POLYGONAL PROFILE COUPLING OF PUMPS IN A LUBRICATION ASSEMBLY

AIRFOIL ROTOR HUB SYSTEM HAVING INTENTIONAL FREQUENCY MISTUNING

TURBINE COMPONENT HAVING AIR-JET COOLING STRUCTURE, AND GAS TURBINE INCLUDING SAME

MOVING BLADE FOR A TURBINE OF A TURBINE ENGINE, COMPRISING A STILT EQUIPPED WITH PROJECTIONS FOR RADIALLY RETAINING THE BLADE

AEROFOIL AND METHOD

COOLING SCHEMES FOR AIRFOILS FOR GAS TURBINE ENGINES

Turbine rotor for a turbomachine

Method and system for component alignment in turbine casing and related turbine casing

MULTI-CORE ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION SYSTEM

PROPULSION SYSTEM FOR A GAS TURBINE ENGINE

Bore compartment seals for gas turbine engines

Triangular-frame connection between fan case and core housing in a gas turbine engine

Cooling schemes for airfoils for gas turbine engines

Tube gallery for gas turbine engine

Variable gap between impeller rotor and static structure

Method and system for component alignment in turbine casing and related turbine casing

LABYRINTH SEAL COMPRISING AN ABRADABLE ELEMENT WITH VARIABLE CELL DENSITY

Method for manufacturing an engine component with a cooling duct arrangement and engine component

Impact-cooling tubular insert for a turbomachine distributor

Inserts for airfoils of gas turbine engines

Impeller

Component with mechanical locking features incorporating adaptive cooling and method of making

Acoustic device and gas turbine

Lubricant nozzle for a planetary gear set speed reducer of a turbomachine

Turbine stator blade cooled by air-jet impacts

Locking spacer assembly, corresponding blade assembly, method for installing a locking spacer

Systems and methods for manufacturing film cooling hole diffuser portion

Device for holding a centripetal radial air sampling member

Composite gas turbine engine component

Turbine blade tip wall cooling

Gas turbine engines including tangential on-board injectors and methods for manufacturing the same

Article having cooling passage network with inter-row sub-passages

Assembly comprising a lubricating wheel and lubricant nozzles for a planetary gear speed reducer of a turbomachine

Cooling hole with shaped meter

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Vortex generators for turbine engine exhaust

Reduced stress boss geometry for a gas turbine engine

TURBINE ELEMENT FOR HIGH PRESSURE DROP AND HEAT TRANSFER

COOLING ARRANGEMENT WITH CRENELLATION FEATURES FOR GAS TURBINE ENGINE COMPONENT

Wall comprising a film cooling hole

Blade outer air seal cooling fin

Heat shield, systems and methods

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

Vane ring assembly, method of assembling the same, and gas turbine including the same

Method and apparatus for cooling an rotor assembly

Gas turbine engine vane attachment feature

Fluid collection gutter for a geared turbine engine

Double wall turbine gas turbine engine blade cooling configuration

CERAMIC COMPONENT FOR COMBUSTION TURBINE ENGINES

Support rail truss for gas turbine engines

Modified structural truss for airfoils

Strip seal axial assembly groove

Gas turbine engine front center body architecture

Turbine engine and components for use therein

High thermal response exhaust diffuser strut collar

Turbomachine airfoil

Rotor with subset of blades having a cutout leading edge

Systems and methods for manufacturing film cooling hole diffuser portion

Turbomachine rotor blade tip shroud cavity

Ceramic matrix composite components having a deltoid region and methods for fabricating the same

Spline alignment

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

Turbine engine part with non-axisymmetric surface

Blade comprising a shank, provided with a depressed portion

Fan blade with structural spar and integrated leading edge

TURBINE COMPONENT THERMAL BARRIER COATING WITH VERTICALLY ALIGNED, ENGINEERED SURFACE AND MULTIFURCATED GROOVE FEATURES

System and apparatus for diversified gearbox

Acoustic liners for use in a turbine engine

Cooling hole with shaped meter

ANTI-BIRD STRIKE PROTECTION NET FOR AIRCRAFT JET ENGINE

Rotor with overhang at blades for a locking element

CMC turbine blade platform damper

Aerofoil

Propulsion unit for an aircraft and method for opening a movable cowl of said propulsion unit

