TURBINE ENGINE VANE WITH MULTI-BAFFLE ARRANGEMENT

GAS TURBINE ENGINE NOZZLE

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

STATOR BLADE AND GAS TURBINE PROVIDED WITH SAME

INLET GUIDE VANE AND ROTARY MACHINE

TANDEM STATOR

GUIDE VANE

BLADING ASSEMBLY FOR A TURBOMACHINE AND TURBOMACHINE

LOCALIZED REWORK USING DIRECTED ENERGY DEPOSITION

AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF

CARTRIDGE FOR PULSE-SEPARATED VARIABLE TURBINE GEOMETRY TURBOCHARGERS

VANE ARRAY STRUCTURE WITH RECESSED STATOR VANES

TURBINE AIRFOILS

Compressor bleed pressure recovery

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A STATOR VANE INTEGRATED INTO AN UPSTREAM PART OF A MOUNTING PYLON OF REDUCED HEIGHT

Platform outside diameter channel for dual supply pressure vane applications

Centrifugal pump for pumping a multiphase suspension and a gas removal device for use in a centrifugal pump

Guide vanes in a gas turbine engine

Engine systems and methods

CMC trailing edge 3D weaved cross brace

Exhaust diffuser strut for reducing flow separation

Stator vane for a turbomachine

Air turbine starter with shaped vanes

Components for gas turbine engines

Integrated stator-fan frame assembly

OUTLET GUIDE VANE COOLER

Bi-cast trailing edge feed and purge hole cooling scheme

Adaptive vertical lift engine (AVLE) fan

Turbine and turbocharger

COMPOSITE LAYER SYSTEM HAVING AN ADDITIVELY MANUFACTURED SUBSTRATE AND A CERAMIC THERMAL PROTECTION SYSTEM

Nozzle guide vane

High temperature capable additively manufactured turbine component design

Gas turbine blade arrangement

Gas turbine engine airfoil fairing with rib having radial notch

Air turbine starter with shaped vanes

Method for coating a turbomachine guide vane, associated guide vane

Turbine guide vane

Variable guide vane for gas turbine engine

Variable-pitch stator vane for an aircraft turbine engine

Turbine stator blade and steam turbine

Engine systems and methods

System and method for air injection passageway integration and optimization in turbomachinery

Profiled structure for an aircraft or turbomachine

Multi-material vane for a gas turbine engine

Multi-material vane for a gas turbine engine

CMC AIRFOIL WITH SHARP TRAILING EDGE AND METHOD OF MAKING SAME

Exhaust diffuser strut for reducing flow separation

Turbine nozzle airfoil and/or trailing edge profile

Turbine nozzle airfoil and/or trailing edge profile

Nozzle vane

Multi-stage centrifugal compressor, casing, and return vane

Turbine vane with dust tolerant cooling system

Turbine vane with dust tolerant cooling system

Turbomachine nozzle with an airfoil having a circular trailing edge

Turbomachine nozzle with an airfoil having a curvilinear trailing edge

Method for creating an aircraft turbomachine vane using additive manufacturing

First-stage stator vane for gas turbine, gas turbine, stator vane unit for gas turbine, and combustor assembly

SYSTEM FOR AN IMPROVED STATOR ASSEMBLY

Turbine blade and gas turbine

Gas turbine engine airfoils having multimodal thickness distributions

Steam turbine

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

Turbine incorporating endwall fences

Adaptive vertical lift engine (AVLE) fan

Stator vane of fan or compressor

Lost core structural frame

Airfoils having tapered tip flag cavity and cores for forming the same

Trailing edge pressure and flow regulator

Blade for a gas turbine engine

Turbine nozzle and axial-flow turbine including same

Turbine component and methods of making and cooling a turbine component

Gas turbine engine airfoil

Ceramic matrix composite component cooling

Gas turbine engine

Airfoil cooling circuit

Vane platform leading edge recessed pocket with cover

Integral half vane, ringcase, and id shroud

Internally cooled airfoil

Reinforced axial diffuser

System and Method for Airfoil Vibration Control

Variable vane devices containing rotationally-driven translating vane structures and methods for the production thereof

Turbine component and methods of making and cooling a turbine component

Turbine nozzle with CMC aft band

Turbine vane with dust tolerant cooling system

Guide vane arrangement for use in a turbine

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

Trailing edge cooling for a turbine blade

Turbocharger, nozzle vane for turbocharger, and turbine

Turbine vane having improved flexibility

AIRFOILS FOR GAS TURBINE ENGINES

Baffle for a component of a gas turbine engine

Engine systems and methods

Dual cavity baffle

Repair member for a vane assembly of a gas turbine and method for repairing a damaged vane of a vane assembly of a gas turbine

