An object is to predict a microstructure of Al in an industrial process more accurately than conventional techniques. In an information processor (1), an inter-step information integration section supplies a PC(i) and an MS(i, 0) to each i-th step calculating section included in a step calculating section. Each i-th step calculating section supplies an MS(i, t) and a TMP(i, t) to a microstructure calculating section and thereby causes the microstructure calculating section to find an MS(i, tfi), and supplies the MS(i, tfi) to the inter-step information integration section (11). The inter-step information integration section (11) sets, as an MS(i+1, 0), the MS(i, tfi) received from the i-th step calculating section.

A method of forming an aluminum alloy component including melting and solidifying an aluminum alloy, solution treating the aluminum alloy, and heat treating the aluminum alloy. The aluminum alloy includes scandium, zirconium, erbium, silicon, at least one of molybdenum and tungsten, manganese and the balance aluminum and incidental impurities. The concentration of the alloying elements, in atom %, is greater than 0.0 and less than or equal to 0.15 scandium, greater than 0.0 and less than or equal to 0.35 zirconium, greater than 0.0 and less than or equal to 0.15 erbium, greater than 0.0 and less than or equal to 0.2 silicon, greater than 0.0 and less or equal to 0.75 molybdenum when included, greater than 0.0 and less than or equal to 0.35 tungsten when included.

A method of forming an aluminum alloy component including melting and solidifying an aluminum alloy, solution treating the aluminum alloy, and heat treating the aluminum alloy. The aluminum alloy includes scandium, zirconium, erbium, silicon, at least one of molybdenum and tungsten, manganese and the balance aluminum and incidental impurities. The concentration of the alloying elements, in atom %, is greater than 0.0 and less than or equal to 0.15 scandium, greater than 0.0 and less than or equal to 0.35 zirconium, greater than 0.0 and less than or equal to 0.15 erbium, greater than 0.0 and less than or equal to 0.2 silicon, greater than 0.0 and less or equal to 0.75 molybdenum when included, greater than 0.0 and less than or equal to 0.35 tungsten when included.

In a brazing sheet manufacturing method, a cladding slab is prepared by overlaying at least a core-material slab composed of an aluminum material and a filler-material slab composed of an Al—Si series alloy, in which a metal element that oxidizes more readily than Al is included in at least one of the slabs. A clad sheet is prepared by hot rolling this cladding slab, which then has at least a core material layer composed of the core-material slab and a filler material layer composed of the filler-material slab and disposed on at least one side of the core material. Then, a surface of the clad sheet is etched using a liquid etchant that contains an acid. Subsequently, the clad sheet is cold rolled to a desired thickness. In flux-free brazing, such a brazing sheet is capable of curtailing degradation in brazeability caused by fluctuations in dew point and oxygen concentration.

An alloy formed of aluminum, nickel, scandium and optionally one, two or more further metals. The aluminum alloy is suitable for additive manufacturing of lightweight highly thermally conductive components for aircraft, such as heat exchangers. In a first step, a powder of the described aluminum alloy is produced by additive manufacturing, such as laser melting in the L-PBF process. Large grains are able to grow epitaxially along the build direction thereby increasing phonon and electron mobility along the build direction. With this, a higher thermal conductivity can be achieved. In a second step, the preliminary part is hardened by precipitation of secondary phases at 250 to 400 C to form the hardened part. 3D-printed lightweight parts with high thermal conductivity are obtained.

An alloy formed of aluminum, nickel, scandium and optionally one, two or more further metals. The aluminum alloy is suitable for additive manufacturing of lightweight highly thermally conductive components for aircraft, such as heat exchangers. In a first step, a powder of the described aluminum alloy is produced by additive manufacturing, such as laser melting in the L-PBF process. Large grains are able to grow epitaxially along the build direction thereby increasing phonon and electron mobility along the build direction. With this, a higher thermal conductivity can be achieved. In a second step, the preliminary part is hardened by precipitation of secondary phases at 250 to 400 C to form the hardened part. 3D-printed lightweight parts with high thermal conductivity are obtained.

In a method of forming a beverage container, a can body is formed from a metal alloy. A can end is formed from a substantially compositionally identical metal alloy. The metal alloy is a heat treatable aluminum alloy . The heat treatable aluminum alloy is produced from up to 100% recycled aluminum material.

In a method of forming a beverage container, a can body is formed from a metal alloy. A can end is formed from a substantially compositionally identical metal alloy. The metal alloy is a heat treatable aluminum alloy . The heat treatable aluminum alloy is produced from up to 100% recycled aluminum material.

The invention provides a component formed of an aluminum alloy for use in a vehicle, for example an automotive vehicle component requiring high strength, light-weight, and a complex three-dimensional shape, and a method of manufacturing the component. The method begins by providing a blank formed of an aluminum alloy which is already solution heat treated and tempered, and thus has a temper designation of about T4. The method further includes heating the blank to a temperature of 150° C. to 350° C., preferably 190° C. to 225° C. The method next includes quickly transferring the blank to a hot or warm forming apparatus, and stamping the blank to form the complex three-dimensional shape. Immediately after the forming step, the component has a temper designation of about T6, but preferably not greater than T6, and thus is ready for use in the vehicle without any post heat treatment or machining.

The invention provides a component formed of an aluminum alloy for use in a vehicle, for example an automotive vehicle component requiring high strength, light-weight, and a complex three-dimensional shape, and a method of manufacturing the component. The method begins by providing a blank formed of an aluminum alloy which is already solution heat treated and tempered, and thus has a temper designation of about T4. The method further includes heating the blank to a temperature of 150° C. to 350° C., preferably 190° C. to 225° C. The method next includes quickly transferring the blank to a hot or warm forming apparatus, and stamping the blank to form the complex three-dimensional shape. Immediately after the forming step, the component has a temper designation of about T6, but preferably not greater than T6, and thus is ready for use in the vehicle without any post heat treatment or machining.