OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH GUIDE VANE STRUCTURE RECEPTACLE

SYSTEM AND METHOD FOR OVERHAULING A TURBINE COMPONENT

TURBOCOMPRESSOR UNIT FOR AN AIRCRAFT PROPULSION SYSTEM

SYSTEM AND METHOD FOR OVERHAULING A TURBINE COMPONENT

PERFORMING VANE CLASSIFICATION FOR TURBINE ENGINES USING STRUCTURED LIGHT THREE-DIMENSIONAL (3D) SCANS

STEAM TURBINE BLADE, STEAM TURBINE, AND METHOD FOR MANUFACTURING STEAM TURBINE BLADE

TURBINE AND TURBOCHARGER

VANE ASSEMBLY FOR A GAS TURBINE ENGINE SYSTEM

METHOD FOR REPAIRING A GAS TURBINE ENGINE COMPONENT

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR CONVENTIONAL GAS TURBINE ENGINES

STATOR VANE WITH MULTI-ACCESS COOLING AIR FEED PASSAGE

GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES

TURBINE ENGINE FOR AIRCRAFT WITH HEAT EXCHANGER

Deflector Device and Turbine Guide Shoe

TURBINE ENGINE WITH COMPOSITE AIRFOILS

TURBINE ENGINE WITH COMPOSITE AIRFOILS

GAS TURBINE ENGINE WITH RELATIVE CLOCKING OF BIFURCATIONS

TURBINE ENGINE WITH COMPOSITE AIRFOILS

OUTLET GUIDE VANE FOR A GAS TURBINE ENGINE AND METHOD

REINFORCEMENT FOR A COMPOSITE BLADE OF A TURBOMACHINE, COMPRISING A STACK OF PLIES

Turbine Dosing System

TRAILING MEMBER FOR A STRUT OF A GAS TURBINE EXHAUST DIFFUSER, STRUT ASSEMBLY, AND GAS TURBINE EXHAUST DIFFUSER

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

ASSEMBLY FOR AN AIRCRAFT TURBOMACHINE, AND AIRCRAFT TURBOMACHINE

METAL COUPON WITH POROUS REGION FOR COMPONENT AND COMPONENT WITH SAME

CYCLONIC PARTICLE SEPARATOR

STATOR VANE COMPRISING A HEAT PIPE

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

SYSTEM AND METHOD FOR CONTOURING EDGES OF AIRFOILS

VIBRATIONAL DAMPING ASSEMBLY FOR A TURBOMACHINE EXHAUST DIFFUSER

TURBINE STATOR VANE

TURBINE ENGINE WITH COMPSITE AIRFOILS

Turbine engine with composite airfoils

TURBINE ENGINE WITH COMPOSITE AIRFOILS

UNDUCTED THRUST PRODUCING SYSTEM ARCHITECTURE

TURBINE ENGINE WITH COMPOSITE AIRFOILS

Composite guide vane with insert

Pipe diffuser for centrifugal compressor

THROUGH THICKNESS REINFORCEMENT

GAS TURBINE ENGINE WITH BLEED DIFFUSER BAFFLES

METHOD FOR SIMULATING PARTICLE IMPACT

SPLITTER FOR AERONAUTIC TURBOMACHINE

Component for a turbine engine with a cooling hole

ELECTRIC FAN AND ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT

TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT

Engine strut flow control

Gas turbine engine component having an airfoil with internal cross-ribs

METHOD OF MANUFACTURING A TURBINE COMPONENT

Sectioned engine structure for a gas turbine engine

PRE-CERAMIC THERMAL BARRIER FOR GAS TURBINE ENGINE COMPONENTS

Stator blade and gas turbine comprising same

MODULE FOR A TURBOMACHINE

Centrifugal compressor and turbocharger

Fiber Reinforced Polymer Blade

STATOR RETENTION OF GAS TURBINE ENGINE

Engine mount system for a gas turbine engine

PERFORMING VANE CLASSIFICATION FOR TURBINE ENGINES USING STRUCTURED LIGHT THREE-DIMENSIONAL (3D) SCANS

Flow deflector for aperture in gas turbine engine flowpath wall

Radial turbine nozzle and method for assembling the same

Front section stiffness ratio

COMPOSITE COMPONENTS AND METHODS FOR PREVENTING FLOW FROM INFILTRATED COMPONENT DURING RE-INFILTRATION

