WEAR PAD FOR ROOT OF FAN BLADE

PROTECTION ELEMENT FOR A COMPRESSOR DRUM AND METHOD FOR REPAIRING A COMPRESSOR DRUM

COMPOSITE AIRFOIL ASSEMBLY HAVING A COMPOSITE AIRFOIL AND SPAR

METHOD FOR MAINTAINING A BLADED WHEEL OF A HIGH-PRESSURE TURBINE OF A TURBOMACHINE

WEAR PAD FOR ROOT OF FAN BLADE

TURBINE ENGINE HAVING A ROTATABLE DISK AND A BLADE

MOVABLE RING ASSEMBLY FOR A TURBOMACHINE ROTOR

SYSTEM AND METHOD FOR COUPLING A COMPONENT TO A GAS TURBINE ENGINE BLADE

Rotor assembly having protective core and gas turbine engine comprising same

TURBINE BLADE AND ASSEMBLY WITH DOVETAIL ARRANGEMENT FOR ENLARGED ROTOR GROOVE

ROTOR BLADE FOR A GAS TURBINE

Method for providing a gas turbine blade and rotor wear-protection system

Fan rotor with variable pitch blades and turbomachine equipped with such a rotor

System with a rotor blade for a gas turbine with a blade root protective plate having a sealing section

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

Gas turbine blade and rotor wear-protection system

Rotor and turbo machine including same

Self-lubricating blade root/disk interface

Seal element for sealing a joint between a rotor blade and a rotor disk

Extended root region and platform over-wrap for a blade of a gas turbine engine

Turbine shroud assembly with multi-piece support for ceramic matrix composite material seal segments

Composite blade and method for molding composite blade

Cooled attachment sleeve for a ceramic matrix composite rotor blade

Turbine wheel assembly

Attachment of structures having different physical characteristics

COATING SYSTEM INCLUDING OXIDE NANOPARTICLES IN OXIDE MATRIX

Methods and articles relating to ionic liquid bath plating of aluminum-containing layers utilizing shaped consumable aluminum anodes

Vane ring assembly and compressor and gas turbine including the same

Removable anti-wear part for blade tip

ROTOR DISK ASSEMBLY FOR A GAS TURBINE ENGINE

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

Gas turbine blade or compressor blade having anti-fretting coating in the blade root region and rotor

Thermal shielding in a gas turbine

Airfoil with tie member and spring

Turbine wheel with circumferentially-installed inter-blade heat shields

Turbine blade with three-dimensional CMC construction elements

Graphene discs and bores and methods of preparing the same

Anti-rotation feature for wear liners

Dual alloy blade

Bearing element and turbomachine with a bearing element

Methods and articles relating to ionic liquid bath plating of aluminum-containing layers utilizing shaped consumable aluminum anodes

Blade

BLADE OF A TURBOMACHINE HAVING BLADE ROOT THERMAL INSULATION

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

Ductile compensation layer for brittle components

Rotating structure and a method of producing the rotating structure

Composite airfoil metal patch

Composite blade root stress reducing shim

Electrostatic discharge prevention for a fan blade

Fan blade and method of covering a fan blade root portion

Hot corrosion-protected articles and manufacture methods

Ceramic attachment configuration and method for manufacturing same

Blade wedge attachment lay-up

Fan blade root

CMC blade with monolithic ceramic platform and dovetail

PLATED POLYMER COMPONENTS FOR A GAS TURBINE ENGINE

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

Plated polymer compressor

Turbine engine components with chemical vapor infiltrated isolation layers

Rotor disk assembly for a gas turbine engine

GAS TURBINE BLADE AND METHOD OF PROTECTING SAME

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

FAN BLADE WITH STATIC DISSIPATIVE COATING

Engine component having support with intermediate layer

Blade wear pads and manufacture methods

Co-formed element with low conductivity layer

Fan blade lubrication

Rotor blade manufacture

Rotor blade root spacer with grip element

Developments in or relating to rotor balancing

Coating system including diffusion barrier layer including iridium and oxide layer