Gas turbine engine airfoil trailing edge suction side cooling

Technique for controlling rotating stall in compressor for a gas turbine engine

Method of forming a component

Gas turbine engine cooling component

Steam turbine

Modified J type cantilevered vane and gas turbine having the same

Shroud having elevations, for a turbomachine compressor

Turbine airfoil with internal cooling channels having flow splitter feature

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

INLET GUIDE VANE HAVING A VARIED TRAILING EDGE GEOMETRY

Steam turbine

Hot section engine components having segment gap discharge holes

Vane for variable area turbine

Airfoil having end wall contoured pedestals

Turbine vane cluster including enhanced vane cooling

TURBINE VANE CLUSTER INCLUDING ENHANCED PLATFORM COOLING

Gas turbine engine with diversion pathway and semi-dimensional mass flow control

Fan wheel, fan, and system having at least one fan

Flow arrangement for placing in a hot gas duct of a turbomachine

Turbomachine airfoil

Ice detection

Aircraft incorporating a thrust recovery system using cabin air

Turbine engine component with an insert

Airfoil assembly with a scalloped flow surface

Inlet pre-swirl gas turbine engine

Coated turbine component and method for forming a component

Ceramic matrix composite (CMC) hollow blade and method of forming CMC hollow blade

Turbine engine with variable effective throat

Engine component with insert

Method of repairing a component using an additive manufacture replacement coupon, and alloy for additive manufacturing

Gas turbine with a radial-to-axial intake, variable-angle inlet guide vane therefore, and method of operation

Turbine blade, gas turbine, intermediate product of turbine blade, and method of manufacturing turbine blade

Blade comprising a trailing edge having three distinct cooling regions

Turbine vane and gas turbine including the same

Turbine nozzle with CMC aft band

Turbine nozzle with CMC aft Band

Stator vanes including curved trailing edges

Vane cooling system

Turbomachine and turbine nozzle therefor

Cartridge for pulse-separated variable turbine geometry turbochargers

Method of manufacturing a coated turbine blade and a coated turbine vane

Gas turbine engine vanes

Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan

Variable vane devices containing rotationally-driven translating vane structures and methods for the production thereof

Hybrid airfoil cooling

Trailing edge pressure and flow regulator

Trailing edge configuration with cast slots and drilled filmholes

Flow path routing within a gas turbine engine

Blade, cut-back of blade or vane and gas turbine having the same

Turbofan nacelle assembly with flow disruptor

Turbine blade comprising an improved trailing-edge

Dual wall airfoil with stiffened trailing edge

Airfoil trailing edge segment

GAS TURBINE ENGINE BLEED CONFIGURATION

Radially diffused tip flag

INLET GUIDE WHEEL FOR A TURBO ENGINE

Airfoil with ceramic airfoil piece having internal cooling circuit

SELF-SEALING IMPINGEMENT COOLING TUBE FOR A TURBINE VANE

Gas turbine engine airfoils having multimodal thickness distributions

Turbine airfoil trailing edge coolant passage created by cover

Cooling circuits for a multi-wall blade

Cooling circuits for a multi-wall blade

Partially wrapped trailing edge cooling circuits with pressure side impingements

Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities

Turbine blade trailing edge with low flow framing channel

Systems for removing heat from turbine components

Impingement system for an airfoil

Impingement system for an airfoil

Stationary blades for a steam turbine and method of assembling same

Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end element

Internal cooling system with converging-diverging exit slots in trailing edge cooling channel for an airfoil in a turbine engine

Turbine vane with coupon having corrugated surface(s)

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

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

TURBOMACHINE COMPONENT HAVING A PLATFORM CAVITY WITH A STRESS REDUCTION FEATURE

Aerodynamic link in part of a turbine engine

Trailing edge ejection cooling

Ceramic matrix composite component cooling

Turbine component and methods of making and cooling a turbine component

Turbine component and methods of making and cooling a turbine component

Turbine component and methods of making and cooling a turbine component

System for an improved stator assembly

Gas turbine engine turbine vane baffle and serpentine cooling passage

Aerofoil body

Vane with spoiler

Internally cooled airfoil

Modulated hybrid variable area turbine nozzle for gas turbine engine

Airfoil having pedestals in trailing edge cavity

Article with improved coating system and methods of forming the same

Turbomachine blade, comprising a root with reduced stress concentrations

Airfoil trailing edge cooling

Gas turbine engine trailing edge ejection holes

Turbine nozzle having fillet, pinbank, throat region and profile

STATOR VANE

GAS TURBINE AEROFOIL TRAILING EDGE

Turbine airfoil trailing edge cooling passage

Turbine blade with optimised cooling at the trailing edge of same comprising upstream and downstream ducts and inner side cavities