Turbine stator vane and steam turbine

System and method for repairing high-temperature gas turbine components

System and method for contouring edges of airfoils

Engine airfoil metal edge

Gas turbine engine with third stream

Gas turbine engine with third stream

Unducted propulsion system

Exhaust diffuser strut for reducing flow separation

Vane forward rail for gas turbine engine assembly

Turbine housing

Gas turbine engines with improved guide vane configurations

Stator vane segment and steam turbine provided with same

Seal for a rotor

Forming lined cooling aperture(s) in a turbine engine component

Exhaust collector conversion system and method

METHODS OF PROTECTING METALLIC COMPONENTS AGAINST CORROSION USING CHROMIUM-CONTAINING THIN FILMS

DOVETAILED COMPOSITE OUTLET GUIDE VANE ASSEMBLY AND METHOD OF ASSEMBLING THEREOF

Stationary turbine blade and steam turbine

Sectioned engine structure for a gas turbine engine

Turbocharger

Turbine engine stator control valve comprising a continuous and free sealing ring

Composite turbomachine vane and method for manufacturing same

ARRANGEMENT OF PEDESTALS OF VARYING ASPECT RATIO FOR DUAL-WALL COOLING OF AN AIRFOIL

Turbine vane, and turbine and gas turbine including same

Unducted propulsion system

Turbocharger turbine housing

Multilayer protective coating systems for gas turbine engine applications and methods for fabricating the same

Acoustic turbofan airfoil apparatus

CMC gas turbine engine component with separated fiber plies

Front section stiffness ratio

ASSEMBLY FOR A TURBINE ENGINE

STEAM TURBINE MEMBER

Clearance control assembly

Method for manufacturing a turbine engine vane and turbine engine vane

Seal for combustion apparatus

Through thickness reinforcement

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

Split-line stator vane assembly

CMC vane sealing arrangement

Hybrid Thermal Barrier Coating

Blade element

TURBINE

High temperature capable additively manufactured turbine component design

Engine having variable pitch outlet guide vanes

Ceramic component with support structure

Ceramic matrix composite articles having different localized properties and methods for forming same

Turbine engine with soaring air conduit

Engine airfoil metal edge

Impulse turbine and turbine device

Methods for depositing coatings on aerospace components

Gas turbine engine nozzles

Diffuser bleed assembly

Turbine vane and gas turbine comprising same

Sealing apparatus for an axial flow turbomachine

Secondary flow suppression structure

POST-SHUTDOWN ENGINE HEAT REMOVAL SYSTEM

Fiber-reinforced aircraft component and aircraft comprising same

Gas turbine blade repair method

Gas turbine engine airfoil

Steam turbine stator vane, steam turbine, and production method for steam turbine stator vane

Separation nozzle for aeronautic turbomachine

Electrical strut for a turbine engine

Rotating machine

Turbine vane, and turbine and gas turbine including the same

Turbine stator vane and gas turbine

Airfoil having a spline fillet

FLUID FLOW GUIDING DEVICE AND A GAS TURBINE ENGINE

Turbine engine vane equipped with a cooling circuit and lost-wax method for manufacturing such a vane

