TURBINE AIRFOIL AND GAS TURBINE INCLUDING THE SAME

TURBOMACHINE SUBASSEMBLY COMPRISING A GOOSENECK OF IMPROVED CONFIGURATION, AND TURBOMACHINE COMPRISING SUCH A SUBASSEMBLY

CURVED BLADE, PREPARATION METHOD THEREOF, AND CENTRIFUGAL IMPELLER COMPRISING THE SAME

GEARED GAS TURBINE ENGINE

Method for Manufacturing Heat Exchanger and Heat Exchanger

EXHAUST DUCT FOR GAS TURBINE ENGINE

GUIDE VANES ASSEMBLY WITH POSITION-MAINTAINING DEVICE

Guide vanes assembly with position-maintaining device

Air flow straightening stage for a turbomachine

ANNULUS CONTOURING

Stator vane for a turbomachine

Tangentially bowed airfoil

Diffuser pipe with exit flare

Transition piece, combustor, and gas turbine engine

Bladed disc

Deployable fairing for door reversers systems and methods

Gas turbine blade arrangement

Airbag device

Thrust reverser cascade including acoustic treatment

Gas turbine engine airfoil

AIRFLOW DEVICE

Turbomachine assembly having a damper

Airfoil having a spline fillet

Assembly for a turbomachine turbine

Rotor assembly and rotating machine

Finger seal assembly for gas turbine engine and method of making

Turbine blade assembly

Blade assembly for gas turbine engine

Controlled flow turbine blades

Expander and fluid circulation system comprising same

Diffuser for rotating detonation engine

Turbomachine nozzle with an airfoil having a curvilinear trailing edge

Mateface for blade outer air seals in a gas turbine engine

CONTROLLED FLOW TURBINE BLADES

Stator vane ring or ring segment

Engine component with set of cooling holes

Diffuser vane and centrifugal compressor

DIFFUSER PIPE EXIT FLARE

Deswirler assembly for a centrifugal compressor

Windmill and blower comprising the same

Gas turbine engine airfoil

Rotatable valve for turbocharger system with plural volute members

Blade for a gas turbine engine

Contoured endwall for a gas turbine engine

Gas turbine engine airfoil

GEARED GAS TURBINE ENGINE

Turbine assembly with ring segments

Gas turbine engine airfoil

Rotor blade arrangement

Deployable fairing for door reversers systems and methods

Turbine wheel

Airfoil with leading edge guard

COOLING HOLE GEOMETRY FOR GAS TURBINE ENGINE COMPONENTS

Blade of fan or compressor

Reinforced axial diffuser

Composite translating cowl assembly for a thrust reverser system

Hot section dual wall component anti-blockage system

Airfoil for a turbomachine

Leading edge profile of vanes

Airfoil of axial flow machine

Blade or vane, blade or vane segment and assembly for a turbomachine, and turbomachine

Diffuser pipe with non-axisymmetric end wall

INTER-STAGE CAVITY PURGE DUCTS

Guide vane airfoil for the hot gas flow path of a turbomachine

Fan blade and method for determining shape of fan blade

Centrifugal compressor with diffuser with throat

Gas turbine engine components having internal hybrid cooling cavities

Recuperator for gas turbine engine

Radial compressor

Fluid recirculation turbine system

Rotatable component for turbomachines, including a non-axisymmetric overhanging portion

Modified J type cantilevered vane and gas turbine having the same

Asymmetrical shroud for a compressor of a turbine engine

Shroud having elevations, for a turbomachine compressor

Combination for sealing a gap between turbomachine blades and for reducing vibrations of the turbomachine blades

Blade and rotor for a turbomachine and turbomachine

FLUID SEAL

HEAT EXCHANGER FRAME

Gas turbine engine inlet

CONICAL FAN HUB AND METHOD FOR REDUCING BLADE OFF LOADS

Gas turbine engine airfoil

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

Gas turbine engine with optimized fan, core passage inlet, and compressor forward stage diameter ratios

Stator vane segment for a turbomachine

Dilution holes for gas turbine engines

Integrally bladed rotor having double fillet

Method and configuration for improved variable vane positioning

Inlet pre-swirl gas turbine engine

FAN WHEEL FOR AN AXIAL FAN

Rotatable valve for turbocharger system with plural volute members

Sealing assembly for a gas turbine

Fan blade surface features

Turbo fan and air conditioner including same

Gas turbine engine component incorporating a seal slot

Blockage-resistant vane impingement tubes and turbine nozzles containing the same