Propeller fan and blower unit

Turbomachine and turbine nozzle therefor

Turbomachine and turbine blade therefor

Guide vane segment for a turbomachine

Trailing edge cooling for a turbine blade

Baffle for a component of a gas turbine engine

Multistage compressor with aerofoil portion profiled in a spanwise direction

Cooling of turbine blades and method for turbine blade manufacture

Air conditioner

Blade for a gas turbine and method of cooling the blade

Gas turbine components having non-uniformly applied coating and methods of assembling the same

LOCK-UP PREVENTION VANE FOR VARIABLE GEOMETRY TURBOCHARGER

Components with microchannel cooling

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

Lost core structural frame

Cooling structure for stationary blade

Turbine stator vane of ceramic matrix composite

Guide vane of a gas turbine engine, in particular of an aircraft engine

Erosion and wear protection for composites and plated polymers

Vehicle cooling fan with aerodynamic stator struts

Hot gas path component trailing edge having near wall cooling features

Gas turbine stator with winglets

Gas turbine engine airfoil

Method for forming components using additive manufacturing and re-melt

Compressor system and airfoil assembly

Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same

Airfoils

Compound fillet varying chordwise and method to manufacture

Compound fillet for a gas turbine airfoil

Gas turbine engine airfoil cooling configuration with pressure gradient separators

CMC AIRFOIL WITH SHARP TRAILING EDGE AND METHOD OF MAKING SAME

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

Method for manufacturing a propeller blade

Gas turbine axial compressor

Gas turbine engine diffuser cooling and mixing arrangement

Method of fabricating a reinforcing edge for a blade and reinforcing edge obtained by the method

Method for the high-temperature shaping of a metal blade reinforcement

Diffuser for a forward-swept tangential flow compressor

Turbine Vane With Platform Rib

Gas turbine vane

Hybrid airfoil for a gas turbine engine

Cooling of engine components

Turbomachine blade, comprising intersecting partitions for circulation of air in the direction of the trailing edge

Stress Reduction For Film Cooled Gas Turbine Engine Component

High-modulus coating for local stiffening of airfoil trailing edges

Vacuum pump

Multi-piece turbine airfoil

Gas turbine engine component

Blading

Gas turbine engine airfoil trailing edge suction side cooling

Incidence-tolerant, high-turning fan exit stator

Turbine vane with variable trailing edge inner radius

Structural frame integrated with variable-vectoring flow control for use in turbine systems

Turbine vane with non-uniform wall thickness

Turbomachine component with a stress relief cavity

Undulating stator for reducing the noise produced by interaction with a rotor

Flow path routing within a gas turbine engine

Method for forming components using additive manufacturing and re-melt

Method for forming a directionally solidified replacement body for a component using additive manufacturing

Variable vane and seal arrangement

Gas turbine blade

Group of blade rows

Nozzle endwall film cooling with airfoil cooling holes

Compressor variable vane assembly

FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE

Steam turbine

ATR axial V-groove

Integrated nozzle and plug

ATR full ring sliding nacelle

ATR guide pins for sliding nacelle

Transition duct assembly with modified trailing edge in turbine system

Gas turbine nozzle trailing edge fillet

Method and system for providing cooling for turbine components

Diffuser with strut-induced vortex mixing

Turbine guide wheel

Trailing edge cooling arrangement for an airfoil of a gas turbine engine

Method for making gas turbine engine ceramic matrix composite airfoil

Noise attenuation in rotating blades

Turbomachinery stationary vane arrangement for disk and blade excitation reduction and phase cancellation

Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor

Turbine blade

Trenched cooling hole arrangement for a ceramic matrix composite vane

Turbomachine nozzle having fluid conduit and related turbomachine

Reduction of equally spaced turbine nozzle vane excitation

Gas turbine diffuser blowing method and corresponding diffuser

Impulse turbine for use in bi-directional flows

Crack-resistant environmental barrier coatings

Continuous-flow machine with at least one guide vane ring

Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways

Static vane assembly for an axial flow turbine

Gas turbine engine component with discharge slot having oval geometry

Cooling for a turbine airfoil trailing edge

Turbomachinery component cooling scheme

Asymmetrically shaped trailing edge cooling holes

METHOD OF REPAIRING A TURBINE COMPONENT

Method of making a piece of metal reinforcement

Turbine airfoil trailing edge cooling slots

Trailing edge or tip flag antiflow separation

Hybrid airfoil for a gas turbine engine

Gas turbine annular diffusor

Ceramic core tapered trip strips

Noise-reduced turbomachine

Gas turbine engine exhaust diffuser including circumferential vane

Turbine blade incorporating trailing edge cooling design

Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine

Turbine airfoil and method for thermal barrier coating

Process and refractory metal core for creating varying thickness microcircuits for turbine engine components

EXHAUST GAS DIFFUSER