Additively Manufactured Turbine Engine Case with Fuel Manifold

MACHINABLE COATING FOR DAMPING

COMPONENTS WITH THERMAL BARRIER COATINGS HAVING SOLID FILMS THEREON AND METHODS OF COATING THE SAME

INTEGRATED AIR CYCLE MACHINE FOR AN ENVIRONMENTAL CONTROL SYSTEM OF AN AIRCRAFT

CMC COMPONENT WITH COOLING CAVITY

PROTECTIVE TREATMENT AND METHOD OF APPLYING THE SAME

GAS TURBINE ENGINE

COST-EFFECTIVE SOLID-STATE DEPOSITION OF FUNCTIONALLY GRADED TITANIUM HOLLOW FAN BLADE SHEATH FOR IMPROVED GALVANIC CORROSION RESISTANCE

BLADE ARRANGEMENT OF A THERMAL TURBOMACHINE THROUGH WHICH AXIAL FLOW MAY PASS, AND THERMAL TURBOMACHINE THROUGH WHICH AXIAL FLOW MAY PASS

LEADING EDGE PLATING ON LOW PRESSURE COMPRESSOR VANE FOR WEIGHT AND STRENGTH OPTIMIZATION

FLUID FLOW DISTRIBUTOR FOR VAPOR PHASE COATING OF TURBINE COMPONENTS

METHOD AND SYSTEM OF FORMING A COMPOSITE AIRFOIL HAVING A SET OF PLIES

Micro Gas Turbine Engine and Related Methods of Manufacture

ENGINE COMPONENT WITH ABRADABLE MATERIAL AND TREATMENT

SEAL ASSEMBLY FOR A ROTARY MACHINE

ADDITIVELY MANUFACTURED COMBUSTOR WITH AIR RE-USE FROM AFT FRAME TO AXIAL FUEL STAGE INJECTOR(S)

SUPPORT STRUCTURE FOR FORMING TURBINE ENGINE ROTATING STRUCTURE

FAN BLADE LEADING EDGE SHEATH

DESIGN OF A REAR-CONE EXHAUST DUCT FOR ADDITIVE MANUFACTURING

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

ADDITIVELY MANUFACTURED ARTICLES HAVING A MICROSTRUCTURE WITH A HIGH GAMMA-PRIME VOLUME FRACTION

THERMALLY STABLE THIN-FILM REFLECTIVE COATING AND COATING PROCESS

MULTI-MATERIAL FLOWPATH WALL FOR TURBINE ENGINE

AIR INTAKE LIP FOR A NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

METHOD OF MANUFACTURING A COMPONENT OF A GAS TURBINE ENGINE

FIRE RETARDANT ENGINE CASING APPARATUS

LEADING-EDGE STRUCTURES FOR AIRFOILS AND SYSTEMS AND METHODS FOR FABRICATING THE SAME

Support structure for forming turbine engine rotating structure

COATING SYSTEM AND SUBSTRATE WITH COATING SYSTEM

CMC materials with integrated thermocouple

Method for manufacturing turbine labyrinth seal using wire arc additive manufacturing

MONOLITHIC SHAFT FOR CRYOGENIC TURBO MACHINE, CRYOGENIC TURBO MACHINE AND METHOD FOR MANUFACTURING

TURBINE ENGINE ELEMENT COMPRISING AT LEAST ONE BLADE OBTAINED BY ADDITIVE MANUFACTURING

SINGLE-PIECE ANNULAR VANE ARRAY FOR A GAS TURBINE ENGINE

COOLING-AIR INJECTION CASING FOR A TURBOMACHINE TURBINE

FLOW BODY FOR A GAS TURBINE, GAS TURBINE, METHOD FOR MANUFACTURING A FLOW BODY FOR A GAS TURBINE, AND METHOD FOR REPAIRING A FLOW BODY OF A GAS TURBINE

ADDITIVELY MANUFACTURED SELF-SUPPORTING ASYMMETRIC VALVE CORES

Transpiration-cooled systems having permeable and non-permeable portions

Transpiration-cooled systems having permeable and non-permeable portions

PROTECTIVE TREATMENT AND METHOD OF APPLYING THE SAME

WHEELS HAVING A BI-LAYERED COATING INCLUDING A HARD COATING LAYER AND METHODS FOR MAKING THE SAME

Axial expandable exhaust duct

TURBOMACHINE WITH UNITARY HOUSING MEMBER HAVING CHAMBER WITH PLURALITY OF INTERNAL BRACES

MACHINABLE COATING FOR DAMPING

Cooling jacket of a hollow blade of a distributor

SPLITTER FOR AERONAUTIC TURBOMACHINE

ADDITIVE MANUFACTURING PROCESS FOR PRODUCING A STRUCTURE

Metal plated additively manufactured plastic rotor shrouds and their method of manufacturing

