AIR LEAKAGE RESTRICTOR ARRANGEMENT FOR AN AIRCRAFT POWERPLANT

CANTILEVER STATOR VANE

TURBOMACHINE FOR A FLIGHT PROPULSION DRIVE

TAILORING AIRCRAFT POWERPLANT SPLIT LINE PARAMETER WITH INFLATABLE BLADDER

SYSTEM AND APPARATUS FOR REDUCING BOW WAVES IN GAS TURBINE ENGINES

COMPRESSOR IMPELLER

FAN ASSEMBLIES WITH FAN DISK INSERTS AND METHODS OF ASSEMBLING THE SAME

TURBINE ENGINE WITH REDUCED CROSS FLOW AIRFOILS

Tie for a component

FAN

Turbine blade and gas turbine including the same

Turbine wheel

Vane Forward Rail for Gas Turbine Engine Assembly

Curved beams stacked structures-compliant shrouds

Bathtub damper seal arrangement for gas turbine engine

PROPULSION SYSTEM FOR A GAS TURBINE ENGINE

Method for manufacturing a composite platform for an aircraft turbine engine fan

Turbine blade and turbine

Blade for a rotating bladed disk for an aircraft turbine engine comprising a sealing lip having an optimized non-constant cross section

Planetary gear box

Shaped cavity at interface between journal bearing and rotor

Blade root receptacle for receiving a rotor blade

Integrated bladed rotor

Centrifugal fan

Turbomachine polyspherical hub for variable pitch blades

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

Rotor blade with blade root contour having a straight portion provided in a concave contour portion

Turbine engine with reduced cross flow airfoils

Turbine vane provided with a recess for embrittlement of a frangible section

Turbine engine with an airfoil having a set of dimples

ENGINE COMPONENT ASSEMBLY

Turbomachine comprising a heat exchanger in the secondary path

Turbine blade trailing edge cooling feed

Modeling method for a fan assembly of an aero engine

Masking bladed disc for reducing the radar signature of a moving compressor moving disc of a jet engine

Tip squealer configurations

Torque limiting device in a connection between a gearbox and a stationary structure in a gas turbine engine and a gas turbine engine

Variable geometry inlet system

Turbine blade

Composite airfoil assembly with separate airfoil, inner band, and outer band

Single suction centrifugal blower

Rounded radial snap configuration for a gas turbine engine cover plate

Centrifugal fan

Engine components with cooling holes having tailored metering and diffuser portions

Turbine rotor blade with platform with non-linear cooling passages by additive manufacture

Acoustic device and gas turbine

Erosion-resistant coating with patterned leading edge

Pre-swirl nozzle carrier and method of manufacturing the same

Nozzle vane

Vane with chevron face

Cooled airfoil, guide vane, and method for manufacturing the airfoil and guide vane

Turbine incorporating endwall fences

Shroud interlock

Internally-cooled turbomachine component

Blade for a gas turbine engine

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

Turbine nozzle and axial-flow turbine including same

High performance wedge diffusers for compression systems

Compressor aerofoil

Turbomachine blade

Integral half vane, ringcase, and id shroud

Turbine blade of gas turbine having cast tip

Centrifugal compressor and turbocharger

Centrifugal fan

Jet noise suppressor

Radial fan

CMC aerofoil

Impeller and water pump having the same

Fan

Composite airfoil assembly with separate airfoil, inner band, and outer band

Variable nozzle unit and turbocharger

Impingement cooling features for gas turbines

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

First-stage turbine vane supporting structure and gas turbine including same

Variable geometry inlet system

Impeller, turbocharger, and method for forming flow field for gas in impeller and turbocharger

