methods of assembling the same

Process of producing a ceramic matrix composite turbine bucket, insert for a ceramic matrix composite turbine bucket and ceramic matrix composite turbine bucket

Turbine airfoil with laterally extending snubber having internal cooling system

Gas turbine

Low profile fan platform attachment

Mass offset for damping performance

Gas turbine engine rotor assembly and method of assembling the same

Method and systems for providing cooling for a turbine assembly

Adjustable blade root spring for turbine blade fixation in turbomachinery

Retainer plate

Turbine with bucket fixing means

Fan blade root integrated sealing solution

Castings, casting cores, and methods

Method and system for relieving turbine rotor blade dovetail stress

Rotor blade arrangement and gas turbine

Integrated strut and turbine vane nozzle arrangement

Gas turbine engines with turbine rotor blades having improved platform edges

Turbine blade and non-integral platform with pin attachment

Turbine system and adapter

Composite retention feature

Method for repairing wear marks on a rotor supporting the fan of a bypass engine

Turbomachine assembly alleviating stresses at turbine discs

Turbine blade or vane

Composite gas turbine engine blade having multiple airfoils

Compliant intermediate component of a gas turbine engine

Turbomachine rotor blade

Axial Turbomachine Compressor Drum with Dual Means of Blade Fixing

Turbine wheel in a turbine engine

Repair tool for a turbine rotor wheel, and a turbine rotor wheel

Turbine rotor blade for a turbine section of a gas turbine

Disk hoisting tool

Turbomachine vane cooperating with a vane retention disk

Rotor wheel for a turbine engine

Rotor blade assembly tool for gas turbine engine

Securement system and method for securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base

Turbine engine blade

Integral fan blade wear pad and platform seal

Systems and method for a composite blade with fillet transition

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

Axial compressor and method for controlling stage-to-stage leakage therein

Environmental severity measurement tool

Attachment feature of a gas turbine engine blade having a curved profile

System and method for attaching a rotating blade in a turbine

Drum rotor dovetail component and related drum rotor system

Turbine blade insertion tool

Under-root spacer for gas turbine engine fan blade

Rotor blade support structure

Low radius ratio fan for a gas turbine engine

Non-integral fan blade platform

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

Rotor blade root spacer with a fracture feature

Turbine under platform air seal strip

Apparatus having engineered surface feature and method to reduce wear and friction between CMC-to-metal attachment and interface

System for damping vibrations in a turbine

Blade root, corresponding blade, rotor disc, and turbomachine assembly

Redundant airfoil attachment

Blade attachment assembly

Systems and methods to axially retain blades

High pressure rotor disk

Grounding for fan blades on an underblade spacer

Cleat for open-work blade foot

Turbine blade root profile

CMC blade attachment shim relief

Attaching the blades to the drum of an axial turbocompressor

Turbine airfoil platform rail with gusset

Electrical grounding for blades

Compressor fairing segment

Turbine engine rotor assembly

Ductile compensation layer for brittle components

Apparatus for providing firtree slots

Axial retention of a platform seal

ARTICLE OF MANUFACTURE FOR TURBOMACHINE

Fairing assembly

Hybrid load differential amplifier operable in a high temperature environment of a turbine engine

Voltage regulator circuitry operable in a high temperature environment of a turbine engine

Turbine wheel in a turbine engine

Turbine blade support

MANUFACTURING A FAMILY OF AIRFOILS

Detachable fan blade platform and method of repairing same

Device for attaching blades to a turbine engine rotor disk

Blade dovetail bottom

Method for damping a gas-turbine blade, and vibration damper for implementing same

Annulus filler

Securing device for axially securing a blade root of a turbomachine blade

Blade wedge attachment