Illuminated and Modular Soft Tissue Retractor

TURBINE COMPONENT WITH A THIN INTERIOR PARTITION

Nickel-based superalloy, single-crystal blade and turbomachine

Method of making a single-crystal turbine blade

Low density nickel-based superalloy having high mechanical strength and environmental robustness at a high temperatures

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

Nickel-based superalloy, single-crystal blade and turbomachine

Turbine component made from superalloy comprising rhenium and associated manufacturing process

Illuminated and modular soft tissue retractor

Turbine component made from superalloy and associated manufacturing method

Method of making a single-crystal turbine blade

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

Highly processable single crystal nickel alloys

GEARED TURBOFAN WITH HIGH GEAR RATIO AND HIGH TEMPERATURE CAPABILITY

Particle separator

Method for forming single crystal components using additive manufacturing and re-melt

Turbine component with a thin interior partition

Multiple piece engine component

Turbine blades and manufacture methods

Illuminated and modular soft tissue retractor

DIRECTIONAL SOLIDIFICATION APPARATUS AND RELATED METHODS

Method for seeding a mold

Arcuate directionally solidified components and manufacture methods

METHODS FOR MANUFACTURING A TURBINE NOZZLE WITH SINGLE CRYSTAL ALLOY NOZZLE SEGMENTS

Method of manufacturing turbine airfoil and tip component thereof

Method of manufacturing turbine airfoil with open tip casting and tip component thereof

Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations

Staged high temperature heat exchanger

RADIAL TURBINE WITH BONDED SINGLE CRYSTAL BLADES

Low rhenium single crystal superalloy for turbine blades and vane applications

Turbine systems with sealing components

Illuminated and modular soft tissue retractor

Dual alloy turbine rotors and methods for manufacturing the same

Blade outer air seal support for a gas turbine engine

Turbine blade attachment curved rib stiffeners

Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof

REPAIR METHOD FOR SEALING SEGMENTS

Hydraulic geofracture energy storage system with desalination

Hybrid bonded turbine rotors and methods for manufacturing the same

Particle separator

Method for forming components using additive manufacturing and re-melt

Method for forming components using additive manufacturing and re-melt

Single crystal grain structure seals and method of forming

Hybrid nozzle segment assemblies for a gas turbine engine

Multiple piece engine component

CMC blade with monolithic ceramic platform and dovetail

Turbine blades and manufacture methods

Corrosion and abrasion resistant coating

Arcuate directionally solidified components and manufacture methods

Methods for manufacturing a turbine nozzle with single crystal alloy nozzle segments

Turbomachine blade arrangement with first and second guides with respective movable first and second elements to reduce vibrational response

Blade cascade for a turbomachine

Method of making a Ni—based single crystal superalloy and turbine blade incorporating same

Article with sections having different microstructures and method therefor

Cast component having corner radius to reduce recrystallization

Multi-airfoil split and rejoin method

Dual alloy turbine rotors and methods for manufacturing the same

Multi-airfoil split and rejoin method to produce enhanced durability coating

Method for forming components using additive manufacturing and re-melt

Ni-based single crystal superalloy and turbine blade incorporating the same

Ni-based single crystal superalloy

Method for repairing a single crystal turbine blade

Blade cascade

Blade cascade

Ni-based casting superalloy and cast article therefrom

Method for utilizing a braze material with carbon structures

Hydraulic geofracture energy storage system with desalinization

Method for manufacturing components made of single crystal (SX) or directionally solidified (DS) nickelbase superalloys

Single crystal welding of directionally compacted materials

REPAIRED SUPERALLOY COMPONENTS AND METHODS FOR REPAIRING SUPERALLOY COMPONENTS

LOW RHENIUM SINGLE CRYSTAL SUPERALLOY FOR TURBINE BLADES AND VANE APPLICATIONS

RHENIUM-FREE SINGLE CRYSTAL SUPERALLOY FOR TURBINE BLADES AND VANE APPLICATIONS

NICKEL-BASE ALLOY

SINGLE CRYSTAL WELDING OF DIRECTIONALLY SOLIDIFIED MATERIALS

Turbine airfoil component and method for making

TURBINE COMPONENT AND METHOD FOR DEVELOPING A COMPONENT

Turbine Component Having Easily Removable Protective Layer, Set of Turbine Components, a Turbine and a Method for Protecting a Turbine Component

Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE

Ni-based single crystal superalloy and turbine blade incorporating the same

Ni-based single crystal superalloy

Multi-component assembly casting

COMPONENT HAVING VARYING STRUCTURES AND METHOD FOR PRODUCTION

Blades, turbine blade assemblies, and methods of forming blades

System and method for reducing grain boundaries in shrouded airfoils

Nickel-based superalloys, turbine blades, and methods of improving or repairing turbine engine components

Methods for joining a monocrystalline part to a polycrystalline part by means of an adapter piece made of polycrystalline material

PROCESS FOR PRODUCING A JOIN TO SINGLE-CRYSTAL OR DIRECTIONALLY SOLIDIFIED MATERIAL

Turbine engine alloys and crystalline orientations

Method of producing or repairing turbine or engine components, and a component, namely a turbine or engine component

Ni-base superalloy, method for producing the same, and turbine blade or turbine vane components

PREHEATING TEMPERATURE DURING REMELTING

Preferential hardening of single crystal blades

Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE INCORPORATING THE SAME

Moderate density, low density, and extremely low density single crystal alloys for high ANapplications

Gas turbine engine airfoil

Single crystal component and a method of heat treating a single crystal component

Metal casting

SINGLE CRYSTAL NICKEL-BASED SUPERALLOY COMPOSITIONS, COMPONENTS, AND MANUFACTURING METHODS THEREFOR

Process for Repairing a Component with a Directional Microstructure

Multi-cast turbine airfoils and method for making same

NI-BASED SINGLE CRYSTAL ALLOY

Turbine components and methods of manufacturing turbine components

Turbomachine blade that is cast with a local fattening of the section of the airfoil

Preheating temperature during welding

SHROUDED SINGLE CRYSTAL DUAL ALLOY TURBINE DISK

Method and mould for casting articles with a pre-determined crystalline orientation

Method of forming a component on a substrate

Moderate density, low density, and extremely low density single crystal alloys for high ANapplications

Turbine blade for a gas turbine engine

Nickel based superalloys with excellent mechanical strength, corrosion resistance and oxidation resistance

Method and mould for casting articles with a pre-determined crystalline orientation

Turbine blade assembly and method of manufacture

Assembly and method for manufacture of component by hot isostatic pressing

Composition of matter

Stable, high-temperature nickel-base superalloy and single-crystal articles utilizing the superalloy

Integrated ceramic/metallic components and methods of making same

Monocrystalline alloys with controlled partitioning

Casting method

Welding method

Repair of nickel-based alloy turbine disk

Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk

Nickel base superalloy and single crystal castings

Illuminated and modular soft tissue retractor