Provided is a polycrystalline ceramic substrate to be bonded to a compound semiconductor substrate with a bonding layer interposed therebetween, wherein at least one of relational expression (1) 0.7<.sub.1/.sub.2<0.9 and relational expression (2) 0.7<.sub.3/.sub.4<0.9 holds, where .sub.1 represents a linear expansion coefficient of the polycrystalline ceramic substrate at 30 C. to 300 C. and .sub.2 represents a linear expansion coefficient of the compound semiconductor substrate at 30 C. to 300 C., and .sub.3 represents a linear expansion coefficient of the polycrystalline ceramic substrate at 30 C. to 1000 C. and .sub.4 represents a linear expansion coefficient of the compound semiconductor substrate at 30 C. to 1000 C.

A ceramic article includes a flexible backing selected from paper, woven fabric, non-woven fabric, polymeric films, metal foils, and combinations thereof. A green ceramic layer is on a first side of the flexible backing, wherein the green ceramic layer includes a ceramic material and a polymeric binder. A major surface of the green ceramic layer includes a pattern of features.

A system for producing chemicals, such as, ethylene or gasoline, at high temperature (above 1100 degrees C.) having a feedstock source. The system includes a chemical conversion portion connected with the feedstock source to receive feedstock and convert the feedstock to ethylene or gasoline. The conversion portion includes a coil array and a furnace that heats the feedstock to temperatures in excess of 1100 C. or 1200 C. or even 1250 C. or even 1300 C. or even 1400 C. A method for producing chemicals, such as ethylene or gasoline, at high temperature.

An apparatus and method of manufacturing a porous ceramic segmented honeycomb body (340,340) comprising axial channels (216) extending from a first end face (220) to a second end face (224). A plurality of porous ceramic honeycomb segments (204) is moved axially past respective apertures (110) of an adhesive applying device (100). Adhesive (118) is applied through openings (126) in the adhesive applying device (100) onto peripheral axial surfaces of each porous ceramic honeycomb segment (204). The plurality of porous ceramic honeycomb segments (204) enters a wide opening (318) of a tapered chamber (314) and exits a narrow opening (322) of the tapered chamber (314); a tapered wall (326) from the wide opening (318) to the narrow opening (322) presses the plurality of porous ceramic honeycomb segments (204) together forming the porous ceramic segmented honeycomb body (340,340). The adhesive (118) on the peripheral axial surfaces between respective porous ceramic honeycomb segments (204) is distributed by the pressing.

A container comprising: a container body that includes a wall portion separating inside and outside and is formed of a long-fiber-reinforced silicon-carbide composite material obtained by combining monofilaments of silicon carbide with a silicon carbide matrix, the wall portion having a thickness equal to a specific dimension; and a lid configured to close an opening of the container body, formed of a material containing at least silicon carbide, and equipped with such a wall portion separating inside and outside that thickness is within a range of 1 to 3 times the specific dimension.

The invention provides tooling (100) for acting during heat treatment to support a preform (110) of a three-dimensional part obtained by shaping a metal or ceramic powder, the preform presenting at least one bearing surface (112) on which it can rest and at least one suspended surface (111) that is suspended relative to the bearing surface, the tooling comprising a tray (120), and a plurality of blocks (130) arranged on the tray and each having at least one surface (130a) for supporting the preform, the blocks being suitable for moving relative to one another by sliding on the tray between a first position in which the blocks are spaced apart from one another and together define a first volume, and a second position in which the blocks together define a second volume that is smaller than the first volume. The invention also provides a method of heat treating a preform made of powder and using such tooling.

A ceramic matrix composite component and methods of making are described herein. The ceramic matrix composite may include a silicon containing matrix and refractory fibers embedded within the silicon containing matrix. The ceramic matrix composite component may further include a silicide layer sandwiched between the silicon containing matrix and the refractory fibers. A method of forming a ceramic matrix composite may include infiltrating a fluid that includes a refractory metal element containing compound into a fiber preform that includes fibers. The method may further include depositing the refractory metal element from the refractory metal element containing compound onto the fibers and forming, from the refractory metal element deposited onto the fibers, a refractory metal silicide.

A bonding tape for joining carbide ceramic structures, wherein the bonding tape comprises: a mixture comprising carbide ceramic particles, preceramic polymer liquid, fine carbon particles and metal nanoparticles that form a eutectic liquid at temperatures below 1400? C.

A method of assembling a composite panel includes disposing a pliable matrix material between a first side of a ceramic core structure and a ceramic matrix composite face sheet, wherein the ceramic core structure comprises a plurality of hollow cells defined by a plurality of walls extending from the first side of the ceramic core structure to a second side of the ceramic core structure opposite the first side; and densifying the pliable matrix material to bond the pliable matrix material with the ceramic core structure and the ceramic matrix composite face sheet.

Ceramic composite materials that are reinforced with carbide fibers can exhibit ultra-high temperature resistance. For example, such materials may exhibit very low creep at temperatures of up to 2700 F. (1480 C.). The present composites are specifically engineered to exhibit matched thermodynamically stable crystalline phases between the materials included within the composite. In other words, the reinforcing fibers, a debonding interface layer disposed over the reinforcing fibers, and the matrix material of the composite may all be of the same crystalline structural phase (all hexagonal), for increased compatibility and improved properties. Such composite materials may be used in numerous applications.