Patent classifications
B22F10/25
METHODS OF MANUFACTURING PERMANENT MAGNETS BY ADDITIVE MANUFACTURING
The present disclosure is directed towards a method of manufacturing a permanent magnet such that the magnet defines a channel for allowing circulation of a coolant through the permanent magnet, or defines a channel for allowing circulation of the coolant through an interface between the permanent magnet and a substrate. Magnets made by this method may be useful for manufacturing and/or operating a machine, such as a motor, engine, or sensor.
Additive manufacturing controlled failure structure and method of making same
A downhole component including a first portion; a second portion; a controlled failure structure between the first portion and second portion. A method for improving efficiency in downhole components.
Additively manufactured component and production method therefor
A component includes a multiplicity of individual powder particles of Mo, a Mo-based alloy, W or a W-based alloy that have been fused together to give a solid structure by a high-energy beam via an additive manufacturing method. The component has an oxygen content of not more than 0.1 at %. An additive manufacturing method includes producing the powder via the melt phase and providing a carbon content in the region of not less than 0.15 at %. The components are crack-free and have high grain boundary strength.
Additively manufactured component and production method therefor
A component includes a multiplicity of individual powder particles of Mo, a Mo-based alloy, W or a W-based alloy that have been fused together to give a solid structure by a high-energy beam via an additive manufacturing method. The component has an oxygen content of not more than 0.1 at %. An additive manufacturing method includes producing the powder via the melt phase and providing a carbon content in the region of not less than 0.15 at %. The components are crack-free and have high grain boundary strength.
Method of molding anisotropic composite material and die using anisotropic composite material
Provided is a method of molding a composite material by laser metal deposition in which a powder metal material is irradiated with a laser beam while supplying the powder metal material onto a surface of a base material, in which the powder metal material is a mixed powder of an Fe alloy powder and a Cu powder, and a mixing ratio of the Fe alloy powder and the Cu powder is 15% or more and 30% or less by weight % of the Cu powder, and in which the composite material having anisotropy is molded by setting energy of the laser beam to be 9 KJ/g or more and 10 KJ/g or less in a mixed powder ratio.
Method of molding anisotropic composite material and die using anisotropic composite material
Provided is a method of molding a composite material by laser metal deposition in which a powder metal material is irradiated with a laser beam while supplying the powder metal material onto a surface of a base material, in which the powder metal material is a mixed powder of an Fe alloy powder and a Cu powder, and a mixing ratio of the Fe alloy powder and the Cu powder is 15% or more and 30% or less by weight % of the Cu powder, and in which the composite material having anisotropy is molded by setting energy of the laser beam to be 9 KJ/g or more and 10 KJ/g or less in a mixed powder ratio.
3D printed chamber components configured for lower film stress and lower operating temperature
A chamber component for a processing chamber is disclosed herein. In one embodiment, a chamber component for a processing chamber includes a component part body having unitary monolithic construction. The component part body has a textured surface. The textured surface includes a plurality of independent engineered macro features integrally formed with the component part body. The engineered macro features include a macro feature body extending from the textured surface.
3D printed chamber components configured for lower film stress and lower operating temperature
A chamber component for a processing chamber is disclosed herein. In one embodiment, a chamber component for a processing chamber includes a component part body having unitary monolithic construction. The component part body has a textured surface. The textured surface includes a plurality of independent engineered macro features integrally formed with the component part body. The engineered macro features include a macro feature body extending from the textured surface.
System and method for hybrid additive and subtractive manufacturing with dimensional verification
A system, is disclosed having a polymer-based additive manufacturing subsystem, a metallic-based additive manufacturing subsystem, an exchanger to place at least one of the polymer-based additive manufacturing subsystem and the metallic-based additive manufacturing subsystem into a position to provide a manufacturing process, a build area where a part is created with the polymer-based additive manufacturing subsystem and the metallic-based additive manufacturing subsystem, and an environmental control unit to collect debris produced during operation of the polymer-based additive manufacturing subsystem and the metallic-based additive manufacturing subsystem. Another system and method are also disclosed.
METHOD FOR DETERMINING ADDITIVE MANUFACTURING PARAMETERS
A method for determining additive manufacturing parameters for the manufacture of an additive manufacturing support (1) for a target part exhibiting an overhang comprises the steps of: (a) additive manufacture of a plurality of supports for each supporting an overhang (2) of a test part (3), each support (1) being associated with a collection of manufacturing parameters and a collection of geometric parameters pertaining to the overhang (2); (b) manufacturing the test part (3) and observing, for each support (1), a collection of mechanical parameters pertaining to the support (1); (c) determining the additive manufacturing parameters for the manufacture of the support (1) of the target part on the basis of the geometric parameters pertaining to the overhang of the target part and of the mechanical parameters pertaining to the support.