COATED AND UNCOATED SURFACE-MODIFIED AIRFOILS FOR A GAS TURBINE ENGINE COMPONENT AND METHODS FOR CONTROLLING THE DIRECTION OF INCIDENT ENERGY REFLECTION FROM AN AIRFOIL

AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER PEDESTALS FOR A GAS TURBINE ENGINE COMPONENT AND SYSTEMS FOR COOLING AN AIRFOIL PLATFORM

Platform for an airfoil having bowed sidewalls

Turbine blade attachment mechanism

Gas turbine disk

Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine

Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element

Diffuser part for a gas turbine

Cover plate for a component of a gas turbine engine

Gas turbine engine front center body architecture

Reduced stress boss geometry for a gas turbine engine

Gas turbine stator with winglets

Gas turbine diffuser outer diameter and inner diameter wall strips for turbine exhaust manifold pressure oscillation reduction

Angled impingement inserts with cooling features

Turbine airfoil with additive manufactured reinforcement of thermoplastic body

Heat shield, systems and methods

GAS TURBINE ENGINE COMPONENT WITH SEPARATION RIB FOR COOLING PASSAGES

Seals for a gas turbine engine assembly

Supersonic caret inlet system

Blade outer air seal having angled retention hook

System and apparatus for diversified gearbox

Airfoil with an integrally stiffened composite cover

Gas turbine engine component providing prioritized cooling

Flowpath boundary and rotor assemblies in gas turbines

Engine mount

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

POWER TURBINE AIR STRUT

Tie shaft flow trip

Gas turbine engine airfoil platform cooling passage and core

Divot for blocker doors of thrust reverser system

Acoustically treated thrust reverser track beam

Borescope assembly and method of installing borescope plugs

Vortex generators placed in the interblade channel of a compressor rectifier

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Pivoting ring petal actuation for variable area fan nozzle

Closure bucket for turbo-machine

Fan containment system

Fan spacer having unitary over molded feature

System and method for reducing back pressure in a gas turbine system

System for damping vibrations in a turbine

Cover plate for a component of a gas turbine engine

Turbomachine containment structure

Shark-bite tip shelf cooling configuration

Surface area augmentation of hot-section turbomachine component

Blade and method for manufacturing blade

Device for reducing the noise emitted by the jet of an aircraft propulsion engine

Rotor device for a jet engine with a disk wheel and several rotor blades

COMPLIANT PLATE SEAL ASSEMBLY FOR A TURBO MACHINE

FLOW DISCHARGE DEVICE

LEADING EDGE AIRFOIL-TO-PLATFORM FILLET COOLING TUBE

Exhaust hood diffuser

Turbine airfoil and method for cooling a turbine airfoil

Flow discouraging systems and gas turbine engines

Composite flange, duct incorporating a flange and method of making a flange

Turbine blade equipped with means of adjusting its cooling fluid flow rate

Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron

Sealing System Between a Shroud Segment and a Rotor Blade Tip and Manufacturing Method for Such a Segment

Fan

DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION

Device with secondary jets reducing the noise generated by an aircraft jet engine

Trailing edge for an aircraft engine, of the type with moving chevrons

Cooling arrangements

Passive boundary layer control elements

Microcircuit cooling for blades

Turbine shroud support coupling assembly

THERMALLY BALANCED AERO STRUCTURES

Diffuser for decelerating a compressed fluid

Systems and methods for reducing noise from jet engine exhaust

Counter-vortex film cooling hole design

Counter-vortex paired film cooling hole design

Thermally conductive structure

Modular chevron exhaust nozzle

Turbine blade having a convergent cavity cooling system for a trailing edge

Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods

Method for preventing backflow and forming a cooling layer in an airfoil

Cooling arrangement for a component of a gas turbine engine

Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise

Vectorable nozzle with pivotable triangular panels

Bleed air relief system for engines

Leading edge configuration for compressor blades of gas turbine engines

Mistake proof identification feature for turbine blades

Turbine heat shield with ribs

Duct liner acoustic splice

Split shroud exhaust nozzle

Device and method for detachably connecting an impeller to a shaft

Device for reducing jet engine exhaust noise using oscillating jets

Component and turbine assembly with film cooling