Asymmetrical shroud for a compressor of a turbine engine

Shroud having elevations, for a turbomachine compressor

Compressor for turbine engine

Heat dissipation blade and heat dissipation fan

Sealing structure for turbines, and turbine and gas turbine having the same

Stator vanes including curved trailing edges

Varying seal rail fillet for turbine blades

AXIAL FAN

High-pressure compressor rotor with leading edge having indent segment

Rainbow flowpath low pressure turbine rotor assembly

VENT NOZZLE SHOCKWAVE CANCELLATION

High-pressure distributor blading having a variable-geometry insert

Device for modulating a gas ejection section

Blade outer air seal surface

FAN CASING ASSEMBLY WITH COOLER AND METHOD OF MOVING

Chamfered stator vane rail

Blade with parallel corrugated surfaces on inner and outer surfaces

Gas turbine engine rotor including squealer tip pocket

Labyrinth seal with lubricant directing projection

Diffuser having shaped vanes

Engine component assembly

Engine components with cooling holes having tailored metering and diffuser portions

Internal rib with defined concave surface curvature for airfoil

Intermediate central passage spanning outer walls aft of airfoil leading edge passage

Guide vane ring for a turbomachine

THREE-VANE DOUBLE ROTOR FOR VERTICAL AXIS TURBINE

HIGH SPEED SPINDLE

Nacelle short inlet

Turbine engine guide vane

Turbine rotor blade

Centrifugal pump with impeller centering and vibration dampening

Gas turbine engine trailing edge ejection holes

Turbine blade attachment curved rib stiffeners

End wall contour for an axial flow turbine stage

Tube thermal coupling assembly

System for an inlet guide vane shroud and baffle assembly

Interior cooling configurations in turbine rotor blades

Gas turbine engine

Compression cowl for jet engine exhaust

Turbine engine flow path

Turbine blade with airfoil tip vortex control

Rotor for gas turbine engine

CMC articles having small complex features for advanced film cooling

Ceramic matrix composite ring shroud retention methods-wiggle strip spring seal

Gas turbine engine blade platform modification

AXIAL TURBO MACHINE

Sealing attachment for a gas turbine engine

Cooling device with small structured rib-dimple hybrid structures

METHOD FOR GENERATING AN AIRFOIL INCLUDING AN AERODYNAMICALLY-SHAPED FILLET AND AIRFOILS INCLUDING THE AERODYNAMICALLY-SHAPED FILLET

Turbofan bypass air cooled oil cooler fairings

Heat shield for mixed flow turbine wheel turbochargers

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

Film cooled multi-walled structure with one or more indentations

AIRFOIL AND METHOD FOR MANAGING PRESSURE AT TIP OF AIRFOIL

CENTRIFUGAL COMPRESSOR IMPELLER WITH BLADES HAVING AN S-SHAPED TRAILING EDGE

Alignment system for exhaust installation

Variable area vane endwall treatments

Endwall countouring trench

Stator vane with platform having sloped face

COOLED AIRFOIL, GUIDE VANE, AND METHOD FOR MANUFACTURING THE AIRFOIL AND GUIDE VANE

Gas turbine axial compressor

Shielding pockets for case holes

TURBINE AIRFOIL

INTERIOR COOLING CHANNELS IN TURBINE BLADES

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

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

Centrifugal compressor and turbocharger

Turbine rotor segmented sideplates with anti-rotation

Casting optimized to improve suction side cooling shaped hole performance

Variable geometry inlet system

Aerodynamic track fairing for a gas turbine engine fan nacelle

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

Gas turbine engine component having shaped pedestals

Fan blade dovetail and spacer

Fan exit guide vane platform contouring

Fan, molding die, and fluid feeder

Fan, molding die, and fluid feeder

Contoured blade outer air seal for a gas turbine engine

Gas turbine blade

Power turbine blade airfoil profile

Rotor of an exhaust gas turbocharger

Structural configurations and cooling circuits in turbine blades

Turbine airfoil with an internal cooling system having trip strips with reduced pressure drop

Structural configurations and cooling circuits in turbine blades

Structural configurations and cooling circuits in turbine blades

Structural configurations and cooling circuits in turbine blades

Interior cooling circuits in turbine blades

Structural configurations and cooling circuits in turbine blades

Stator casing cooling system

Steam turbine nozzle segment having transitional interface, and nozzle assembly and steam turbine including such nozzle segment

