MITIGATION STRATEGY FOR AIRFOIL CRACKS FOR INTEGRALLY BLADED ROTORS

TURBINE BLADE TIP SHROUD WITH AXIALLY OFFSET CUTTER TEETH, AND RELATED SURFACE PROFILES AND METHOD

GUIDE VANE ELEMENT FOR A COMPRESSOR OF A TURBOMACHINE, GUIDE VANE CLUSTER AND TURBOMACHINE

MOTORIZED COMPRESSOR DEVICE WITH AIR BEARING HAVING REDUCED AXIAL AND RADIAL STACK-UP

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

GAS TURBINE ENGINE

GAS TURBINE ENGINE

INSERTION OF CERAMIC MEMBERS FOR GAS PATH ENDWALL CONTOURING

GAS TURBINE ENGINE

GAS TURBINE ENGINE BLADING COMPRISING A BLADE AND A PLATFORM WHICH HAS AN INTERNAL FLOW-INTAKE AND FLOW-EJECTION CANAL

TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES

GAS TURBINE ENGINE

BLADING ASSEMBLY FOR A TURBOMACHINE AND TURBOMACHINE

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

TURBINE TIP SHROUD REMOVAL FEATURE

ROTOR DISK, TURBINE BLADE, AND TURBINE BLADE ASSEMBLY EQUIPPED WITH THESE

RADIAL TURBINE IMPELLER

AERONAUTICAL PROPULSION SYSTEM

TURBINE BLADE TIP SHROUD WITH AXIALLY OFFSET CUTTER TEETH, AND RELATED SURFACE PROFILES AND METHOD

Geometric approach to stress reduced intra-flow path shrouds for tuning modal responses in ram air turbine rotors

TURBINE BLADE FOR AN AIRCRAFT TURBOMACHINE, PROVIDED WITH A CHANNEL FOR EJECTING A PRIMARY FLOW TOWARDS AN INTER-LIP CAVITY

Flow deflector for aperture in gas turbine engine flowpath wall

Rotor blade and rotor blade assembly for a turbomachine

Fairing element for surrounding an obstacle in a fluid flow

GUIDE VANE ARRANGEMENT FOR A TURBOMACHINE, COMPRESSOR MODULE, AND TURBOMACHINE

Intermediate casing for a gas turbine engine

TURBINE TIP SHROUD REMOVAL FEATURE

Turbine vane, and turbine and gas turbine including same

Blade set and blisk

Blade for a turbine engine, and associated turbine engine

Turbine blade tip shroud with axially offset cutter teeth, and related surface profiles and method

Turbine blade tip shroud with protrusion under wing

ADDITIVE MANUFACTURED COMPONENTS INCLUDING INTEGRALLY FORMED PASSAGES, CHANNELS, AND CONDUITS, AND METHODS OF FORMING SAME

Airfoil having a spline fillet

Geometric approach to stress reduced intra-flow path shrouds for tuning modal responses in ram air turbine rotors

Turbine shroud with containment features

Shaft-mounted slinger for electric motor

Turbine blade and steam turbine including the same

Turbine blades including aero-brake features and methods for using the same

TURBINE BLADE WITH NON-AXISYMMETRIC FORWARD FEATURE

Compressor stator with leading edge fillet

SNUBBER SHROUD CONFIGURATIONS

MOTORIZED COMPRESSOR DEVICE WITH AIR BEARING HAVING REDUCED AXIAL AND RADIAL STACK-UP

Core duct assembly

Gas turbine blade for re-using cooling air and turbomachine assembly and gas turbine comprising the same

Aerofoil assembly and method

Nozzle with slash face(s) with swept surfaces joining at arc with peak aligned with stiffening member

Channeling furrow upstream of a blade

Turbomachine nozzle with an airfoil having a curvilinear trailing edge

SYSTEM FOR AN IMPROVED STATOR ASSEMBLY

Turbine stage platform with endwall contouring incorporating wavy mate face

Composite gas turbine engine component with lattice

High pressure turbine blade airfoil profile

TURBINE ENGINE

Non-axisymmetric end wall contouring with forward mid-passage peak

Non-axisymmetric end wall contouring with aft mid-passage peak

Core duct assembly

Turbine engine airfoil and method

Axial flow turbine

Turbine blades having damper pin slot features

Mate face arrangement for gas turbine engine components

Unitary body turbine shroud for turbine systems

Unitary body turbine shrouds including internal cooling passages

Unitary body turbine shrouds including structural breakdown and collapsible features

Fan blade

Shaft-mounted slinger for electric motor

Composite gas turbine engine component with lattice structure

Axial flow turbomachine and blade thereof

Compressor stator with leading edge fillet

Blade structure for turbomachine

Second stage turbine blade

Airfoil with trailing edge rounding

GAS TURBINE

Endwall Controuring

METHOD FOR MODIFYING A TURBINE

Combustion chamber arrangement and a gas turbine engine comprising a combustion chamber arrangement

