TURBINE ENGINE SYSTEM

DAMPER RING FOR REDUCING UNWANTED VIBRATIONS OF A BLISK, AS WELL AS BLISK AND TURBOMACHINE

ACTUATION SYSTEM WITH SPHERICAL PLAIN BEARING

Turbomachine polyspherical hub for variable pitch blades

Device for cooling an outer casing of a turbomachine and turbomachine provided with such a device

Centralized oil distribution system

Variable stator vanes with anti-lock trunnions

Rotor assembly and rotating machine

Distributed hybrid damping system

BACKPACK BLOWER

Assembly for axial turbomachine, associated axial turbomachine, assembly method, and sealing joint

Rotor balance weight system

Fan blade attachment root with improved strain response

A TURBOMACHINE BLADE OR VANE HAVING A VORTEX GENERATING ELEMENT

Film-cooled multi-walled structure with one or more indentations

Linkage assembly preventing axial rotation of the link rod for a gas turbine engine

Gas turbine blade impulse body module

Abradable layer with glass microballoons

Fan blade attachment root with improved strain response

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Hot section dual wall component anti-blockage system

AXIAL STIFFENING RIBS/AUGMENTATION FINS

Assembly for a turbine engine

Impingement cooling features for gas turbines

Turbomachine blade cooling circuit

Fan blade with filled pocket

Rotor balance weight system

Acoustic panel employing rounded particles in septum layer and system and method for making same

Lever with pre-attached self locking nut for a variable turbine geometry turbocharger

Backpack blower

GAS TURBINE

Linkage assembly preventing axial rotation of the link rod

Gas turbine engine cooling air manifolds with spoolies

Air-collecting structure for enhancing cooling performance for transition piece and gas turbine combustor having same

Turbojet engine with thrust take-up means on the inter-compressors case

Aircraft turbomachine assembly having an improved decoupling system in the event of a fan blade loss

Abradable layer with glass microballoons

High-pressure distributor blading having a variable-geometry insert

Investment casting core

Flexural spring-energized interface for bellowed ball-joint assemblies for controlled rotational constraint

Pulse body module with bearing protection

Rotary machine

Rotary machine

Turbomachine blade assembly

Impulse element module for a turbomachine

Fuel nozzle with increased spray angle range

Guide vane segment

Turbine blade with heat shield

Turbine blade with heat shield

Airfoil trailing edge cooling

Core component having toroidal structures

Turbomachine stage

Gas turbine engine cooling air manifolds with spoolies

Cooling device with small structured rib-dimple hybrid structures

Journal bearing for rotating gear carrier

Fan blade attachment root with improved strain response

Nacelle for an airplane turbojet

Angled impingement inserts with cooling features

Gas turbine bucket shanks with seal pins

Film cooled multi-walled structure with one or more indentations

Alignment system for exhaust installation

Variable area vane endwall treatments

Turbomachine accessory gearbox alignment pin

Support arrangement for a transition piece of a gas turbine engine

Gas turbine engine and foil bearing system

Gas turbine engine and method of assembling the same

Turbomachine blade arrangement with first and second guides with respective movable first and second elements to reduce vibrational response

Blade cascade for a turbomachine

Exhaust system having a flow path liner supported by structural duct segments

Thermocouple with a vortex reducing probe

Fluid film conical or hemispherical floating ring bearings

Rotor of a supercharging device

Layered arrangement, hot-gas path component, and process of producing a layered arrangement

Baffle with flow augmentation feature

Rod end tensioner and self adjusting rod end

Internally cooled airfoil

Impingement cooling mechanism, turbine blade and cumbustor

Active turbine or compressor tip clearance control

System for damping vibrations in a turbine

Ceramic matrix composite liner attachment

VARIABLE AREA TURBINE NOZZLE

Airfoil cooling enhancement and method of making the same

Rotor blade arrangement for a turbo machine

Elder Rotary Stirling Engine

Turbine combustion system cooling scoop

Self-oscillating fuel injection jets

Reduction of turbocharger core unbalance with centering device

STEAM VALVE

Guide blade carrier

Gas turbine engine and foil bearing system

Turbine nozzle for a turbomachine

Compliant spherical bearing mount

Borescope boss and plug cooling

Conical pin to maintain bearing system

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

ABRADABLE MATERIAL COMPOSITION, A THERMOMECHANICAL PART OR CASING INCLUDING A COATING, AND A METHOD OF FABRICATING OR REPAIRING A COATING PRESENTING SAID COMPOSITION

Gas turbine component with reduced cooling air requirement

Gas turbine engine with fan variable area nozzle having a rotational valve system

Percussion drilled shaped through hole and method of forming

Bearing-like structure to control deflections of a rotating component

Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes

Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade

Bleed valve outlet flow deflector

Embedded mount for mid-turbine frame

Aeroengine bleed valve

Gap control arrangement for a gas turbine

Abradable material composition, a thermomechanical part or casing including a coating, and a method of fabricating or repairing a coating presenting said composition

Axial locking device for turbine blades

Vibration isolation engine mount system and method for ducted fans

Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps

Heat transfer arrangement

Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites

Rotor blade connecting arrangement for a turbomachine