The invention relates to a high-strength copper-nickel-tin alloy with excellent castability, hot workability and cold workability, high resistance to abrasive wear, adhesive wear and fretting wear and improved resistance to corrosion and stress relaxation stability, consisting of (in weight %): 2.0-10.0% Ni, 2.0-10.0% Sn, 0.01-1.5% Si, 0.01-1.0% Fe, 0.002-0.45% B, 0.001-0.15% P, selectively up to a maximum of 2.0% Co, optionally also up to a maximum 2.0% Zn, selectively up to a maximum of0.25% Pb, the residue being copper and unavoidable impurities, characterised in thatthe ratio Si/B of the element contents in wt. % of the elements silicon and boron is a minimum 0.4 and a maximum 8; such that the copper-nickel-tin alloy has Si-containing and B-containing phases and phases of the systems NiSiB, NiB, FeB, NiP, FeP, NiSi and other Fe-containing phases which significantly improve the processing properties and use properties of the alloy. The invention also relates to a casting variant and a further-processed variant of the high-strength copper-nickel-tin alloy, to a production method, and to the use of the alloy.

Provided are a casting die inspection method and a casting device, the method including: a step for acquiring the ultimate pressure in a cavity section, at the time when a prescribed vacuuming time has elapsed since evacuation the inside of the cavity section of the casting die was started; a step for evacuating the inside of the cavity section and acquiring an increased pressure in the cavity section that has increased during a prescribed stop time, at the time when the prescribed stop time has elapsed since the evacuation was stopped; a step for evaluating a first sealing property of the casting device on the basis of the ultimate pressure; and a step for evaluating a second sealing property of the casting device on the basis of the increased pressure.

A core structure for a providing a cooling passage in a gas turbine engine includes a core body that has a first cooling passage core. The first cooling passage core has a first width in a chord-wise direction near a first wall. A second width in the chord-wise direction near a second wall. A third width in the chord-wise direction between the first and second walls. The third width being smaller than the first and second widths to form an hourglass shape.

A core structure for a providing a cooling passage in a gas turbine engine includes a core body that has a first cooling passage core. The first cooling passage core has a first width in a chord-wise direction near a first wall. A second width in the chord-wise direction near a second wall. A third width in the chord-wise direction between the first and second walls. The third width being smaller than the first and second widths to form an hourglass shape.

A method of casting is provided, wherein a molten material is introduced into a mould such that the molten material flows out of the mould, wherein once a desired temperature of the mould is achieved, the molten material is prevented from flowing out of the mould such that the molten material at least partially fills the mould.

A method of casting is provided, wherein a molten material is introduced into a mould such that the molten material flows out of the mould, wherein once a desired temperature of the mould is achieved, the molten material is prevented from flowing out of the mould such that the molten material at least partially fills the mould.

A mold molding method includes a binder reaction amount calculation step of calculating a reaction amount C(, t.sub.i) [wt %] (i=1, 2) of a binder, a specimen room temperature compressive strength calculation step of calculating room temperature compressive strength .sub.c(, t) [MPa] of a specimen, a mold room temperature compressive strength prediction step of predicting room temperature compressive strength .sub.ca(, t) of the mold in advance, and a mold room temperature compressive strength extraction step of extracting room temperature compressive strength .sub.ce(, t) of the mold. When the mold is actually molded, the model is removed just after elapse of the time t.sub.1, as one of the molding condition parameters which satisfies the room temperature compressive strength .sub.ce(, t).

An intermediate product for a vacuum insulation panel includes an outer covering member having a sealed space, a core material disposed in the sealed space and having heat insulation properties, and a first gas absorbent disposed in the sealed space, sealed by a container having gas barrier properties and absorbing a first specific gas, wherein the first specific gas is sealed in the sealed space, and an unsealing member configured to unseal the container when a pressing force is applied from an outside is attached to the container.

An intermediate product for a vacuum insulation panel includes an outer covering member having a sealed space, a core material disposed in the sealed space and having heat insulation properties, and a first gas absorbent disposed in the sealed space, sealed by a container having gas barrier properties and absorbing a first specific gas, wherein the first specific gas is sealed in the sealed space, and an unsealing member configured to unseal the container when a pressing force is applied from an outside is attached to the container.

A process for producing a metal alloy balance wheel by molding, the process including the following steps: a) making a mold in the negative shape of the balance wheel, b) getting hold of a metal alloy that has a thermal expansion coefficient of less than 25 ppm/ C. and is able to be in an at least partly amorphous state when it is heated to a temperature between its glass transition temperature and its crystallization temperature, c) putting the metal alloy into the mold, the metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature so as to be hot-molded and to form a balance wheel, d) cooling the metal alloy to obtain a balance wheel made of the metal alloy, e) releasing the balance wheel obtained in step d) from its mold.