Endwall contour

Edge profiles for tip shrouds of turbine rotor blades

Tip shroud fillets for turbine rotor blades

Gas turbine engine with ultra high pressure compressor

Passageway between a shroud and a rotor platform in a turbine engine

Axial flow rotating machine and diffuser

Gas turbine engine having a mistuned stage

Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interface

Two portion cooling passage for airfoil

Method of forming cooling passage for turbine component with cap element

Turbine module for a turbomachine

Turbine blade of a turbine blade ring

Aircraft propulsion system comprising a member covered with a grooved structure

Asymmetrical shroud for a compressor of a turbine engine

Shroud having elevations, for a turbomachine compressor

Compressor for turbine engine

TURBINE BLADE

Blade and rotor for a turbomachine and turbomachine

Geared gas turbine engine

Gas turbine engine blade containment system

Compressor and gas turbine including the same

Mistuned compressor rotor with hub scoops

GAS TURBINE

Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile

Hub for propeller having variable-pitch blades, with radial and axial dimensioning variation

Vane assembly of a gas turbine engine

Rotor blade having anti-wear surface

Integrally bladed rotor having double fillet

Turbomachine airfoil array

Airfoil assembly with a scalloped flow surface

Turbine center frame

Turbine blade including balanced mateface condition

Turbine nozzle airfoil profile

Contouring of an airfoil array platform

Endwall contouring for a turbomachine

Turbine nozzle airfoil profile

Airfoil shape for a turbine rotor blade

Airfoil shape for a turbine rotor blade

Airfoil shape for a turbine rotor blade

Contouring a blade/vane cascade stage

Centrifugal compressor impeller and compressor comprising said impeller

Contouring a blade/vane cascade stage

Methods for assembling a unitary flow path structure

Airflow straightening assembly having improved aerodynamic performances

Thrust-ring and rotor fan system

Turbine blades having damper pin slot features and methods of fabricating the same

Contouring a blade/vane cascade stage

Compressor with segmented inner shroud for an axial turbine engine

Turbofan nacelle assembly with flow disruptor

TURBINE BLADE WITH CONTOURED TIP SHROUD

Turbine engine assembly with a component having a leading edge trough

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

Turbine engine part with non-axisymmetric surface

Thrust ring and rotor fan system with passive leading edge slats

Rotary machine

Stator with adjustable vanes for the compressor of an axial turbine engine

Gas turbine engine having support structure with swept leading edge

Rotor blade for a gas turbine engine

Fitted platform for a turbine engine fan, and a method of fabricating it

COMBUSTOR INLET MIXING SYSTEM WITH SWIRLER VANES HAVING SLOTS

Cooling passage for gas turbine system rotor blade

Gas turbine engine transition duct and turbine center frame

Blade with a platform and a hollow bumper

Turbine

Turbine nozzle having non-axisymmetric endwall contour (EWC)

Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile

BLADE CASCADE AND TURBOMACHINE

End wall contour for an axial flow turbine stage

Turbine rear frame for a turbine engine

Controlled convergence compressor flowpath for a gas turbine engine

Gas turbine engine components with optimized leading edge geometry

Rotor blade cooling circuit

Guide vane segment for a turbomachine

Blade channel, blade cascade and turbomachine

Turbine engine flow path

Blade for a turbomachine impeller and method for modelling the same

Compressor stator vane, axial flow compressor, and gas turbine

End wall configuration for gas turbine engine

FLOW PATH TRENCHES AND METHODS OF FORMING THE SAME

Compressor variable vane assembly

Device and method for producing a blade airfoil

System and method for creating a fluidic barrier with vortices from the upstream splitter