FORMING DUCT STRUCTURE WITH OVERBRAIDED WOVEN FIBER SLEEVE

COMPOSITE AIRFOIL ASSEMBLIES AND METHOD FOR MANUFACTURING THE SAME

Surface topology manipulation for performance enhancement of additively manufactured fluid-interacting components

Turbomachine cooling trench

Method of manufacturing CMC component

METHOD FOR MANUFACTURING GAS TURBINE ROTOR HEAT SHIELDING SEGMENT BY THREE-DIMENSIONAL PRINTING

Machinable coating for CMC and metal interface in a turbine section

METHODS FOR CREATING A NICKEL STRIKE LAYER AND NICKEL ELECTROLYTIC BONDCOAT ONTO A NON-CONDUCTIVE CARBON FIBER COMPOSITE SURFACE AND THE COATING SYSTEM DERIVED THEREFROM

SUPPORT STRUCTURE AND SPRING FOR BEARING COMPARTMENT

Manufacture of an impeller in a hybrid process

FLUID PUMPS

PRE-CERAMIC THERMAL BARRIER FOR GAS TURBINE ENGINE COMPONENTS

Coated article for hot hydrocarbon fluid and method of preventing fuel thermal degradation deposits

CERAMIC MATRIX COMPOSITE ARTICLE AND METHOD OF MAKING THE SAME

HIGH-PRESSURE TURBINE VANE INCLUDING A CAVITY UNDER A SQUEALER TIP

COLD SPRAY DUCT FOR A GAS TURBINE ENGINE

Oxidation and SRZ Resistant Coatings on Nickel Superalloys

POLYMERIC FOAMS FOR HOLLOW CAVITIES

ADDITIVELY MANUFACTURED TURBOMACHINERY COMPONENTS WITH DESIGNED ATMOSPHERE OF AN INNER VOIDED CORE FOR HEAT TRANSFER CONTROL

Face sheet of acoustic liner having streamlined holes with elongated edges

Engine airfoil metal edge

Sublayer for a nickel-based superalloy for enhancing the lifetime of the parts and implementation method thereof

Thermally stable thin-film reflective coating and coating process

GAS TURBINE ENGINE ROTATION UNIT CONSTITUENT MEMBER AND METHOD FOR PRODUCING SAME

CMC trailing edge 3D weaved cross brace

System and Method for Manufacture of Abrasive Coating

Surface topology manipulation for performance enchancement of additively manufactured fluid-interacting components

Seals for managing thermal distortion in a turbomachine and methods for building the same

Housing for flow-conducting components

Perforated impeller blades

Illuminated and Modular Soft Tissue Retractor

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

Bladed turbine stator for a turbine engine

Engine component with abradable material and treatment

Method for providing a gas turbine blade and rotor wear-protection system

Reinforcement of a deposited structure forming a metal matrix composite

Adjustment lever for a turbomachine

ADDITIVELY MANUFACTURED GAS TURBINE ENGINE AND VENTILATOR

Heat exchanger assembly with unitary body and manifold and methods of formng same

Methods involving and apparatuses for a turbine engine fairing

Fire retardant engine casing apparatus

Seal assembly for a rotary machine

PROCESS AND MATERIAL CONFIGURATION FOR MAKING HOT CORROSION RESISTANT HPC ABRASIVE BLADE TIPS

Perforated impeller blades

Airfoil with sintered powder components

Woven fibrous preform for producing a part from composite material, in particular a turbomachine blade

Axial expandable exhaust duct

Attritable engine additively manufactured inlet cap

Aircraft turbomachine casing and method of manufacturing same

Methods and multi-purpose powder removal features for additive manufacturing

Abradable insert with lattice structure

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

Methods for vehicle propulsion

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

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

Frangible airfoil with shape memory alloy

HEAT TRANSFER DEVICE, TURBOMACHINE CASING AND RELATED STORAGE MEDIUM

Blade made of composite material with variable-density attached leading edge

Radial turbine rotor with complex cooling channels and method of making same

Fluid pumps

Fluid pumps

Part having improved abrasion resistance

Hybrid platform manufacturing

Anti-vortex tube retaining ring and bore basket

Method for the layer-by-layer additive manufacturing of a composite material

Method for coating a component

Bearing chamber housing for a turbomachine

METHOD FOR REPAIRING AN AIR INTAKE LIP

Combined additive and subtractive manufacturing of bladed rotors

Cold spray duct for a gas turbine engine

Turbomachine cooling trench

Method for manufacturing or for repairing a component of a rotary machine as well as a component manufactured or repaired using such a method

