AIR LEAKAGE RESTRICTOR ARRANGEMENT FOR AN AIRCRAFT POWERPLANT

SEAL STRUCTURE FOR A GAS TURBINE ENGINE

TAILORING AIRCRAFT POWERPLANT SPLIT LINE PARAMETER WITH INFLATABLE BLADDER

NOZZLE RING FOR A RADIAL TURBINE, EXHAUST TURBINE, AND TURBOCHARGER

TURBINE WHEEL

MOLD AND BLADE MEMBER

TURBINE ENGINE WITH REDUCED CROSS FLOW AIRFOILS

Midshaft rating for turbomachine engines

Rotor blade and rotor blade assembly for a turbomachine

Turbine wheel

Vane Forward Rail for Gas Turbine Engine Assembly

COOLING ASSEMBLY FOR A TURBINE ASSEMBLY

ROTOR BLADE FOR A GAS TURBINE

Axial-flow fan, and outdoor unit for air-conditioning apparatus

Curved beams stacked structures-compliant shrouds

Bathtub damper seal arrangement for gas turbine engine

PROPULSION SYSTEM FOR A GAS TURBINE ENGINE

Midshaft rating for turbomachine engines

Turbine housing for an exhaust gas turbocharger

Front frame and deflection grid of a thrust reverser of an aircraft nacelle

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

Centrifugal fan

Midshaft rating for turbomachine engines

Connector and an anti thermal mismatch connecting device

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

PLENUM RESONANCE PREVENTION FOR GAS TURBINE ENGINE

Turbine blade trailing edge cooling feed

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

Film cooling structure and turbine blade for gas turbine engine

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

Single suction centrifugal blower

Centrifugal fan

Acoustic device and gas turbine

Erosion-resistant coating with patterned leading edge

Pre-swirl nozzle carrier and method of manufacturing the same

Cooling assembly for a turbine assembly

Nozzle vane

SYSTEM FOR AN IMPROVED STATOR ASSEMBLY

Gas turbine engine airfoils having multimodal thickness distributions

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

Internally-cooled turbomachine component

Turbocharger

Blade for a gas turbine engine

Airfoil with convex sides and multi-piece baffle

Turbomachine blade

Centrifugal compressor and turbocharger

Centrifugal fan

Jet noise suppressor

CMC aerofoil

Assembly for a turbine engine

Centrifugal blower

Vane arrangement for a turbo-machine

Collar support assembly for airfoils

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

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

Centrifugal compressor with diffuser with throat

Vane air inlet with fillet

Asymmetrical shroud for a compressor of a turbine engine

Shroud having elevations, for a turbomachine compressor

Compressor for turbine engine

Impeller, rotary machine, and turbocharger

Rotor having improved structure, and turbine and gas turbine including the same

Turbomachine airfoil array

VANE WHEEL AND BLOWING DEVICE

VANE WHEEL AND BLOWING DEVICE

Ceramic matrix composite joints

Turbomachine and turbine blade therefor

Turbine component with tip film cooling and method of cooling

Compressor aerofoil member

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

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Stator vanes including curved trailing edges

