The present invention relates to a welded structural member having excellent corrosion resistance and crack resistance, and a method for manufacturing same.

The invention relates to a method for laser welding the end faces of joints (2, 2.1) of two connecting flanges, which are held against each other, of two connecting partners (1, 1.1) made from a steel material, of which at least one is provided with a metallic coating with an evaporation temperature that is below the melting temperature of the steel material. The method is carried out such that, for the process of laser welding, the connecting flanges (1, 1.1) of the two connecting partners (1, 1.1) are held against each other enclosing an angle that opens pointing in a direction from the joint side on which the laser is applied, as a result of which a degassing gap (5), which increases in the direction of heat introduction, is provided between the connecting flanges (3, 3.1), through which degassing gap evaporation products of the coating material (8, 8.1) resulting from the introduction of heat are carried off.

A method for non-destructive testing a cutting insert to determine coating thickness id disclosed. The method includes the steps of using a source of electromagnetic energy to ablate a surface of the cutting insert to non-destructively form a geometric feature and expose the substrate and each layer of the coating; and measuring the thickness of each layer of the coating. In one example, the geometric feature is a groove with a generally trapezoidal shape. In other examples, the groove can have a U-shape, V-shape, and the like. The thickness of each layer of the coating is determined using focus variation, contrast detection, confocal microscopy, an interferometric microscopy, an imaging interferometric microscopy, or similar technique.

The present invention relates to a method for creating modifications in a solid state, wherein a crack guidance region for guiding a crack for separating a solid-state portion, in particular a solid-state layer, from the solid state body, is predetermined by the modifications. The method according to the invention preferably comprises the steps: Moving the solid state (1) relative to a laser processing system, then generating a plurality of laser beams by means of the laser processing system for creating at least one modification, wherein the laser processing system is adjusted for defined focusing of the laser beams continuously as a function of a plurality of parameters, in particular at least two parameters.

The invention relates to a method for machining a multi-layer workpiece blank (3) by means of a laser beam, comprising the following steps: specifying a machining program for machining the workpiece blank according to an ablation geometry in order to generate a desired edge and/or surface geometry (13) using a laser machining device; tensioning the workpiece blank in the laser machining device and positioning the workpiece holder in a measuring position; measuring a thickness of at least one of the layers of the multi-layer workpiece blank (3); modifying the machining program in order to machine the multi-layer workpiece blank (3) according to the measured layer thickness with an consistent ablation geometry; and machining the tensioned workpiece blank (3) using the modified machining program via a laser of the laser machining device in order to generate the desired edge and/or surface geometry (13) with a cutting edge (12). The invention also relates to a correspondingly configured device.

A plate heat exchanger includes a number of titanium plates arranged in a plate package. Every second plate is a titanium plate that has been cladded with a melting depressant foil on each side of the plate, and at least every second titanium plate has a corrugated pattern, such that tops and bottoms are formed in the plate. The cladded titanium plates are stacked on the corrugated titanium plates, so as to form the plate package of titanium plates. Contact areas are formed between adjacent titanium plates in the plate package. The plate package of titanium plates has been heated, such that the melting depressant foil has acted as a melting depressant for the titanium in the cladded titanium plates and caused surface layers of the cladded titanium plates to melt and flow to the contact areas between adjacent titanium plates and form joints at the contact areas between adjacent titanium plates when the melted titanium has been allowed to solidify.

Provided herein are anode assembly, conductive contact strips, electrochemical cells containing the anode assembly and the conductive contact strips, and methods to use and manufacture the same, where the anode assembly includes a plurality of V-shaped, U-shaped, or Z-shaped elements positioned outside the anode shell and in electrical contact with the anode.

Disclosed are a high-strength corrosion-resistant cladding chequered steel and a manufacturing method therefor. The high-strength corrosion-resistant cladding chequered steel includes a substrate and a chequered cladding layer cladded on the substrate by single-sided or double-sided rolling. The mass percentages of the chemical elements of the substrate are: C: 0.01% to 0.20%, Si: 0.10% to 0.5%, Mn: 0.5% to 2.0%, Al: 0.02% to 0.04%, Ti: 0.005% to 0.018%, Nb: 0.005% to 0.020%, 0<B0.0003%, N0.006%, and the balance being steel and other inevitable impurities. The high-strength corrosion-resistant cladding steel plate has a high strength, a high corrosion resistance, a yield strength 470 MPa, a tensile strength 610 MPa, a shear strength 410 MPa, and an elongation 40%.

A brazed joint having excellent tensile strength (TSS and CTS) and a method of production of the same are provided. A sheet combination 200 comprised of steel sheets 210, 220 between which a brazing filler metal 230 is clamped is heated at a temperature of the Ac3 point of the steel sheet (matrix material) or more. The Ar3 point of the regions near the brazing filler metal at the steel sheets is made higher than the Ar3 point of the steel sheets (matrix material), then the quenching start temperature X is made a temperature of the Ar3 point of the steel sheet (matrix material) or less and hot stamping is performed to produce a brazed joint.

In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.