Rapid processing of laminar composite components

Component for a turbine engine with a cooling hole

System and method for repairing high-temperature gas turbine components

Axial turbine with two supply levels

TURBINE ENGINE WITH STRUTS

Gas Turbine Nozzle

Turbine engine component with deflector

Turbine blade and steam turbine including the same

Stator vane segment of axial turbine

Turbine nozzle and method of manufacture

Turbocharger

CMC vane with support spar and baffle

Impingement panel support structure and method of manufacture

Flexible support structure for a geared architecture gas turbine engine

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

Turbomachine stator

APPARATUS FOR GENERATING ENERGY

Exhaust baffle component for an air turbine assembly

SCREW ROCKET NOZZLE

Exhaust collector conversion system and method

Turbine stator blade

Reverse flow engine architecture

COBALT BASED ALLOY PRODUCT

Engine mount system for a gas turbine engine

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

Turbine module

Composite aerofoils

Airfoil having internally cooled wall with liner and shell

Spring loaded airfoil vane

Multi-material vane for a gas turbine engine

Multi-material vane for a gas turbine engine

Bypass turbomachine

Vane support system with seal

Systems and methods for identifying and mitigating gas turbine component misalignment using virtual simulation

Blade and gas turbine

INTEGRATED CASTING CORE-SHELL STRUCTURE FOR MAKING CAST COMPONENT WITH NOVEL COOLING HOLE ARCHITECTURE

Adhesive bonded composite-to-metal hybrid vanes and method of manufacture

Methods of protecting metallic components against corrosion using chromium-containing thin films

METHOD FOR CONTROLLING FLOW SEPARATION ON SUCTION SURFACE OF STATOR BLADE OF AXIAL COMPRESSOR/FAN BY MEANS OF MICRO AIR INJECTION

Exhaust diffuser strut for reducing flow separation

Turbine nozzle airfoil profile

Turbine nozzle airfoil and/or trailing edge profile

Turbine nozzle airfoil and/or trailing edge profile

Turbofan engine

Vane core assemblies and methods

Turbine nozzle for a turbine engine, comprising a passive system for reintroducing blow-by gas into a gas jet

Vane arc segment load path

Flow guide, steam turbine, inside member, and method for manufacturing flow guide

Gas turbine engine outlet guide vane assembly

Contoured stop for variable area turbine

Turbine component made from superalloy comprising rhenium and associated manufacturing process

CMC component with integral cooling channels and method of manufacture

Ceramic matrix composite component including cooling channels in multiple plies and method of producing

Ceramic matrix composite component including counterflow channels and method of producing

Blade of steam turbine and steam turbine

Exhaust hood and steam turbine

ROTARY ENGINE SYSTEM WITH WORK DONE IN MULTIPLE CAVITIES

Fuel nozzle of gas turbine combustor and manufacturing method thereof, and gas turbine combustor

Vane with collar

Method of selectively bonding braze powders to a surface

Stator retention of gas turbine engine

Ceramic airfoil with cooling air turn

Turbine vane assembly having ceramic matrix composite airfoils and metallic support spar

Rotor blade, rotor unit, and rotating machine

Gas turbine engine airfoil

ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE

Mount for an airfoil

HIGH OXIDATION-RESISTANT ALLOY AND GAS TURBINE APPLICATIONS USING THE SAME

Gas turbine for aircraft

Actuation Assembly for Concentric Variable Stator Vanes

Spline for a turbine engine

CONTROL STAGE BLADES FOR TURBINES

Sealing arrangement with pressure-loaded feather seals to seal gap between components of gas turbine engine

Electric motor having an integrated cooling system and methods of cooling an electric motor

Fiber-reinforced aircraft component and aircraft comprising same

Multi-purpose anti-rotation lock pin

Engine component with set of cooling holes

Turbine vane, and turbine and gas turbine including the same

Nacelle thrust reverser compression rod supporting system

Diffuser pipe with axially-directed exit

Turbine

Systems and methods for manufacturing film cooling hole diffuser portion

Turbine vane assembly having ceramic matrix composite components with sliding support

