A computer-implemented method of generating scan instructions for forming a product using additive layer manufacture as a series of layers is provided. The method comprises determining a beam acceleration voltage to be used when forming the product; for each hatch area of layers of the product, determining a respective beam current to be used when forming the hatch area and providing a respective beam current value to the hatch area description in the scan pattern instruction file; and for each line of each hatch area, determining a respective beam spot size to be used when scanning the beam along the line and providing a respective beam spot size value to the line description in the scan pattern instruction file, and determining a respective series of beam step sizes and beam step dwell times to be used when scanning the beam along the line, and providing a respective series of beam position values and beam step dwell times to the line description in the scan pattern instruction file thereby defining how the beam is to be scanned along the line. Also provided are a file of scan instructions, an additive layer manufacture apparatus, and a method of forming a product using the additive layer manufacturing apparatus.

In various embodiments, metallic wires are fabricated by combining one or more powders of substantially spherical metal particles with one or more powders of non-spherical particles within one or more optional metallic tubes. The metal elements within the powders (and the one or more tubes, if present) collectively define a high entropy alloy of five or more metallic elements or a multi-principal element alloy of four or more metallic elements.

A powder feeding device includes: a hopper including a discharge port for discharging powder; and a conveyance device configured to move a conveyance surface disposed below the discharge port in a first direction and invert the conveyance surface in a front end portion. The hopper includes a front wall portion positioned on a downstream side of the discharge port in the first direction. A predetermined gap is formed between a lower end of the front wall portion and the conveyance surface. In the powder feeding device, powder deposited on the conveyance surface is conveyed in the first direction by the conveyance device with a thickness corresponding to the gap and dropped from the front end portion.

This disclosure describes machining units for machining a workpiece, in particular for welding a workpiece by, using a thermal machining beam. The thermal machining beam can be directed onto a workpiece along a beam incidence axis by means of the machining unit, wherein the machining unit has a rotary drive device by means of which an auxiliary module for workpiece machining is rotatable about the beam incidence axis. The machining unit includes a coupling device by which the auxiliary module can be moved between a position coupled to the rotary drive device and a position uncoupled from the rotary drive device.

A component includes an additively manufactured component with an internal passage and an additively manufactured elongated member within the internal passage. A method of additively manufacturing a component including additively manufacturing a component with an internal passage; and additively manufacturing an elongated member within the internal passage concurrent with additively manufacturing the component.

Devices, systems, methods, and kits of parts for monitoring operation of an electron beam additive manufacturing systems are disclosed. A monitoring system includes one or more measuring devices positioned on the at least one wall in the interior of a build chamber of the additive manufacturing system. Each one of the one or more measuring devices includes a piezoelectric crystal. The monitoring system further includes an analysis component communicatively coupled to the one or more measuring devices. The analysis component is programmed to receive information pertaining to a frequency of oscillation of the piezoelectric crystal. A collection of material on the one or more measuring devices during formation of an article within the build chamber causes a change to the frequency of oscillation of the piezoelectric crystal that is detectable by the analysis component and usable to determine a potential build anomaly of the article.

A repair method for self-detecting and self-healing of corrosion defects in metals can achieve self-detecting and self-healing repair of an initial corrosion defect and be used to repair a micron-level corrosion defect. Furthermore, the self-detecting and self-healing repair method can be used to effectively repair an initial corrosion defect in a large-sized high-precision structural component, thus effectively improving the service safety of the high-precision metal structural component and prolonging the service life of the same.

The dual focused ion beam and scanning electron beam system includes an electron source that generates an electron beam and an ion source that generates an ion beam. The electron beam column directs an electron beam at a normal angle relative to a top surface of the stage. An ion beam column directs the ion beam at the stage. The ion beam is at an angle relative to the electron beam. A detector receives the electron beam reflected from the wafer on the stage.

Systems, apparatus, and methods for weld tapering at a trailing edge using time multiplexing are disclosed. Systems, apparatus, and methods for control of an electron beam for welding using time multiplexing are disclosed. An example apparatus includes memory and at least one processor to execute instructions to at least: in a first portion of a line of an object being formed, control an energy beam at a first position at a first time to form a weld from a powder; and in a second portion of a line of the object being formed, control the energy beam to perform a dispersion sweep at a second position at a second time.

A method of forming a passage in a turbine component includes: using an additive manufacturing process to form a first support structure on a first surface of the turbine component; forming a second support structure on a second surface of the turbine component, the second support structure being spaced apart from the first support structure; and forming a passage in the turbine component between the first and second support structures.