Turbomachine rotor blade

Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine

Gas turbine seal

Turbine exhaust hood

Diffuser for a turbine engine and method of forming same

RING SEGMENT WITH DIFFERENT RADII

Aero loading shroud sealing

Device for exhaust-gas routing having a turbocharger

TURBINE BLADE WITH CONTOURED TIP SHROUD

Blade comprising a shank, provided with a depressed portion

Gas turbine engine with dovetail connection having contoured root

Interwoven near surface cooled channels for cooled structures

Flowpath component for a gas turbine engine including a chordal seal

Volute pump

Composite translating cowl assembly for a thrust reverser system

Airfoil for a turbine engine

Fan blade surface features

Airfoil with stress-reducing fillet adapted for use in a gas turbine engine

Turbine

Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the first stage of a turbine

Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the second stage of a turbine

Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine

Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the sixth stage of a turbine

OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE VANE, IN PARTICULAR FOR A NOZZLE OF THE FIRST STAGE OF A TURBINE

Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbine

Particle extraction system for a gas turbine engine

Method for designing and building a wheel

Toroidal spinner aft flange

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

Cooling features with three dimensional chevron geometry

Turbine engine guide vane

Air bypass system for rotor shaft cooling

Heat exchanger for aircraft engine

Guide vane plate with a chamfered and a cylindrical edge region

Curved blade retention slot for turbine blade in a turbine disk

Turbomachine turbine blade squealer tip

Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern

Turbine rear frame for a turbine engine

Turbine housing and method of producing turbine housing

Inlet particle separator system with high curvature hub

Seal-plate anti-rotation in a stage of a gas turbine engine

GAS TURBINE ENGINE AIRFOIL

GAS TURBINE ENGINE AIRFOIL

Gas turbine engine airfoil

Turbomachine and turbine blade therefor

Gas turbine engine airfoil

Gas turbine engine airfoil

Turbine discs and methods of fabricating the same

Turbine disc assemblies and methods of fabricating the same

Cooling passages for a gas path component of a gas turbine engine

Gas turbine engine

Turbine engine stator vane, fan casing comprising such a vane, thrust reverser system of a turbine engine equipped with such a vane and turbine engine equipped with said vane, said casing or said system

Gas turbine engine with a vane having a cooling air turning nozzle

Propulsive assembly for aircraft comprising a turbojet fitted with a fan with removable blades

Compressor

Turbine slotted arcuate leaf seal

Aircraft propulsion system having at least one anti-fire tank

Self crystalline orientation for increased compliance

Axial flow compressor, gas turbine including the same, and stator blade of axial flow compressor

Cooling structure for stationary blade

Toggle seal for a rim seal

Turbine abradable layer with inclined angle surface ridge or groove pattern

Gas turbine engine airfoil

Bladed rotor for a gas turbine engine

Oil flow enhancer bearing assembly

Turbomachinery blade outer air seal

APPARATUS FOR MOUNTING A BLADE ON A TURBINE DISK

Shroud arrangement of a row of blades of stator vanes or rotor blades

Enhanced cooling for blade tip

Flange relief for split casing

Compound fillet for a gas turbine airfoil

Turbomachine part with a non-axisymmetric surface

Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

Gas turbine engine airfoil

Blade tip clearance control system including BOAS support

STEAM TURBINE DIFFUSER CONFIGURATION

Seal for gas turbine engine

Gas turbine engine truncated airfoil fillet

Mateface surfaces having a geometry on turbomachinery hardware

Coating pocket stress reduction for rotor disk of a gas turbine engine

Mini blind stator leakage reduction

Gas turbine engine component with conformal fillet cooling path

Pre-diffuser with multiple radii

Gas turbine engine

Gas turbine engine

Curved plate/fin heater exchanger

Turbine vanes with variable fillets

Heat exchanger assembly

Gas turbine blade configuration

Fan containing fan blades with a U-shaped slot having a decreased length planar section