Method for the repair welding of an aircraft turbine engine blade

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

TURBINE ENGINE FUEL INJECTOR WITH NON-CIRCULAR NOZZLE PASSAGE

Additive manufactured ducted heat exchanger system

Compound angle accelerator

Engine airfoil metal edge

Vane arc segment with flange having step

Surface cooler assembly

Component formed from hybrid material

Combustor for gas turbine engine and method of manufacture

Turbomachine output bearing support

Method for coating a turbomachine guide vane, associated guide vane

Coated article for hot hydrocarbon fluid and method of preventing fuel thermal degradation deposits

Turbine casing component and repair method therefor

Coolant delivery via an independent cooling circuit

Method for manufacturing or for repairing a component of a rotary machine as well as a component manufactured or repaired using such a method

MODULE OF AN AIRCRAFT TURBINE ENGINE

Sealing ring for a wheel of a turbomachine turbine

Method for applying a coating to a surface of a mullite material, mullite material having a coating, and gas turbine component

Separation nozzle for aeronautic turbomachine

Coolant delivery via an independent cooling circuit

Combustor for a gas turbine engine

Method for detecting a roughness in an abradable layer in a fan casing

Turbine blade platform cooling holes

Turbine guide vane

Gas turbine blade and rotor wear-protection system

Method for producing steam turbine member

Two-layer abrasive coating for rotor-blade tips, method, component, and turbine assembly

COLD SPRAY REINFORCED IMPELLER SHROUD

METHOD FOR MANUFACTURING A COMPRESSOR IMPELLER FOR A TURBOMACHINE

Hollow blade containing an internal lattice

Spall plate for consumable combustor support structures

Turbine nozzle and method of manufacture

Turbomachine stator sector having flexible regions subjected to high stress

Anti-vortex tube retaining ring and bore basket

ALUMINUM OXIDE PROTECTIVE COATINGS ON TURBOCHARGER COMPONENTS AND OTHER ROTARY EQUIPMENT COMPONENTS

Additively manufactured booster splitter with integral heating passageways

Turbine part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method

Impeller design and manufacturing method with pentagonal channel geometry

Aerodynamic arm for an aircraft turbine engine casing

High-temperature component, production method for high-temperature component, and flow rate control method

Impact-cooling tubular insert for a turbomachine distributor

Repair of organic matrix composite parts

Internal turbomachine casing having improved thermal insulation

Gas turbine engine including seal assembly with abradable coating including magnetic particles

Method of manufacturing folded structure with additive features

COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE

Fan track liner

Methods and materials for repairing a thermal barrier coating of a gas turbine component

Monolithic diffuser and deswirl flow structure for gas turbine engine

CMAS resistant thermal barrier coating system

DEVICE FOR DE-ICING A TURBOMACHINE NOZZLE

Low friction, wear resistant variable vane bushing

Composite aerofoils

Conforming coating mask for a component and system background

Process and material configuration for making hot corrosion resistant HPC abrasive blade tips

Reflective coating and coating process therefor

Acoustic cores with sound-attenuating protuberances

Turbomachine housing having at least one cover, turbomachine, method for producing a cover

Manufacture of a fan track liner

Cooled airfoil and method of making

Gas turbine combustor and method of manufacturing burner component

Gas Turbine Combustor and Fuel Nozzle Manufacturing Method

Rotatable forged disc for a bladed rotor wheel and a method for manufacturing thereof

Long-fibre-reinforced-joints-composite thrust reverser cascade

Abrasive tip coating

Post deposition heat treatment procedures for EBC and abradable coating on ceramic or CMC substrate

Frame for a heat engine

Protection of components from corrosion

Double row compressor stators

Impingement cooled rotating seal

Protection of components from corrosion

Protection of components from corrosion

FUNCTIONALLY GRADED SANDPHOBIC BLENDED COMPOSITE COATINGS

Containment system for gas turbine engine

Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture

Leachable casting core and method of manufacture

TURBINE IMPELLER

Hybrid manufacturing of a support housing

Turbine component made from superalloy comprising rhenium and associated manufacturing process

Axial expandable exhaust duct

Element for distributing a cooling fluid and associated turbine ring assembly

Valve assembly for an active clearance control system

Ceramic matrix composite component and method of producing a ceramic matrix composite component

Surface topology manipulation for performance enhancement of additively manufactured fluid-interacting components

SINTERED-BONDED HIGH TEMPERATURE COATINGS FOR CERAMIC TURBOMACHINE COMPONENTS

Turbomachine blade comprising an internal fluid flow passage equipped with a plurality of optimally arranged disruptive elements

Contour weaving to form airfoil

Component wall of a hot gas component

Method for creating an aircraft turbomachine vane using additive manufacturing

Fused filament fabrication of abradable coatings

Reinforcement of a deposited structure forming a metal matrix composite

Method of selectively bonding braze powders to a surface

Bracket

Part coated with a composition for protection against CMAS with controlled cracking, and corresponding treatment method

