Control of leakage for gas turbine engine compressor blades

TANDEM BLADE ROTOR DISK

ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

ROTOR AND COMPRESSOR

Method for configuring a leading edge of a compressor stator platform and the corresponding stator platform

BLADE PLATFORM, BLADE RING, IMPELLER DISK AND GAS TURBINE ENGINE

Rotor arrangement for a rotor of a gas turbine

Tandem blade rotor disk

Turbine circumferential dovetail leakage reduction

Turbomachine polyspherical hub for variable pitch blades

Damping device

Intermediate element for a blade/rotor disc connection in a rotor of a turbomachine, associated rotor for a turbomachine, and turbomachine

Rotor and compressor

Tandem blade rotor disk

Rotor blade and disc of rotating body

Axial compressor

Turbine circumferential dovetail leakage reduction

Turbmachine fan disc

Damping device

Propeller fan

Fan blade attachment root with improved strain response

Tandem blade rotor disk

Multi-blade vane for a turbomachine rotor and rotor comprising same

COMBINED CEILING FAN AND LIGHT FIXTURE

Device for holding a centripetal radial air sampling member

Turbomachine stage and method of making same

Methods for processing bonded dual alloy rotors including differential heat treatment processes

Platform with axial attachment for blade with circumferential attachment

Blade retainer for gas turbine engine

Variable pitch blade holder for gas turbine engine

Aircraft fan with low part-span solidity

Fan blade attachment root with improved strain response

Vacuum pump and spiral plate, spacer, and rotating cylindrical body each included vacuum pump

Attachment of structures having different physical characteristics

Fan platform wedge seal

Interference fit with high friction material

Fan for a turbomachine

Blade for a gas turbine engine

Composite aircraft propeller blade with an integrated spar

Turbofan engine's fan blade and setting method thereof

Combination for sealing a gap between turbomachine blades and for reducing vibrations of the turbomachine blades

Compressor rotor disk for gas turbine

LOCKING SPACER ASSEMBLY

Entrance and exit chip rings for balancing broach forces

Processes and tooling associated with diffusion bonding

Compressor rotor stack assembly for gas turbine engine

Rotary machines including a hybrid rotor with hollow and solid rotor blade sets

Method for removing turbine blade, removal device for executing said method, and rotor set with said removal device

Method of manufacturing a fan blade

COMPRESSOR ROTOR AND AXIAL COMPRESSOR

Vane ring assembly and compressor and gas turbine including the same

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

Wear-resistant shield for a rotating blade of a gas turbine

Compressor blade locking mechanism in disk with tangential groove

Compressor blade locking mechanism in disk with axial groove

Turbomachine stage and method of making same

TURBINE ENGINE WITH AN EXTENSION INTO A BUFFER CAVITY

Compressor blade locking mechanism in disk with tangential groove

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

Rotor blade arrangement having elastic support elements for a thermal turbomachine

BLADE PLATFORM WITH CHAMFER

Turbine blade and locking set

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

Damper with varying thickness for a blade

Airfoil with retention pocket holding airfoil piece

Composite blisk

Vacuum-pump rotor

Rim seal for gas turbine engine

Gas turbine wheel assembly, method of modifying a compressor wheel, and method of mounting a blade to a gas turbine wheel

Method for release of fan blisk airfoil with external shaped charge

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

Air injection for an axial compressor with radially outer annulus

Composite rotatable assembly for an axial-flow compressor

Turbomachine blade fitted with an elastomer gasket

Method and system for mitigating rotor bow

Low profile fan platform attachment

Airfoil machining

Fan blade removal feature for a gas turbine engine

Rotor, axial compressor, installation method

Methods for processing bonded dual alloy rotors including differential heat treatment processes

Rotor wheel and impeller inserts

Load absorption systems and methods

Ceiling fan

Method and system for separable blade platform retention clip

Gas turbine engine with short inlet and mistuned fan blades

Portable milling tool with method for turbomachine milling

Method for repairing a generator rotor blade connection

Fan for a turbomachine

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

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

Airfoil platform having dual pin apertures and a vertical stiffener

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

Rotating blade

Rotating structure and a method of producing the rotating structure

Composite booster spool with separable composite blades

Bladed gas turbine rotor

Turbine engine rotor lock

ROTATING COMPONENTS WITH BLIND HOLES

Diffuser part for a gas turbine

Method and system for repairing turbomachine dovetail slots

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

Fan blade attachment root with improved strain response

Inertia friction welding method for welding together two portions of a rotary subassembly of a turbine engine

Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof

APPARATUS FOR MOUNTING A BLADE ON A TURBINE DISK

TURBINE BLADE RETENTION CONFIGURATION

Fan, in particular for a turbine engine

Bladed rotor

Article of manufacture for turbomachine

METHOD OF ATTACHING A CERAMIC MATRIX COMPOSITE ARTICLE

Turbomachine part with a non-axisymmetric surface

Locking element and turbomachine

Vibration isolation system for a fan motor

Rotor disc

Friction welding rotor blades to a rotor disk

Integrally bladed rotor having axial arm and pocket

Flowpath boundary and rotor assemblies in gas turbines

Flowpath boundary and rotor assemblies in gas turbines

Cover plate assembly for a gas turbine engine

Plated polymer compressor

Turbomachine rotor assembly and method

Fan containing fan blades with a U-shaped slot having a decreased length planar section

Tangential blade root neck conic

Integrally bladed rotor

Composite fan slider with nano-coating

Composite airfoil bonded to a metallic root

Rotor blade manufacture

Blade anchored securely in radial translation, propeller, turbine engine and aircraft

Root lightening holes with slot

Attachment of structures having different physical characteristics

Low profile fan platform attachment

Method and system for controlling compressor forward leakage

Fan blade root integrated sealing solution

Compressor blade mounting arrangement

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

Compliant intermediate component of a gas turbine engine

Turbine or compressor stage including an interface part made of ceramic material

Compressor rotor heat shield

Blade arrangement

Turbine engine impeller

Bladed rotor wheel for a turbine engine

Grounding for fan blades on an underblade spacer

Attaching the blades to the drum of an axial turbocompressor

Demountable propeller

Turbomachine rotor with a means for axial retention of the blades

Article of manufacture

ARTICLE OF MANUFACTURE FOR TURBOMACHINE

Fan rotor and associated turbojet engine

Blade dovetail bottom

Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted

Fan with overmolded blades

Turbomachine rotor with blade roots with adjusting protrusions

Bearing surface combined load-lock slots for tangential rotors

ALUMINUM FAN BLADE ROOT

Fan blade protection system

Propeller for a hydraulic machine, hydraulic machine equipped with such a propeller, and a method for assembling such a propeller

Integrally bladed rotor with slotted outer rim

Gas turbine compressor last stage rotor blades with axial retention

Turbine engine fan

Turbine engine fan disk

Rotor structure

Bladed rotor

METHOD AND COATING FOR PROTECTING AND REPAIRING AN AIRFOIL SURFACE

Blade-retaining device for turbomachine propeller

Composite vane mounting

Fan rotor for an airplane turbojet

Lightened axial compressor rotor

COMPRESSOR SECTION WITH TIE SHAFT COUPLING AND CANTILEVER MOUNTED VANES

Vibration damper device for turbomachine blade attachments, associated turbomachine and associated engines

Integrally bladed rotor with slotted outer rim

Device for axial retention of mobile vanes mounted on a rotor disc

Locking spacer assembly for a circumferential entry airfoil attachment system

Aerofoil blade assembly

Turbomachine rotor comprising an anti-wear plug, and anti-wear plug

Anti-wear device of a turbomachine rotor

Arrangement for axially securing blades in a rotor of a gas turbine

Device and method for connecting a blade to a rotor shaft of a continuous flow machine

Shim for a turbojet blade

Blade retaining device for turbo machine propeller

Seal coating between rotor blade and rotor disk slot in gas turbine engine

Rotor for a compressor

Fan rotor blade support structure and turbofan engine having the same

Method and apparatus for assembling gas turbine engines

Blade fastening means of a turbine

Sealing arrangement in a gas turbine engine

Axial compressor blade retention

Locking of the blades in a fan rotor

Turbine blade

Assembly of a fan blade and of its damper, fan blade damper and method for calibrating the damper

Apparatus and related method for sensing cracks in rotating engine blades

Rotor blade, method for producing a rotor blade, and compressor with a rotor blade

Replaceable staking insert

SHIM FOR A TURBOMACHINE BLADE

FAN BLADE RETAINING STRUCTURE

Stator joining strip and method of linking adjacent stators

FAN BLADE RETAINING STRUCTURE

TURBOMACHINE ROTOR ASSEMBLY

Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted

Rotor disk for turbomachine fan

BLADE ATTACHMENT RETENTION DEVICE

Metallic blade having a composite inlay

Turbomachine fan

Turbomachine rotor disk

Assembly for an aircraft engine compressor comprising blades with hammer attachment with inclined root

Methods and systems for assembling rotatable machines

Turbomachine rotor and turbomachine comprising such a rotor

Axial-flow compressor for a gas turbine engine

Dovetail surface enhancement for durability

Device for damping vibration of a ring for axially retaining turbomachine fan blades

Coated forward stub shaft dovetail slot

Method of repairing a threaded generator rotor blower assembly

Rotor for a compressor

Device for the positioning of a blade and bladed disk comprising such a device

Fan blade and disk assembly

Blade fixing relief mismatch

Restraining device for fan blade root

Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum

Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge

Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge

Compressor blade platform extension and methods of retrofitting blades of different blade angles

Blade fastening assembly and gas turbine including same

Turbomachine and method of assembly

C-connect fastener for a ceiling fan blade