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.

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.

A method of manufacturing a gas permeable metal is provided. First a plurality of metal powder particles is spread out tightly to form a first deposited layer and a second deposited layer is formed over the first deposited layer. Then scan the first and the second deposited layers along a plurality of parallel and spaced linear paths. A gap is formed by a difference between a width of melt pool and a linear distance between the two adjacent linear paths. The linear paths of the first and the second deposited layers are arranged with an angle therebetween. The gaps of the first and the second deposited layers are crossed over to form pores distributed like a grid graph. A plurality of the first and the second deposited layers are stacked and the pores are aligned to form continuous pore channels. Thereby the metal with good venting is produced conveniently.

A method of manufacturing a gas permeable metal is provided. First a plurality of metal powder particles is spread out tightly to form a first deposited layer and a second deposited layer is formed over the first deposited layer. Then scan the first and the second deposited layers along a plurality of parallel and spaced linear paths. A gap is formed by a difference between a width of melt pool and a linear distance between the two adjacent linear paths. The linear paths of the first and the second deposited layers are arranged with an angle therebetween. The gaps of the first and the second deposited layers are crossed over to form pores distributed like a grid graph. A plurality of the first and the second deposited layers are stacked and the pores are aligned to form continuous pore channels. Thereby the metal with good venting is produced conveniently.

A three-dimensional printing system includes a motorized build platform, a material coating module, and a beam generation module. The beam generation module includes a laser beam formation unit, a scan module, and flat field focusing system. The laser beam formation unit includes a laser configured to output a laser beam. The scan module is configured to receive the laser beam and to scan the laser beam over a build plane that is above the motorized build platform. The flat field focusing system is configured to focus the laser beam across the laser beam and includes an input component and an output component. The input component is configured to receive the laser beam from the beam formation unit and to pass the laser beam to the scan module. The output component is configured to receive the laser beam from the scan module and pass the laser beam to the build plane.

A three-dimensional printing system includes a motorized build platform, a material coating module, and a beam generation module. The beam generation module includes a laser beam formation unit, a scan module, and flat field focusing system. The laser beam formation unit includes a laser configured to output a laser beam. The scan module is configured to receive the laser beam and to scan the laser beam over a build plane that is above the motorized build platform. The flat field focusing system is configured to focus the laser beam across the laser beam and includes an input component and an output component. The input component is configured to receive the laser beam from the beam formation unit and to pass the laser beam to the scan module. The output component is configured to receive the laser beam from the scan module and pass the laser beam to the build plane.

Aspects of the disclosure are directed to additively manufacturing a three-dimensional structure. As may be implemented in accordance with one or more embodiments, a plurality of stacked layers are deposited, and for one or more respective layers of the plurality of stacked layers, pores are formed within the layer by applying pulsed energy to the layer. The pulsed energy is used to create a space sealed within the layer and having an inner surface defined by material of the layer.

Aspects of the disclosure are directed to additively manufacturing a three-dimensional structure. As may be implemented in accordance with one or more embodiments, a plurality of stacked layers are deposited, and for one or more respective layers of the plurality of stacked layers, pores are formed within the layer by applying pulsed energy to the layer. The pulsed energy is used to create a space sealed within the layer and having an inner surface defined by material of the layer.

Aspects of the disclosure are directed to additively manufacturing a three-dimensional structure. As may be implemented in accordance with one or more embodiments, a plurality of stacked layers are deposited, and for one or more respective layers of the plurality of stacked layers, pores are formed within the layer by applying pulsed energy to the layer. The pulsed energy is used to create a space sealed within the layer and having an inner surface defined by material of the layer.

A method for manufacturing an additively manufactured article, the method comprising subjecting a powder material comprising a first powder containing a precipitation hardening stainless steel and a second powder containing titanium carbide to weaving irradiation with a laser beam to melt and solidify the powder material, thereby laminating at least one hardened clad layer on a base material. In the step for laminating the clad layer, the following requirements are satisfied: 20≤A≤35, 1.1≤B≤1.3, and (40% by mass)≤R2≤(65% by mass). In the formulae, A represents a laser heat input index, B represents a powder feeding rate index, and R2 represents a content ratio of the second powder in the powder material.