Patent classifications
B23K15/00
Micro-forging by a generative manufacturing process
The present invention relates to a device as well as a method for the additive manufacture of components by deposition of material layers by layer-by-layer joining of powder particles to one another and/or to an already produced pre-product or substrate, via selective interaction of the powder particles with a high-energy beam, wherein, for smoothing a surface of the component being produced running crosswise to the deposited material layers in between the deposition of two layers of the component, the complete edge region of the last layer that is applied and that runs along a surface of the component being produced is compacted in a direction of action that has a directional component parallel to the build-up direction of the layers, and/or at least one edge region of a surface of the component is also compacted.
Electron beam melting and cutting composite 3D printing apparatus
The present application relates to the technical field of 3D printing apparatus, and discloses an electron beam melting and cutting composite 3D printing apparatus which comprises a box and an electron beam gun, in which the box has a cavity formed therein, the cavity is provided therein with a cutting structure, a first Y-direction guide rail and a Y-direction movable platform, the electron beam gun has an emitting head formed in the cavity, the Y-direction movable platform is provided thereon with a Z-direction movable platform, the Z-direction movable platform is provided thereon with a powder spreading structure, the cutting structure has a cutting head, a shielding case is arranged between the emitting head and the Z-direction movable platform, the emitting head of the electron beam gun is inserted in an upper opening of the shielding case, and a lower opening of the shielding case is aligned with the Z-direction movable platform.
OPTICAL MANUFACTURING PROCESS SENSING AND STATUS INDICATION SYSTEM
An optical manufacturing process sensing and status indication system is taught that is able to utilize optical emissions from a manufacturing process to infer the state of the process. In one case, it is able to use these optical emissions to distinguish thermal phenomena on two timescales and to perform feature extraction and classification so that nominal process conditions may be uniquely distinguished from off-nominal process conditions at a given instant in time or over a sequential series of instants in time occurring over the duration of the manufacturing process. In other case, it is able to utilize these optical emissions to derive corresponding spectra and identify features within those spectra so that nominal process conditions may be uniquely distinguished from off-nominal process conditions at a given instant in time or over a sequential series of instants in time occurring over the duration of the manufacturing process.
Additive manufacturing apparatus and method for large components
An additive manufacturing apparatus includes: first and second spaced apart side walls extending along a pre-defined path and defining a build chamber therebetween; one or more build units mounted for movement along the pre-defined path, the one or more build units including at least one of: a powder dispenser positioned above the build chamber; an applicator configured to scrape powder dispensed into the build chamber; and a directed energy source configured to fuse the scraped powder.
Method of fabrication for the repair and augmentation of part functionality of metallic components
Methods and systems for manufacturing a three-dimensional product. Fabrication of a three-dimensional part from a powder spread over a work table as a powder bed can be initiated. The fabrication process can be paused to cool down the work table to room temperature to obtain access to the three-dimensional part for post-processing operations such as, for example, embedding external artifacts. Fabrication can continue by preheating the powder rather than the work table until fabrication of the three-dimensional part is complete. A damaged part may be placed within the powder bed, wherein the fabrication process can be directly initiated to achieve part repair. Additionally, a material of the same part's composition can be used or a different material utilized to render the part better than new. Access to the three-dimensional part allows embedding of a foreign object in the three-dimensional part within the powder bed while the three-dimensional part remains non-finished.
Assembly methods for the connection of a turbine wheel to a shaft
A method of assembling an electrified turbocharger comprising assembling a rotor assembly onto a shaft; balancing the shaft and rotor assembly; attaching at least one bearing onto the shaft adjacent the rotor assembly; inserting a stator assembly into a first housing component; axially inserting the shaft, the rotor assembly, and the at least one bearing into the first housing component; attaching a second housing component to the first housing component; attaching a compressor wheel to a first end of the shaft; and attaching a turbine wheel to a second end of the shaft and balancing the electrified turbocharger.
METHOD FOR OPERATING AT LEAST ONE APPARATUS FOR ADDITIVELY MANUFACTURING THREE-DIMENSIONAL OBJECTS
Method for operating at least one apparatus (1) for additively manufacturing three-dimensional objects (2) by means of successive layerwise selective irradiation and consolidation of layers of a build material (3) which can be consolidated by means of at least one energy beam (4), wherein the energy beam (4) can be guided along at least one defined beam path (9) arranged in a build plane (6) to irradiate build material (3), wherein dependent on at least one parameter relating to a length of the at least one defined beam path (9) and/or relating to a geometry of at least one region (10, 13) of at least one layer to be irradiated, the energy beam (4) is guided along the defined beam path (9) or along a substitute beam path (12).
3-DIMENSIONAL PRINTING PROCESS FOR INTEGRATED MAGNETICS
Integrated circuits (ICs) and method for forming IC devices are presented. In one embodiment, a method of forming a device with an integrated magnetic component using 3-dimensional (3-D) printing is disclosed. The method includes providing a substrate with a base dielectric layer, the base dielectric layer serves as a base for the integrated magnetic component. A first metal layer is formed on the substrate by spray coating metal powder over the substrate and performing selective laser melting on the metal powder. A magnetic core is formed on the substrate by spray coating magnet powder over the substrate and performing selective laser sintering on the magnet powder. A second metal layer is formed on the substrate by spray coating metal powder over the substrate and performing selective laser melting on the metal powder. A patterned dielectric layer separates the first and second metal layers and the magnetic core.
3-dimensional printing process for integrated magnetics
Integrated circuits (ICs) and method for forming IC devices are presented. In one embodiment, a method of forming a device with an integrated magnetic component using 3-dimensional (3-D) printing is disclosed. The method includes providing a substrate with a base dielectric layer, the base dielectric layer serves as a base for the integrated magnetic component. A first metal layer is formed on the substrate by spray coating metal powder over the substrate and performing selective laser melting on the metal powder. A magnetic core is formed on the substrate by spray coating magnet powder over the substrate and performing selective laser sintering on the magnet powder. A second metal layer is formed on the substrate by spray coating metal powder over the substrate and performing selective laser melting on the metal powder. A patterned dielectric layer separates the first and second metal layers and the magnetic core.
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.