A method for shaping a ceramic matrix composite (CMC) sheet having a first surface and a second surface is presented. The method includes receiving an input signal representative of a predetermined shape and a type of the CMC sheet. Further, the method includes selecting a laser beam based on the received input signal. Also, the method includes projecting the selected laser beam on the CMC sheet to shape the CMC sheet into the predetermined shape.

A method for solid state joining of dissimilar materials using a friction stir welding device wherein a pin is inserted through an aperture defined in a first material and a second material to hold the materials together and then held in place by friction stir welding a portion of the pin to a material adjacent said pin, or by friction stir welding a cap or plug that holds the pin in place to the adjacent material. The result is a connection or join wherein the central portion of the pin is not friction stir welded but the portions holding the pin in place (the ends or caps) generally are.

A gas flow can be provided together with a liquid jet guided laser beam to remove accumulated liquid on the processing surface. The gas flow can be configured to have minimum interference with the liquid jet guided laser beam, while functions to blow away liquid generated by the liquid jet. Keeping the surface free from accumulated liquid can improve the efficiency of the liquid jet guided laser processing.

A manufacturing process is provided that includes steps of: providing a panel comprising a core connected to a first skin, wherein. the panel is configured with a plurality of cavities extending through the core to the first skin; partially forming a first perforation in the first skin using a laser beam; operating a sensor to sense optical emissions produced during the partial forming of the first perforation; and determining, based on an output of the sensor, whether to: continue formation of the first perforation in the first skin; or terminate formation of the first perforation in the first skin.

The present invention discloses a cutting assembly. The cutting assembly includes a substrate, a cutting edge, and a welding portion. The substrate includes a first metal portion, and the first metal portion has a first side surface. The cutting edge is formed by overlapping a second metal portion with a third metal portion used for an edge, the second metal portion is of high-strength alloy steel and has a second side surface, and the third metal portion is of high-speed tool steel and has a third side surface. The welding portion connects the first metal portion and the second metal portion. The present invention further provides a method for manufacturing a cutting assembly, including: welding a composite steel strip to a substrate, to form a blank body of the cutting assembly; and then performing low-temperature tempering treatment on a welding portion. The cutting assembly in the present invention uses three metal structures, and uses medium-high carbon steel or low alloy steel with relatively low costs as a material of the substrate, so that the costs of a hand saw with a relatively size to which the cutting assembly is applied can be reduced. A tooth tip of the hand saw uses a high-speed steel material such as M2, M42, or M35, so that the abrasive resistance of the hand saw is dramatically improved, and the service life of the saw is increased.

A method can be used to produce a component from a sandwich material in sheet or strip form, which sandwich material comprises at least two metallic surface layers and a plastic layer disposed between the metallic surface layers. The method may involve at least partially heating the sandwich material along an edge region to soften the plastic in the edge region. The plastic may then be substantially completely displaced out of the edge region by exerting a force on at least one of the metallic surface layers. In this way a plastic-free edge region is produced in which the metallic surface layers are in contact in sub-regions or at points. Further, a component comprised of a sandwich material may include at least two metallic surface layers and a plastic layer disposed between the metallic surface layers. The sandwich material may have, at least along one edge, a plastic-free region in which the metallic surface layers are in contact in sub-regions or at points.

One exemplary embodiment of this disclosure relates to a gas turbine engine, including a component having a first portion formed using one of a casting and a forging process, and a second portion formed using an additive manufacturing process.

There is provided a method of manufacturing a composite molded body that can increase a processing speed and a joining strength in a different direction. The method of manufacturing a composite molded body in which a metal molded body and a resin molded body are joined, includes the steps of: continuously irradiating a joint surface of the metal molded body with laser light at an irradiation speed of 2,000 mm/sec or more by using a continuous-wave laser; and arranging, within a mold, a portion of the metal molded body including the joint surface irradiated with the laser light in the preceding step and performing injection molding of a resin forming the resin molded body, or performing compression molding in a state where a portion of the metal molded body including the joint surface irradiated with the laser light in the preceding step and a resin forming the resin molded body are made to contact with each other.

A gas flow can be provided together with a liquid jet guided laser beam to remove accumulated liquid on the processing surface. The gas flow can have minimum interference with the liquid jet guided laser beam, while functions to blow away liquid generated by the liquid jet. Keeping the surface free from accumulated liquid can improve the efficiency of the liquid jet guided laser processing.

A laser machining method performing cutting machining to cut a composite material over a thickness direction thereof by applying a laser beam to the composite material. The method includes applying the laser beam from one side in the thickness direction of the composite material so as to form a first cutout in the composite material; and applying the laser beam from the other side in the thickness direction of the composite material, forming a second cutout in the composite material at a position opposing the first cutout, connecting the second cutout to the first cutout, and cutting the composite material. The first cutout is formed by applying the laser beam through a plurality of machining paths arranged in the width direction of the first cutout. The second cutout is formed by applying the laser beam through a plurality of machining paths arranged in the width direction of the second cutout.