COOLING SCHEME FOR A TURBINE BLADE OF A GAS TURBINE

Plate for metering flow

Gas turbine engine inlet

Incidence-tolerant, high-turning fan exit stator

Blade and blade dihedral angle

Rotary airfoil

Castellated latch mechanism for a gas turbine engine

Airfoil with thickened root and fan and engine incorporating same

Method and system for radial tubular duct heat exchangers

Segmented seal for a gas turbine engine

Gas turbine engine component having curved turbulator

Damper mass distribution to prevent damper rotation

Rotor and gas turbine engine including same

Duct

Methods and apparatus for passive thrust vectoring and plume deflection

Gas turbine engine component having contoured rib end

Gas turbine engine airfoil

Gas turbine engine airfoil total chord relative to span

Airfoil with improved cooling

Blade retaining ring for an internal shroud of an axial-flow turbomachine compressor

Turbine rotor

Heat exchanger for aircraft engine

Turbine blade

Blade for axial compressor rotor

Moving turbine blade

High order shaped curve region for an airfoil

Structural configurations and cooling circuits in turbine blades

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

Transition duct assembly with modified trailing edge in turbine system

Axial turbine wheel with curved leading edge

Methods and apparatus for passive thrust vectoring and plume deflection

Turbine nozzle having non-axisymmetric endwall contour (EWC)

Gas turbine nozzle trailing edge fillet

Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same

Convergent-divergent nozzle for a turbine engine

Plasma flow control inlet particle separator system

Turbojet fan blade

Exhaust mixer with offset lobes

Turbine blade

Heat exchanger for aircraft engine

Method for repairing a blade

Cooling hole with curved metering section

Rotor disc with fluid removal channels to enhance life of spindle bolt

Turbine engine blade, in particular for a one-piece bladed disk

Passive boundary layer bleed system for nacelle inlet airflow control

Seal assembly including grooves in an inner shroud in a gas turbine engine

Rear mounted wash manifold retention system

Rear mounted wash manifold and process

One-block bladed disk provided with blades with adapted foot profile

Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine

Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine

Rotor blade root section with cooling passage and method for supplying cooling fluid to a rotor blade

Aircraft nacelle comprising a deformable connection between an air intake and a power plant

Nozzle with guiding devices

Aeroengine thrust reverser arrangement

Turbine blade

Turbine engine blade

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

CMC blade attachment shim relief

Splicing of curved acoustic honeycomb

Combustor transition duct assembly with inner liner

System having blade segment with curved mounting geometry

Pipe having an upstream core having a sharp curvature

Shroud for a rotary machine and methods of assembling same

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

Turbine bucket with a core cavity having a contoured turn

High order shaped curve region for an airfoil

Turbine Nozzle Insert

Splicing of curved acoustic honeycomb

Gas turbine engine component with compound cusp cooling configuration

Cooling hole with curved metering section

Vane assembly for an axial flow turbine

Turbine and method for separating particulates from a fluid

Contoured honeycomb seal for turbine shroud

Exhaust-gas turbocharger with silencer

METAL GASKET FOR A GAS TURBINE ENGINE

System and method for conditioning air flow to a gas turbine

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

Piping assembly and method for connecting inner and outer shell in turbine system

Turbocharger

FLOW DISCHARGE DEVICE

Layout of a blisk

Curved Passages for a Turbine Component

Turbocharger and wheel housing

Method and system for sealing a dovetail

Stator of an axial compressor stage of a turbomachine

High camber stator vane

Compressor airfoil with tip dihedral

Steam valve device and steam turbine plant

ADJUSTABLE RING

Turbine rotor blade and turbo machine

Curved cooling passages for a turbine component

Guide vane for a turbo-compressor, guide vane arrangement, turbo-compressor, motor vehicle and method

MULTI-STAGE RADIAL TURBINE

BEARING DEVICE, BEARING UNIT, AND ROTARY MACHINE

Turbine and turbine rotor blade

Turbine rotor

Turbine blade tip shroud for use with a tip clearance control system

Air turbine starter inlet housing assembly airflow path

Compressor rectifier architecture

Spring loaded seal assembly for turbines

CURVED LABYRINTH SEALS

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

Gas turbine engine with non-axisymmetric surface contoured vane platform

Apparatus for cooling a platform of a turbine component

Turbocharger

Exhaust diffuser

Axial turbo engine with low gap losses

Stator blade for a turbomachine, especially a stream turbine

Frequency-tunable bracketless fluid manifold

Rotor for an axial-throughflow turbomachine and moving blade for such a rotor