Ceramic matrix composite aerofoil with impact reinforcements

Rapid processing of laminar composite components

Methods for depositing anti-coking protective coatings on aerospace components

Chordal seal

Turbine section assembly with ceramic matrix composite vane

Vane core assemblies and methods

Airfoil with baffle showerhead and cooling passage network having aft inlet

PROTECTION AND ENHANCEMENT OF THERMAL BARRIER COATING INTEGRITY BY LITHOGRAPHY

Manufacturing method of turbine housing

Unducted thrust producing system architecture

Stator vane of fan or compressor

Gas turbine engine airfoil

Flexible support structure for a geared architecture gas turbine engine

ELECTRODEPOSITED NICKEL-CHROMIUM ALLOY

NICKEL-CHROMIUM-ALUMINUM COMPOSITE BY ELECTRODEPOSITION

Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

Turbine shroud cooling

Turbine engine airfoil assembly

Method of making airfoils

Unducted thrust producing system

Blade equipped with a cooling system, associated guide vanes assembly and associated turbomachine

Method for smoothing a surface of a component

Inter-turbine ducts with flow control mechanisms

Methods for depositing coatings on aerospace components

Refractory metal core finishing technique

High velocity fluid nozzle

Flexible support structure for a geared architecture gas turbine engine

Method for manufacturing a turbine engine vane made of a composite material, resulting vane and turbine engine including same

Diffuser case support structure

Turbine blade and gas turbine

Gas turbine engine with integral combustion liner and turbine nozzle

Modular variable vane assembly

Turbine nozzle and axial-flow turbine including same

Axial flow turbomachine and blade thereof

Steam turbine

Heat shield for signature suppression system

Labyrinth seal with variable tooth heights

Reverse flow engine architecture

Engine family platform design

Gas turbine engine

Turbine shroud segment with flange-facing perimeter seal

Diffuser guide vane with deflector panel having curved profile

COMPONENT FOR A TURBINE ENGINE WITH A FILM HOLE

Ceramic matrix composite turbine nozzle shell and method of assembly

Method of processing a ceramic matrix composite (CMC) component

Method of resonant inspection for additive manufacturing

Turbine bucket having outlet path in shroud

Combustion section heat transfer system for a propulsion system

Internally cooled airfoil

Multifunctional nanocellular single crystal nickel for turbine applications

Method of forming CMC component cooling cavities

Aircraft having an aft engine

Steam turbine

System and Method for Airfoil Vibration Control

Floating, non-contact seal and dimensions thereof

Airfoil with seal between end wall and airfoil section

Gas turbine

Brazed blade track for a gas turbine engine

Turbine component and methods of making and cooling a turbine component

Flexible support structure for a geared architecture gas turbine engine

Flexible support structure for a geared architecture gas turbine engine

Dual-mode plug nozzle

Turbine shroud segment with side perimeter seal

Turbine shroud having ceramic matrix composite seal segment

Seal assembly for turbine engine component

GAS TURBINE ENGINE COMPONENT

Integrated strut-vane

Endwall Controuring

Vortex generators for turbine engine exhaust

Leading edge hybrid cavities for airfoils of gas turbine engine

SYSTEMS AND METHODS FOR THERMAL LOCATION OF COOLING HOLES

GAS TURBINE ENGINE COMPONENT COOLING CAVITY WITH VORTEX PROMOTING FEATURES

Flow control nozzle

Turbine engine component with vibration damping

Electric motor having an integrated cooling system and methods of cooling an electric motor

PRIMARY NOZZLE OF A TURBOMACHINE PRIMARY EXHAUST DUCT

TURBINE STATOR VANE WITH MULTIPLE OUTER DIAMETER PRESSURE FEEDS

Guide Baffle Of A Turbomachine And Method For Producing The Same

SCREW ROCKET NOZZLE

Airfoil of axial flow machine

Seal support structure for a circumferential seal of a gas turbine engine

Gas turbine engine flow modulation in a rotating vane

Method of fabricating a turbine engine part

Flow distribution device and method

Apparatus and method for direct writing of single crystal super alloys and metals

Gas turbine engine component for acoustic attenuation

Electrical discharge machining method and electrical discharge machining device