Radial compressor

Variable geometry turbocharger

Systems and methods for modifying a pressure side on an airfoil about a trailing edge

Annulus filler

Blade cascade and turbomachine

Turbomachine assembly alleviating stresses at turbine discs

Turbomachine rotor blade

Housing section of a turbine engine compressor stage or turbine engine turbine stage

Compressor stator with contoured endwall

Aerodynamically active stiffening feature for gas turbine recuperator

Blade outer air seal surface

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

Rotor blade for a turbomachine and turbomachine

Endwall contouring

Endwall contouring

Airfoil

Flow path structure and gas turbine exhaust diffuser

Scalloped surface turbine stage

Turbine engine rotor blade groove

Seals for rotary devices and methods of producing the same

Interlaminar stress reducing configuration for composite turbine components

Gas turbine annular diffusor

Airfoils including tip profile for noise reduction and method for fabricating same

Low-ductility turbine shroud

Fan blade channel termination

Turbine disc sealing assembly

Guide blade of a turbomachine

Fan, molding die, and fluid feeder

Gas turbine stator vane

Compressor having blade tip features

Compressor blade for an axial compressor

Rotor of a turbomachine compressor, with an optimised inner end wall

Self-actuating bleed valve for a gas turbine engine

Gas turbine engine with variable area fan nozzle

Low-pressure turbine

RADIAL FLOW TURBINE WHEEL FOR A GAS TURBINE ENGINE

CURVED LABYRINTH SEALS

Method and system for providing a splitter to improve the recovery of compressor discharge casing

STEAM TURBINE NOZZLE SEGMENT HAVING ARCUATE INTERFACE

Turbine vane for a gas turbine and casting core for the production of such

Seal and seal arrangement for confining leakage flows between adjacent components of turbo-machines and gas turbines

Turbine blade damping device with controlled loading

Compound cooling flow turbulator for turbine component

Method of manufacturing a turbine fan blade

Injection head, mixing space and power unit

Prechorded turbine nozzle

Flared tip turbine blade

Oiling nozzle for thrust bearing

Exhaust gas discharge system and plenum

Turbine engine rotor hub

Method for reducing sound output at the back of a turbo engine and turbo engine improved by this method

Mixed flow turbine or radial turbine

Device that makes it possible to improve the effectiveness of the acoustic treatments in a pipe of an aircraft power plant

Blade with a cooling groove for a bladed wheel of a turbomachine

Blade for a flow machine

Exhaust gas diffuser wall contouring

Method of manufacturing a turbine fan blade

Gas turbine engine with canted pocket and canted knife edge seal

Local indented trailing edge heat transfer devices

Variable nozzle turbocharger

Gas turbine engine with concave pocket with knife edge seal

Turbofan gas turbine engine and nacelle arrangement

Blades

Tip ramp turbine blade

Turbo machine with a rotor which has at least one rotor disk with a bore

Multi-layer ring seal

Tip cambered swept blade

Turbine rotor and turbine blade

Cooled turbine blade

Central cooling circuit for a moving blade of a turbomachine

Active multistable twisting device

Variable nozzle for a gas turbine

Turbine airfoil with curved squealer tip

Turbine airfoil curved squealer tip with tip shelf

Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring

Turbine blade trailing edge construction

Turbine blade cooling system

Steep angle turbine cover buckets having relief grooves

Crescentic ramp turbine stage

Turbomachine inner casing fitted with a heat shield

Scalloped surface turbine stage

Turbine engine disk spacers

Control lever for the angular setting of a stator blade in a turboshaft engine

Gas turbine tip shroud rails

Turbine blade with impingement cooling

Profiled blades for turbocharger turbines, compressors, and the like

Contoured disk bore

Device for mixing two flows of fluid which are initially guided separate from one another in a bypass jet engine

Turbine case structure for an aircraft propulsion system engine

Self-stabilizing turbine and steam-driven turbine assembly using the same

Turbine nozzle with dust tolerant impingement cooling

Water pump and manufacturing method thereof