C04B2237/408

CUSTOMIZED MAGNETIC SUSCEPTIBILITY MATERIALS

One example includes a method for fabricating a compound material. The method includes providing a first discrete material layer having a first thickness dimension. The first discrete material layer includes a first material having a first magnetic susceptibility. The method also includes depositing a second discrete material layer having a second thickness dimension over the first discrete material layer. The second discrete material layer can include a second material having a second magnetic susceptibility. The relative first and second thickness dimensions can be selected to provide a desired magnetic susceptibility of the compound material.

METAL-ON-CERAMIC SUBSTRATES
20170151755 · 2017-06-01 · ·

A metal-on-ceramic substrate comprises a ceramic layer, a first metal layer, and a bonding layer joining the ceramic layer to the first metal layer. The bonding layer includes thermoplastic polyimide adhesive that contains thermally conductive particles. This permits the substrate to withstand most common die attach operations, reduces residual stress in the substrate, and simplifies manufacturing processes.

SUPERCONDUCTING WIRE ROD CONNECTION STRUCTURE AND CONNECTION METHOD, AND SUPERCONDUCTING WIRE ROD

A superconducting wire rod connection structure can comprise first and second superconducting wire rods, wherein the first and second superconducting wire rods are formed by layering a base material, an intermediate layer, and a superconducting conductor layer. The base materials of the first and second superconducting wire rods can be joined to each other, and the superconducting conductor layers of the first and second superconducting wire rods can be connected by a connection wire rod including a superconducting conductor layer. Further, the superconducting wire rod connection structure can comprise a separating portion in which connection ends of the first and second superconducting wire rods with the base materials joined to each other are separated from the connection wire rod.

Joined solid production method
12263525 · 2025-04-01 · ·

A method for producing a joined solid, the method comprising placing a metal powder on a solid; covering at least a portion of the periphery of the metal powder with a high-melting-point material having a melting point higher than the melting point of the metal powder; and irradiating the metal powder, at least a portion of the periphery of which is covered with the high-melting-point material, with microwaves to heat the metal powder, thereby sintering or melt-solidifying the metal powder to form a metal solid on the solid.

Joined body, holding device, and electrostatic chuck

A joining layer of a joined body includes a joining material which contains, as a main component, a metal having a surface tension of 1000 mN/m or less at its melting point, and a metal layer which has a plurality of pores formed therein and in which at least some of the pores are impregnated with the joining material.

Metal solid production method
12246378 · 2025-03-11 · ·

Provided is a method for producing a metal solid, the method being capable of easily producing a metal solid. A method for producing a metal solid, the method comprising covering at least a portion of the periphery of a metal powder with a high-melting-point material having a melting point higher than the melting point of the metal powder; and irradiating the metal powder, at least a portion of the periphery of which is covered with the high-melting-point material, with microwaves to heat the metal powder, thereby sintering or melt-solidifying the metal powder.

JOINED BODY INCLUDING CERAMIC MEMBER AND METALLIC MEMBER AND METHOD FOR MANUFACTURING JOINED BODY
20170036961 · 2017-02-09 · ·

A joined body 10 is manufactured by joining a Mo- or Ti-made terminal 14 having a Ni coating, a Au coating, a NiAu coating (with Ni Serving as a base) to a recess 12a formed in a plate-shaped ceramic member 12 made of alumina or aluminum nitride through a joint layer 16. The joint layer 16 contains Au, Sn, Ag, Cu, and Ti and is in contact with a bottom surface of the recess 12a and with at least part of a side surface of the recess 12a (the entire side surface in this case). In the joint layer 16, its joint interface with the ceramic member 12 is Ti-rich. When the joined body 10 is cut in its thickness direction, the ratio of the total cross sectional area of pores to the cross-sectional area of the joint layer 16 (porosity) is 0.1 to 15%.

Embedding sensors in 3D-printed silicon carbide

An improved method for embedding one or more sensors in SiC is provided. The method includes depositing a binder onto successive layers of a SiC powder feedstock to produce a dimensionally stable green body have a true-sized cavity. A sensor component is then press-fit into the true-sized cavity. Alternatively, the green body is printed around the sensor component. The assembly (the green body and the sensor component) is heated within a chemical vapor infiltration (CVI) chamber for debinding, and a precursor gas is introduced for densifying the SiC matrix material. During infiltration, the sensor component becomes bonded to the densified SiC matrix, the sensor component being selected to be thermodynamically compatible with CVI byproducts at elevated temperatures, including temperatures in excess of 1000 C.

METALLIZATION AND SUPPORT COMPRISING A METALLIZATION
20250234786 · 2025-07-17 ·

A system includes a support and at least one metallization that defines at least a first layer and a second layer. The support defines a support surface on which the first layer is arranged between the support surface and the second layer, which is made of at least 90% by weight of a precious metal. The first layer is made of transition metals and/or metals and/or semi-metals and has an ultrasonic damping effect.

AIRCRAFT SEEKER WINDOWS AND AIRCRAFT WINDOW SYSTEMS INCLUDING THE SAME

An approach to seeker windows for aircraft comprises a window layer comprising an IR transparent material, the window layer comprising a first side and a second side substantially opposite the first side; and a heating layer on the first side or the second side of the window layer, the heating layer configured to apply a heating profile to the window layer to reduce thermal shock imparted to the window layer when the seeker window is exposed to hypersonic flight conditions.