POROUS MACHINED COATINGS

ABRADABLE COATING

COATED COMPONENTS FOR COKE ABATEMENT IN GAS TURBINE ENGINES

ABRADABLE COATING

POROSITY VARIATION OF ABRADABLE BASED ON HARDNESS OF MATERIAL

METAL COUPON WITH POROUS REGION FOR COMPONENT AND COMPONENT WITH SAME

PISTON-RING SEAL LEAKAGE TOLERANT HPC TIE-SHAFT

PROTECTIVE INTERNAL COATINGS FOR POROUS SUBSTRATES

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

Turbomachine cooling trench

Deformable root spacer for a gas turbine engine rotor blade

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

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

Turbomachine cooling trench

Thermal barrier coated component and method for producing thermal barrier coated component

Laminates of polysilazane and carbon fiber reinforced polymer

FULLY STABILIZED ZIRCONIA IN A SEAL SYSTEM

Internal turbomachine casing having improved thermal insulation

Thermal barrier coating with reduced edge crack initiation stress and high insulating factor

THERMAL BARRIER COATING FOR GAS TURBINE ENGINE COMPONENTS

Protective internal coatings for porous substrates

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

THERMAL BARRIER COATING FILM AND TURBINE MEMBER

Segmented environmental barrier coating systems and methods of forming the same

Blade for gas turbine

Outlet guide vanes

Laminates of polysilazane and carbon fiber reinforced polymer

Sealing system for a rotor blade and housing

Multifunctional nanocellular single crystal nickel for turbine applications

ABRADABLE COATING FOR COMPONENTS IN HIGH-TEMPERATURE MECHANICAL SYSTEMS

Wire mesh brush seal windage cover

Abrasive tip blade manufacture methods

Turbomachine cooling trench

Air-oil separator with two flow paths

Air-oil separator with first separator radially outward of matrix separator

Aircraft component and method of manufacture

Gas turbine engine having minimum cooling airflow

Wick structures for heat pipe-based cooling

Thermal barrier coating, turbine member, and gas turbine

Acoustic attenuation on a turbine engine wall

Rotating machine and method for manufacturing casing for rotating machine

THRUST BEARING AS A SEAL

Abradable coatings for high-performance systems

Gas turbine engine fan blade, design, and fabrication

Abradable coating having variable densities

High density bond coat for ceramic or ceramic matrix composites

Abradable coating having variable densities

System for discharging a compressor flow of a turbine engine

Segmented environmental barrier coating systems and methods of forming the same

Protective Internal Coatings for Porous Substrates

Outer airseal abradable rub strip

Liner assembly, engine housing, and methods of assembling the same

Erosion resistant and hydrophobic article

Turbine engine with a rim seal between the rotor and stator

AIRFOIL FOR A TURBINE ENGINE WITH POROUS RIB

Engine component with porous section

Component for a turbine engine with a hole

Engine component with porous trench

Thermally dissipative article and method of forming a thermally dissipative article

HYBRID CERAMIC MATRIX COMPOSITE MATERIALS

Engine component wall with a cooling circuit

COOLED COMPONENT WITH POROUS SKIN

Thermal barrier system with bond coat barrier

Outer airseal abradable rub strip

Outer airseal abradable rub strip

Wire mesh brush seal windage cover

Hybrid blade for turbomachines

Thermal barrier coating with high corrosion resistance

Formation of voids within components formed from porous substrates

Steam turbine, a steam turbine nozzle, and a method of managing moisture in a steam turbine

Ductile compensation layer for brittle components

Compressor variable vane assembly

Cooling holes manufactured with EBC in place

System for thermally isolating a turbine shroud

Gas turbine engine having minimum cooling airflow

Abrasive tip blade manufacture methods

Ceramic attachment configuration and method for manufacturing same

Multifunctional nanocellular single crystal nickel for turbine applications

Method of making an article with internal structure

Turbine engine components with chemical vapor infiltrated isolation layers

Additive process for an abradable blade track used in a gas turbine engine

Corrosion and abrasion resistant coating

Porous media ventless seal

Thrust bearing as a seal

Coatings for high temperature components

Recession resistant ceramic matrix composites and environmental barrier coatings

Protective coating for titanium last stage buckets

Anaerobic hybrid propulsion device with fuel present in the form of divided solids

Formation of voids within components formed from porous substrates

Compressor variable vane assembly

Antivortex device and method of assembling thereof

Ceramic matrix composite component and method of forming thereof

Protective internal coatings for porous substrates

High porosity abradable coating

Gas turbine engine component having foam core and composite skin with cooling slot

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Jet engine with at least one oil separator, through which an air-oil-volume flow can be guided

Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement

Techniques for improved volumetric resistance blower apparatus, system and method

Jet engine with at least one oil separator

Hot gas path component for turbine system

Turbine blade cooling channel formation

Acoustic treatment in an unducted area of a geared turbomachine

Underwater sliding member, method for manufacturing underwater sliding member, and hydraulic machine

System and method for airfoil cover plate

Thermal barrier coating for gas turbine engine components

Ductile compensation layer for brittle components

Deoiler seal

Blade having porous, abradable element

Erosion resistant and hydrophobic article

Protective coating for titanium last stage buckets

HEAT DISSIPATING FAN HAVING A POROUS SINTERED BUSHING FOR AN IMPELLER SHAFT AND METHOD OF MAKING THE BUSHING

PROTECTIVE INTERNAL COATINGS FOR POROUS SUBSTRATES

GAS TURBINE SHROUD WITH CERAMIC ABRADABLE LAYER

Layer system for rotor/stator seal of a turbomachine and method for producing this type of layer system

Nacelle with porous surfaces

Fan Filter Device

Abradable turbine air seal

Method for forming a cast article

Impeller and cooling fan incorporating the same

Fusible gearbox center guide support with frangible catcher pin systems and methods

Abradable composite material and method of making the same