COATING SYSTEM FOR REFRACTORY METALS

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

TURBINE COMPONENT WITH A THIN INTERIOR PARTITION

Method and casting core for forming a landing for welding a baffle inserted in an airfoil

THERMAL BARRIER COATING FOR GAS TURBINE ENGINE COMPONENTS

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

Blade outer air seal fin cooling assembly and method

TURBINE BLADES AND VANES FOR GAS TURBINE ENGINE

Erosion resistant steam valve

NICKEL AND CHROME BASED IRON ALLOY HAVING ENHANCED HIGH TEMPERATURE OXIDATION RESISTANCE

GAS TURBINE ENGINE COMPONENT COOLING CAVITY WITH VORTEX PROMOTING FEATURES

Thermal and environmental barrier coating compositions and methods of deposition

Multi-chamber molten metal pump

Turbine component with a thin interior partition

Compositions for erosion and molten dust resistant environmental barrier coatings

High oxidation-resistant alloy and gas turbine applications using the same

COATING SYSTEM FOR REFRACTORY METALS

LINKAGE OF COMPOSITE CORE FEATURES

Dense environmental barrier coating compositions

Method for manufacturing a component of a rotating machine

Cool core gas turbine engine

ADDITIVELY MANUFACTURED CASTING ARTICLES FOR MANUFACTURING GAS TURBINE ENGINE PARTS

Method for making steel or titanium products containing a precipitation-hardening nickel-base alloy, and part

Method for manufacturing a part coated with a protective coating

Thermal and environmental barrier coating compositions and methods of deposition

Turbomachine component with surface repair

Core assemblies and gas turbine engine components formed therefrom

Method for manufacturing a part coated with a protective coating

REFRACTORY METAL CORE AND COMPONENTS FORMED THEREBY

Turbine engine rotating at high speeds

Compressor vane or blade for engine with exfoliating coating

Turbine apparatus and method for redundant cooling of a turbine apparatus

Abradable compositions and methods for CMC shrouds

Blade outer air seal fin cooling assembly and method

Ceramic and refractory metal core assembly

Method and casting core for forming a landing for welding a baffle inserted in an airfoil

Reflective coating for components

Gas turbine engine component cooling cavity with vortex promoting features

Gas turbine engine blade with ceramic tip and cooling arrangement

Method for producing a component from a composite material comprising a metal matrix and incorporated intermetallic phases

CMC blade with monolithic ceramic platform and dovetail

Engine component having platform with passageway

Steam turbine rotor, steam turbine including same, and thermal power plant using same

Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same

Erosion resistant material and turbine blade

Articles for high temperature service and method for making

GAS TURBINE BLADE AND METHOD OF PROTECTING SAME

Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same

Additively manufactured casting articles for manufacturing gas turbine engine parts

Actively cooled blade outer air seal

Spallation-resistant thermal barrier coating

Turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same

VARIABLE THICKNESS TRAILING EDGE CAVITY AND METHOD OF MAKING

Abrasive preforms and manufacture and use methods

Coating for isolating metallic components from composite components

Gas turbine engine airfoil trailing edge passage and core for making same

Castings, casting cores, and methods

Spallation-resistant thermal barrier coating

Alloy, protective layer and component

Ceramic and refractory metal core assembly

Thermal barrier coating for gas turbine engine components

NICKEL-CHROMIUM-MOLYBDENUM-VANADIUM ALLOY AND TURBINE COMPONENT

Gas turbine engine airfoil with dirt purge feature and core for making same

Turbine shroud assembly and method of forming

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

MAGNETIC ROTOR AND ROTARY PUMP HAVING A MAGNETIC ROTOR

Castings, casting cores, and methods

Extending useful life of a cobalt-based gas turbine component

Gas turbine blade and method of protecting same

Minimizing blockage of holes in turbine engine components

Solid propellant rocket motors employing tungsten alloy burst discs and methods for the manufacture thereof

Component having a film cooling hole

Pulse detonation system

REFRACTORY METAL CORE INTEGRALLY CAST EXIT TRENCH

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

Castings, casting cores, and methods

Method of protecting reactor components from fouling

Airfoil with tapered radial cooling passage

LOW PRESSURE SECTION STEAM TURBINE BUCKET

STEAM TURBINE BUCKET WITH EROSION DURABILITY

Tungsten shell for a spar and shell turbine vane

Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon

Component having a film cooling hole

Cobalt-Free Ni-Base Superalloy

Damping device for a stationary labyrinth seal

RMC-defined tip blowing slots for turbine blades

Microcircuit cooling for vanes

Thin 7YSZ, interfacial layer as cyclic durability (spallation) life enhancement for low conductivity TBCs

Ni-base superalloy having a thermal barrier coating system

Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same

Leading-edge structures for airfoils and systems and methods for fabricating the same

High temperature corrosion resistant composite structure consisting of ruthenium and its alloys

Multiple piece turbine rotor blade