Patent classifications
B23K35/325
Assembly having at least two ceramic bodies joined with one another, especially a pressure measuring cell, and method for joining ceramic bodies by means of an active hard solder, or braze
An assembly comprising: two ceramic bodies, which are joined by means of a joint of an active hard solder, or braze, wherein the active hard solder, or braze, has a continuous core volume, which is spaced, in each case, from the ceramic bodies by at least 1 m, and an average composition C.sub.K with a liquidus temperature T.sub.l(C.sub.K), wherein the composition C.sub.K has a coefficient of thermal expansion (C.sub.K), wherein (C.sub.K)=m.Math.(K), wherein m1.5, especially m1.3 and preferably m1.2, wherein (K) is the average coefficient of thermal expansion of the ceramic material of the ceramic bodies, wherein the joint has boundary layers, which border on the ceramic body, wherein at least one of the boundary layers, which lies outside of the core volume, has an average composition C.sub.B with a liquidus temperature T.sub.l(C.sub.B), which lies not less than 50 K, preferably not less than 100 K, and especially preferably not less than 200 K, under the liquidus temperature T.sub.l(C.sub.K) of the average composition C.sub.K of the core volume.
STEAM TURBINE ROTOR BLADE AND METHOD FOR MANUFACTURING STEAM TURBINE ROTOR BLADE
A steam turbine rotor blade achieving both abrasion resistance and reliability, and a method for manufacturing a steam turbine rotor blade capable of obtaining such a steam turbine rotor blade are provided. A steam turbine rotor blade according to the invention is characterized by including a blade base material and an erosion shield formed on a surface of the blade base material, wherein the blade base material is composed of a titanium alloy, and the erosion shield is composed of a weld overlay layer including a parent phase composed of pure titanium in which a metal element is solid-dissolved or a titanium alloy in which a metal element is solid-dissolved, and a hard phase dispersed in the parent phase.
Supporting unit and substrate treating apparatus including the same
A fabrication method of a supporting unit supporting a substrate is provided. The fabrication method includes providing a supporting plate that is made of a non-conductive material and configured to support the substrate, providing a base plate that is disposed under the supporting plate and made of a material containing a conductive material, and forming a first metal film on a top surface of the base plate and bonding the supporting plate with the base plate through a brazing process.
FLUX-CORED WIRE FOR GAS SHIELDED ARC WELDING
A flux-cored wire for gas shielded arc welding includes C: 0.03 to 0.09%, Si: 0.1 to 0.6%, Mn: 1.3 to 3.0%, Ti: 0.05 to 0.50%, B: 0.002 to 0.015%, and Al.sub.2O.sub.3 converted value: 0.4 to 1.0%, as the total content in the steel sheath and the flux in mass % relative to the total mass of the wire; and TiO.sub.2 converted value: 5.0 to 9.0%, SiO.sub.2 converted value: 0.2 to 0.7%, ZrO.sub.2 converted value: 0.1 to 0.6%, Mg: 0.2 to 0.8%, total of F converted value: 0.02 to 0.20%, and total of Na.sub.2O converted value and K.sub.2O converted value: 0.03 to 0.20%; as a content in the flux; in which a content of C in the steel sheath is 0.03% or less in mass % relative to the total mass of the steel sheath.
Laser net shape manufactured component using an adaptive toolpath deposition method
A laser net shape manufactured BLISK, compressor blade, turbine blade or turbine component including a plurality of overlapping predetermined variable bead widths of a material defining a first material layer, a plurality of overlapping predetermined variable bead widths of a material deposited on top of the first material layer, forming a second material layer; and additional material layers deposited on top of the first material layer and the second material layer. The variable bead width of the deposited material is controlled to maintain the approximately constant percent of bead width overlap. A first 2 to 100 deposited powder layers are deposited by a first laser power and the remaining powder layers are deposited by a laser power that is ramped down over the course of depositing the remaining powder layers. In addition, disclosed is A BLISK, compressor blade, turbine blade or turbine component formed by a method.
LEAD-FREE SOLDER COMPOSITION
A lead-free solder composition includes tin, titanium and zinc. Based on 100 parts by weight of the total weight of tin, titanium and zinc, tin is present in an amount ranging from 20 to 40 parts by weight, and titanium is present in an amount ranging from 0.01 to 0.15 parts by weight.
Toughened solder for downhole applications, methods of manufacture thereof and articles comprising the same
Disclosed herein is a solder composition comprising a metal or a metal alloy; and an electrically conductive high temperature polymeric composition; where the electrically conductive high temperature polymeric composition is dispersed homogeneously in the metal; and where the electrically conductive high temperature polymeric composition has a higher glass transition temperature or a melting point than the flow temperature of the metal or metal alloy. Disclosed herein too is a method comprising mixing an electrically conductive high temperature polymeric composition with a metal or a metal alloy to form the solder composition; where the electrically conductive high temperature polymeric composition is dispersed homogeneously in the metal; and where the electrically conductive high temperature polymeric composition has a higher glass transition temperature or a melting point than the flow temperature of the metal or metal alloy.
BRAZING TITANIUM ALUMINUM ALLOY COMPONENTS
In some examples, the disclosure describes a technique that includes covering a joint surface of a first part including a titanium aluminum (TiAl) alloy with a braze material including aluminum, where covering the joint surface includes at least one of electroplating the braze material on the joint surface, hot dipping the braze material on the joint surface, or positioning a foil of the braze material adjacent to the joint surface, positioning a second part including a titanium alloy in contact with the first part to define a joint region, where the joint region includes the braze material interposed between the second part and the joint surface of the first part, and heating the joint region to at least partially melt the braze material to form a braze joint connecting the first part to the second part.
BRAZE JOINTS WITH A DISPERSED PARTICULATE MICROSTRUCTURE
The microstructure of braze joints in polycrystalline diamond compact (PDC) cutters may be tailored to increase the shear strength of the braze joint, for example, by increasing the amount of a dispersed particulate microstructure therein. A method for forming a dispersed particulate microstructure may include brazing a polycrystalline diamond table to a hard composite substrate with a braze alloy at a braze temperature between 5 C. above a solidus temperature of the braze alloy and 200 C. above a liquidus temperature of the braze alloy; and forming a braze joint between the polycrystalline diamond table and the hard composite substrate that comprises at least 40% by volume of the dispersed particulate microstructure composed of a particulate inter-metallic phase having a diameter of 0.5 m to 2.0 m and an aspect ratio of 1 to 5 dispersed in a ductile matrix.
Toughened and corrosion- and wear-resistant composite structures and fabrication methods thereof
Composite structures having a reinforced material interjoined with a substrate, wherein the reinforced material comprises a compound selected from the group consisting of titanium monoboride, titanium diboride, and combinations thereof.