Rotor disc sealing device, and rotor assembly and gas turbine including the same

Turbine blade with tip vortex control and tip shelf

Impingement jet strike channel system within internal cooling systems

SEALING ELEMENT AND A METHOD OF MANUFACTURING THE SAME

VENT NOZZLE SHOCKWAVE CANCELLATION

High-pressure distributor blading having a variable-geometry insert

Thermal shielding in a gas turbine

Gas turbine engine airfoils having multimodal thickness distributions

Reinforcement for the leading edge of a turbine engine blade

Dual turn thrust reverser cascade systems and methods

Blast fan

Dual-walled components for a gas turbine engine

FAN CASING ASSEMBLY WITH COOLER AND METHOD OF MOVING

Turbocharger

Blade with parallel corrugated surfaces on inner and outer surfaces

Blade or guide vane with raised areas

Gas turbine engine rotor including squealer tip pocket

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

Nacelle short inlet

Turbine engine guide vane

Centrifugal pump with impeller centering and vibration dampening

End wall contour for an axial flow turbine stage

Nacelle short inlet for fan blade removal

Interior cooling configurations in turbine rotor blades

Gas turbine engine

Turbine blade with airfoil tip vortex control

NMR-MAS turbine assembly

Airfoil for axial flow machine

Bulged nozzle for control of secondary flow and optimal diffuser performance

CMC articles having small complex features for advanced film cooling

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

Sealing attachment for a gas turbine engine

Gas turbine membrane seal

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

Device for cooling a wall of a component of a gas turbine

Heat shield for mixed flow turbine wheel turbochargers

Rotary blade manufacturing method

Nacelle for an airplane turbojet

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

Turbine component connection with thermally stress-free fastener

Gas turbine guide vane element

Gas turbine engine airfoil profile

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

Rotor with axial arm having protruding ramp

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

Gas turbine axial compressor

TURBINE AIRFOIL

VANE STRUCTURE FOR AXIAL FLOW TURBOMACHINE AND GAS TURBINE ENGINE

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

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

Axial tension system for a gas turbine engine case

Bell mouth inlet for turbine blade

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

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

Radial compressor

MALE OR FEMALE ELEMENT FOR A CONIC COUPLING

Turbine bucket with endwall contour and airfoil profile

Turbine guide wheel

Blade cascade and turbomachine

Turbomachine assembly alleviating stresses at turbine discs

Sirocco fan and air conditioner having same

Lock plate

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

Intake air cooling system

Compressor stator with contoured endwall

Aerodynamically active stiffening feature for gas turbine recuperator

Active turbine or compressor tip clearance control

Variable displacement turbocharger and assembly method of variable nozzle mechanism

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

Gas turbine engine components with lateral and forward sweep film cooling holes

Endwall contouring

Airfoil

Spherical-link end damper system with near constant engagement

Pipe having an upstream core having a sharp curvature

Airfoil and platform assembly for subsonic flow

Blade dovetail bottom

Scalloped surface turbine stage

Exhaust gas diffuser for a gas turbine and a method for operating a gas turbine that comprises such an exhaust gas diffuser

Butterfly plate for a steam turbine exhaust hood

Guide blade of a turbomachine

Fan, molding die, and fluid feeder

Gas turbine stator vane

Compressor having blade tip features

Rotor of an axial compressor stage of a turbomachine

Compressor blade for an axial compressor

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

Blade

BEARING DEVICE, BEARING UNIT, AND ROTARY MACHINE

Gas turbine engine with variable area fan nozzle

Steam turbine stator vane and steam turbine using the same

CURVED LABYRINTH SEALS

Method for joining components

STEAM TURBINE NOZZLE SEGMENT HAVING ARCUATE INTERFACE

Gas turbine engine steam injection manifold

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

CONJUGATE CURVE PROFILES FOR VANE ARMS, MAIN-ARMS, AND UNISON RINGS

MALE OR FEMALE ELEMENT FOR A CONIC COUPLING

MALE OR FEMALE ELEMENT FOR A CONIC COUPLING

Turbine nozzle for a turbomachine

Compound cooling flow turbulator for turbine component

Method of manufacturing a turbine fan blade

Injection head, mixing space and power unit

Prechorded turbine nozzle

TURBINE BLADE CASCADE ENDWALL

Steam turbine stage

Endwall with leading-edge hump

Variable stator vane contoured button

MECHANICAL COUPLING

Wall of turbo machine and turbo machine

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

Comb for inlet barrier filter system

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

Mixed flow turbine

Method of manufacturing a turbine fan blade

Ring seal for a turbine engine

Variable nozzle turbocharger

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

Mounting disc

Tip cambered swept blade

Turbine rotor and turbine blade

Central cooling circuit for a moving blade of a turbomachine

Active multistable twisting device

Variable nozzle for a gas turbine

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

Crescentic ramp turbine stage

Turbomachine inner casing fitted with a heat shield

Scalloped surface turbine stage

Gas turbine tip shroud rails

Turbine case structure for an aircraft propulsion system engine

Axial seal systems for gas turbine engines

Turbine nozzle with dust tolerant impingement cooling