Fan blade spacer

Platform for ceramic matrix composite turbine blades

Composite turbine blade for high-temperature applications

Attachment of structures having different physical characteristics

Wind turbine blade

Wear pad to prevent cracking of fan blade

Rotor blade arrangement and gas turbine

Retainer plate

Gas turbine engine component including a compliant layer

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

Method of applying a nanocrystalline coating to a gas turbine engine component

Fibrous reinforcement structure for composite material part having a reduced thickness portion

Maskant for use in aluminizing a turbine component

Integral fan blade wear pad and platform seal

Device, system and method for preventing leakage in a turbine

Erosion resistant coating

Turbine engine comprising a metal protection for a composite part

Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface

Airfoil member and composite platform having contoured endwall

Turbine engine impeller

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

Bladed rotor wheel for a turbine engine

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

Dovetail attachment seal for a turbomachine

CMC blade attachment shim relief

Rotary machines and methods of assembling

Ductile compensation layer for brittle components

Turbine wheel in a turbine engine

WEAR RESISTANT ARTICLE

WEAR RESISTANT TURBINE FAN BLADE

ROTOR DISK AND ROTOR ASSEMBLY

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

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

Blade wedge attachment

Pressure maskers and pressure masking systems

Energy absorbent fan blade spacer

MATING STRUCTURE AND METHOD OF FORMING A MATING STRUCTURE

Wear-resistant part for the support of a blade of a turbojet fan

Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element

Compressive stress system for a gas turbine engine

Layout of a blisk

Turbine engine fan

Access means for an electrical machine

ANNULUS FILLER SYSTEM

Annulus filler system

Retention device for a composite blade of a gas turbine engine

Blade preloading method

RING ELEMENT AND TURBOMACHINE HAVING SUCH A RING ELEMENT

Turbine airfoil component assembly for use in a gas turbine engine and methods for fabricating same

Processes for producing components containing ceramic-based and metallic materials

Anti-wear device for the blades of a turbine distributor in an aeronautical turbine engine

Reinforced fan blade shim

Method of applying a nanocrystalline coating to a gas turbine engine component

Gas turbine blade and method of protecting same

Turbine engine component having protective coating

Electroformed conforming rubstrip

Turbine rotor assembly

Airfoil with galvanically isolated metal coating

Ceramic composite with integrated compliance/wear layer

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

Turbomachine rotor comprising a pretensioning device for pretensioning a rotor blade

Apparatus and method for reducing wear in disk lugs

Apparatus and a method of applying a dry film lubricant to a rotor slot

Turbine blade of a gas turbine and method for coating a turbine blade of a gas turbine

Fan blade dovetail with compliant layer

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

Anti-wear device of a turbomachine rotor

Assembly providing contaminant removal

Airfoil attachment

Shim for a turbojet blade

Fan blade anti-fretting insert

Blade preloading system

COMPOSITE MATERIAL TURBOMACHINE BLADE WITH A REINFORCED ROOT

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

Rotor blade arrangement and gas turbine

Turbine bucket with dovetail seal and related method

Methods of maintaining turbine discs to avert critical bucket attachment dovetail cracks

Ceramic composite with integrated compliance/wear layer

Shim for a turbomachine blade

SHIM FOR A TURBOMACHINE BLADE

Wear prevention spring for turbine blade

TURBOMACHINE ROTOR ASSEMBLY

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

Blade of a turbomachine

Turbomachine rotor disk

Fan blade made of a textile composite material

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

MICROWAVE PROCESS FOR FORMING A COATING

Turbomachine rotor and turbomachine comprising such a rotor

System for retaining blades in a rotor

Axial-flow compressor for a gas turbine engine

ANTI-WEAR DEVICE FOR A GUIDE PIVOT OF A VARIABLE-PITCH VANE OF A TURBOMACHINE COMPRESSOR

Dovetail surface enhancement for durability

Assembly and method for the mounting of the foot of a blade of a turbine, blower, compressor, and turbine comprising such an assembly

Methods and apparatus for assembling gas turbine engines

Method of protecting contacting surfaces between two metal parts benefiting from such protection

Coated forward stub shaft dovetail slot

Apparatus and a method of applying a dry film lubricant to a rotor slot

Ceramic composite with integrated compliance/wear layer

Laminated turbomachine airfoil with jacket and method of making the airfoil

Blade fixing relief mismatch

Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts

Methods and apparatus for assembling gas turbine engines