METHOD FOR MACHINING A WORKPIECE HAVING AN IRREGULAR EDGE

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

Fan blade platform spacer mounting

Turbomachine component with non-axisymmetric surface

Blade or vane row and gas turbine

Trench cooling of airfoil structures

Article having cooling passage with undulating profile

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

Gas turbine guide vane element

Gas turbine engine integrally bladed rotor with asymmetrical trench fillets

Blade, bladed wheel, turbomachine, and a method of manufacturing the blade

Rotor assembly with wear member

Blade with tip shroud

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

TURBINE INTRUSION LOSS REDUCTION SYSTEM

Blade or vane arrangement for a gas turbine engine

Compound fillet varying chordwise and method to manufacture

Turbine vane with heat shield

Compound fillet for a gas turbine airfoil

TURBINE BUCKET PLATFORM FOR CONTROLLING INCURSION LOSSES

Production methods of gas turbine

Turbomachine part with a non-axisymmetric surface

Variable area vane endwall treatments

Endwall countouring trench

Fan root endwall contouring

Turbomachine flow path having circumferentially varying outer periphery

Metal leading edge on composite blade airfoil and shank

Gas turbine and mounting method

Gas turbine and mounting method

Mateface surfaces having a geometry on turbomachinery hardware

Axial compressor rotor incorporating splitter blades

Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades

Non-axisymmetric fan flow path

Airfoil fillet

Gas turbine engine component with conformal fillet cooling path

Turbomachine having an annulus enlargment and airfoil

Vane assembly of a gas turbine engine

Compressor end-wall treatment with multiple flow axes

Turbine arrangement

Turbine vanes with variable fillets

Row of aerofoil members

Blading

Endwall contouring for airfoil rows with varying airfoil geometries

Turbomachine blade tip shroud

Gas turbine subassembly

Turbine vane with non-uniform wall thickness

Gas turbine engine airfoil platform edge geometry

Gas turbine engine blade containment system

Aerodynamic track fairing for a gas turbine engine fan nacelle

Gas turbine engine having a mistuned stage

Axial flow rotating machine and diffuser

Fan exit guide vane platform contouring

Pretrenched rotor for gas turbine engine

Gas turbine engine airfoil curvature

Gas turbine engine component having contoured rib end

Platform with curved edges adjacent suction side of airfoil

Platform with curved edges

Variable guide vane extended variable fillet

Gas turbine compressor

Compressor variable vane assembly

Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan

Gas turbine engine having support structure with swept leading edge

Method for producing a tandem blade wheel for a jet engine and tandem blade wheel

Group of blade rows

Multistage axial flow compressor

Relating to centrifugal pump impellers

Contoured flowpath surface

Gas turbine including a contoured end wall section of a rotor blade

Part to modify the profile of an aerodynamic jet

Compressor variable vane assembly

Blade with 3D platform comprising an inter-blade bulb

Industrial gas turbine exhaust system with area ruled exhaust path

Industrial gas turbine exhaust system with splined profile tail cone

Industrial gas turbine exhaust system diffuser inlet lip

Compressor arrangement

Vane array with one or more non-integral platforms

Gas turbine engine flow path geometry

Engine duct and aircraft engine

Impeller for a fluid energy machine

Turbine hub with surface discontinuity and turbocharger incorporating the same

Turbocharger shroud with cross-wise grooves and turbocharger incorporating the same

Turbine bucket having non-axisymmetric base contour

Turbine bucket with endwall contour and airfoil profile

Exhaust centerbody for a turbine engine

TURBINE BLADE OR VANE WITH SEPARATE ENDWALL

Alternating nozzles for radial inflow turbine

Blade cascade and turbomachine

Turbomachine airfoil positioning

Airfoil for gas turbine, blade and vane

Blade cascade and continuous-flow machine

Blade cascade for turbo machine

Gas turbine engine

Compressor stator with contoured endwall

Turbomachine bucket having flow interrupter and related turbomachine

LPC flowpath shape with gas turbine engine shaft bearing configuration

Airfoil member and composite platform having contoured endwall

Airfoil assembly with paired endwall contouring

Fillet for use with a turbine rotor blade tip shroud

Turbine wheel, a turbine and use thereof

Centrifugal pump impellers

Turbine intrusion loss reduction system

Endwall contouring

Endwall contouring

Impeller and electric-motor driven water pump having the same

Compressor fairing segment

Impulse turbine for use in bi-directional flows

Gas turbine and outer shroud

Self-centring cage nut

Blade cascade with side wall contours and continuous-flow machine

Blade cascade with side wall contours and continuous-flow machine

Gas turbine

Rotating airfoil component with platform having a recessed surface region therein

Shroud for a rotary machine and methods of assembling same

AIRFOIL MATEFACE SEALING

Airfoil and platform assembly for subsonic flow

Airfoil and platform assembly for supersonic flow

Blade for a turbomachine, blade arrangement, and turbomachine

Flow path structure and gas turbine exhaust diffuser

Scalloped surface turbine stage

Blade ring segment having an annular space delimiting surface having a wavy height profile

EXHAUST DIFFUSER FOR TURBINE

Scalloped surface turbine stage with purge trough

Low loss airfoil platform trailing edge

Vane assembly for an axial flow turbine

Turbofan flow path trenches

Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling

Compressor and a turbine engine with optimized efficiency

Blading

Blading

Blade skirt

Blade for a gas turbine engine

Turbine bucket platform leading edge scalloping for performance and secondary flow and related method

Turbine bucket platform shaping for gas temperature control and related method

Non axis-symmetric stator vane endwall contour

Blade row for a turbomachine

Tip shroud assembly with contoured seal rail fillet

Vortex generators for generating vortices upstream of a cascade of compressor blades

Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow losses

Air turbine starter

Flow directing member for gas turbine engine

Turbocharger vane

Turbine blade or vane with separate endwall