Restoration coating system and method

Hybrid-additive gear for a wind turbine gearbox

Turbine rotor blade, turbocharger, and method for producing turbine rotor blade

Turbine vane assembly incorporating ceramic matrix composite materials and cooling

Coolant delivery via an independent cooling circuit

Illuminated and modular soft tissue retractor

Method, device and powder for the additive manufacturing of a component with oxide dispersion strengthening and corresponding component

Spall plate for consumable combustor support structures

Support structure for combustor components and method of using same

Unitized rotor assembly

INJECTOR DEVICE AND METHOD FOR MANUFACTURING AN INJECTOR DEVICE

WEAR RESISTANT COATING, METHOD OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME

Method of manufacturing a component of a rotary machine and component manufactured using said method

Bearing support for an aircraft engine manufactured by additive manufacturing

Method for manufacturing a propeller blade and a propeller blade

System for a combined turbine and bearing case for a turbocharger

Method for the hybrid construction of multi-piece parts

Method and apparatus for optimisation of the supports for the additive manufacturing of a component with a recess

3D-printed composite compressor blade having stress-oriented fiber and method of manufacturing the same

Reflective coating and coating process therefor

Attritable engine additively manufactured inlet cap

Flow path assemblies for gas turbine engines and assembly methods therefore

Near wall leading edge cooling channel for airfoil

Sintered-bonded high temperature coatings for ceramic turbomachine components

Method for manufacturing or for repairing a component of a rotary machine as well as a component manufactured or repaired using such a method

Method for manufacturing or for repairing a component of a rotary machine as well as a component manufactured or repaired using such a method

Manufacturing thin-walled castings utilizing adaptive machining

Monolithic body including an internal passage with a generally teardrop shaped cross-sectional geometry

Turbine components and methods of manufacturing

Turbomachine inner housing

Copper combustion chamber attached to injector by non-copper weld transition ring

PROTECTION AND ENHANCEMENT OF THERMAL BARRIER COATING INTEGRITY BY LITHOGRAPHY

Gas impingement in-process cooling system

TURBINE CONTAINMENT ARRANGEMENT

Method for producing a thermal barrier on a part of a turbomachine

Layered manufacturing of single crystal alloy components

CMC BOAS with internal support structure

Turbine blade comprising a cooling structure and associated production method

NICKEL-CHROMIUM-ALUMINUM COMPOSITE BY ELECTRODEPOSITION

Ceramic seal component for gas turbine engine and process of making the same

Internally damped airfoiled component

Abradable turbomachine element provided with visual wear indicators

Non-continuous abradable coatings

Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature

Gas engine component with cooling passages in wall and method of making the same

Fusible bond for gas turbine engine coating system

Turbine part made of superalloy comprising rhenium and/or ruthenium and associated manufacturing method

Multi-wall deposited thin sheet structure

Additive manufactured ducted heat exchanger system

Coated components having adaptive cooling openings and methods of making the same

Three-dimensional additive manufactured product and three-dimensional additive manufacturing method

Diode laser fiber array for powder bed fabrication or repair

CMC LAYERING WITH PLIES WITH INNER PORTION DEFINED WITH OPENING(S), AND NOZZLE ENDWALL

Gas turbine combustor liner with integral chute made by additive manufacturing process

Surface cooler and method of forming

Method of forming an additively manufactured component

Turbine component and methods of making and cooling a turbine component

Control of solidification in laser powder bed fusion additive manufacturing using a diode laser fiber array

THERMAL MANAGEMENT SYSTEM FOR LOW BYPASS GAS TURBINE ENGINE

Turbine blade tip cooling system including tip rail cooling insert

Method of forming a cure tool and method of forming a textured surface using a cure tool

Heat exchanger and method for manufacturing same

Containment system for gas turbine engine

Leachable casting core and method of manufacture

Bellcrank for a turbomachine

Laser powder deposition weld rework for gas turbine engine non-fusion weldable nickel castings

Cowl integration to combustor wall

Turbine airfoil with multiple walls and internal thermal barrier coating

Gas turbine engine dual-wall hot section structure

Additively deposited gas turbine engine cooling component

Ceramic matrix composite turbine nozzle shell and method of assembly

NACELLE INLET AND SYSTEM AND METHOD FOR MAKING SAME

COMBUSTION CHAMBER, A COMBUSTION CHAMBER TILE AND A METHOD OF MANUFACTURING A COMBUSTION CHAMBER TILE

Sealing system for a rotor blade and housing

Additive manufacturing method for making holes bounded by thin walls in turbine components

Frangible gas turbine engine airfoil including an internal cavity

Frangible gas turbine engine airfoil with layup change

Additively manufactured thermally insulating structure

Method of resonant inspection for additive manufacturing

Double row compressor stators

GAS TURBINE ENGINE

Multi-material rotor for attritable engines

Ribbed pin fins

Deposited material structure with integrated component