A method of producing an amorphous alloy ribbon. The method includes radiating a laser to an amorphous alloy ribbon, while the amorphous alloy ribbon travels or is travelling, to thereby form laser irradiation marks on the amorphous alloy ribbon. Further, when the amorphous alloy ribbon has a traveling speed of S1 m/sec and the laser has a scanning speed of S2 m/sec, the S1 is 0.1 m/sec or more and 30 m/sec or less, the S2 is 1 m/sec or more and 800 m/sec or less, and S2/S1 is 3.0 or more.

A multi-material component joined by a high entropy alloy is provided, as well as methods of making a multi-material component by joining materials with high entropy alloys to reduce or eliminate liquid metal embrittlement (LME) cracks.

An electrical connector includes a first layer formed of a copper based material and a second layer formed of an iron-nickel alloy. The second layer has a thickness of 8% to 30% of the thickness of the electrical connector. The electrical connector also includes a third layer which is formed of a solder alloy that consists essentially of 17% to 28% indium by weight, 12% to 20% zinc by weight, 1% to 6% silver by weight, 1% to 3% copper by weight, and a remaining weight of the solder alloy that is tin.

A mask assembly includes: a mask frame provided with a first opening defined through a center portion thereof and including an outer frame surrounding the first opening and provided with at least one concave portion defined therein; a mask body disposed to correspond to the first opening and provided with second openings defined therethrough and having an area smaller than the first opening; a first sub-mask disposed on the mask body, provided with third openings defined therethrough over an entire area thereof and having an area smaller than each of the second openings, and including a metal material; a second sub-mask disposed on the first sub-mask, provided with fourth openings defined therethrough over an entire area thereof and having an area smaller than each of the third openings in a plane, and including a polymer material; and a welding portion disposed on the second sub-mask in the concave portion.

A method to produce a wear and corrosion resistant coating system onto a surface of a substrate, preferably a brake disc, comprising the following steps: (1) providing the substrate having the surface made of an iron-based material or a steel material, (2) selecting a dedicated material for producing one or more coating layers of the coating system, (3) producing onto the substrate surface one or more coating layers of the coating system by using a laser cladding process, wherein the dedicated material selected in step (2) is used as source material for the production of the coating layers, and positioning a laser beam with respect to the substrate surface in such a manner that a coating angle is formed between the laser beam and the substrate surface, and maintaining this coating angle during the production of the one or more coating layers at a value between 10° and 30°.

The disclosure belongs to the technical field of surface coating, and particularly relates to a flux-cored welding wire, a preparation method and use thereof, a porous coating and a preparation method thereof. The disclosure provides a flux-cored welding wire, including a core wire and a sheath, where the core wire includes the following components by mass percentage: 15.0-30.0% of Cr, 1.5-2.5% of Si, 5.0-10.0% of Ni, 1.0-5.0% of TiH.sub.2, and Fe as balance; and the sheath is made of steel. Test results of examples show that, the porous coating obtained by supersonic arc spraying the flux-cored welding wire provided by the disclosure has a porosity of up to 46% and a coating adhesive strength of 45 MPa, which are desired.

A method has acts of providing a blank of head, providing a reinforcement element, combining the blank of head and the reinforcement element, and co-forging. The blank of head is made of a material having a hardness ranging from HRB50 to HRB105 measured by Rockwell Hardness Test and being softer than HRB105 and has a recess. The reinforcement element is made of a material having a hardness ranging from HRC15 to HRC55 measured by Rockwell Hardness Test. The reinforcement element is put into the recess in the blank of head, and an inner surface of the recess and the reinforcement element are combined securely with each other completely by a welding process. The blank of head combined with the reinforcement element is put into a mold, is heated to 700° C. to 1100° C., and is applied with a co-forging process to form an eutectic bonding by thermocompression.

A laser beam shaping device includes a multi-zone structure lens and a focusing lens. The multi-zone structure lens includes a lens body and a refractive structure. The lens body has an incident plane and an emission plane, and one of the incident plane and the emission plane is furnished with the refractive structure. The light source passing through the refractive structure deviates and leaves the lens body via the emission plane. The light source passing through the lens body is divided into N sets of light beams. After the N sets of light beams penetrate through the focusing lens, N set of incident beams are formed to project the interface of the first material and the second material in an oblique inward manner with respect to the optical axis of the focusing lens. In additional, a laser processing system and a laser interlocking welding structure respectively are also provided.

A rotary electric machine member manufacturing method includes: a step of providing a motor core by stacking a plurality of electromagnetic steel sheets; and a step of welding the motor core by keyhole welding while pressurizing the motor core in a stacking direction with a welding pressure lower than that at which the thickness of the motor core in the stacking direction levels off. The thickness is a length of the motor core between a first end of the motor core and a second end of the motor core.

Provided are a laser processing method and a laser processing device which prevent a laser irradiation unit from colliding with an edge of a plate material when the laser irradiation unit returns to a portion just above the plate material from an outer part of the portion just above the plate material. The laser processing method for cutting a plate material by laser irradiation, the method including: a plate material end portion holding process of holding a position of an end portion of the plate material at a predetermined position when a laser irradiation unit is present outside a portion just above the plate material; and a laser irradiation unit moving process in which the laser irradiation unit moves from an outer part of the portion just above the plate material to the portion just above the plate material.