Each of a plurality of divided dies (11, 12) has a divided surface (111, 121) and a defining surface (112, 122) which defines a cavity 100. The divided surface has an inclined divided surface (1112, 1212) inclined with respect to the translational direction, and at least one pair of perpendicular divided surfaces (1112, 1113, 1211, 1213) which is disposed on the opposite side based on the defining surface and is perpendicular to the translational direction. Each of the plurality of divided dies (11) and (12), while abutting against each other at, at least the at least one pair of perpendicular divided surfaces of the divided surface, abuts against each other in a state of being spaced apart from each other with a gap d within a range of 1 to 30 m at the inclined divided surface (1112, 1212), thereby forming the cavity 100.

A high toughness inorganic composite artificial stone panel and preparation method are disclosed. The panel includes a surface layer, an intermediate metal fiber toughening layer and a substrate toughening layer. The surface layer includes the following components: 40-70 parts of quartz sand, 10-30 parts of quartz powder, 20-45 parts of inorganic active powder, 0.5-4 parts of pigment, 0.3-1 part of water reducer and 3-10 parts of water. The intermediate metal fiber toughening layer includes the following components: 40-60 parts of inorganic active powder, 45-65 parts of sand, 0.8-1.5 parts of water reducer, 6-14 parts of water and 4-8 parts of metal fiber. The substrate toughening layer includes the following components: 30-50 parts of inorganic active powder, 30-55 parts of quartz sand, 15-20 parts of quartz powder, 0.5-1.2 parts of water reducer, 4-8 parts of water and 0.8-2.5 parts of toughening agent.

An organic fiber toughened inorganic composite artificial stone panel and a preparation method thereof are disclosed. The panel includes a surface layer, an intermediate organic fiber toughened layer and a toughened base layer. The surface layer includes the following components: 40-70 parts of quartz sand, 20-30 parts of quartz powder, 20-45 parts of inorganic active powder, 0.5-4 parts of pigment, 0.1-3 part of water reducing agent and 3-10 parts of water. The intermediate organic fiber toughened layer includes the following components: 40-60 parts of inorganic active powder, 45-65 parts of sand, 0.8-1.5 parts of water reducing agent, 6-14 parts of water and 4-8 parts of organic fiber. The toughened base layer includes the following components: 30-50 parts of inorganic active powder, 30-55 parts of quartz sand, 15-20 parts of quartz powder, 0.5-1.2 parts of water reducing agent, 4-8 parts of water and 0.8-2.5 parts of toughener.

A transparent sintered body having fewer air bubble-derived defects is provided. More specifically, a method is provided of producing a ceramic molded product including at least a step of pressure-molding ceramic granules having a Hausner ratio, which is a quotient obtained by dividing a tapped bulk density by a loose bulk density, of 1.0 or more but not more than 1.2. Also provided is a method of producing a transparent sintered body including at least each of the steps of the above method to obtain a ceramic molded product and a step of heating and sintering the resulting ceramic molded product. The transparent sintered body has a linear transmittance of 78% or more at a wavelength of 600 nm to 2000 nm inclusive except for an element-derived characteristic absorption wavelength.

This document describes systems and processes for forming synthetic molded slabs, which may be suitable for use in living or working spaces (e.g., along a countertop, table, floor, or the like).

A method for producing microencapsulated fuel pebble fuel more rapidly and with a matrix that engenders added safety attributes. The method includes coating fuel particles with ceramic powder; placing the coated fuel particles in a first die; applying a first current and a first pressure to the first die so as to form a fuel pebble by direct current sintering. The method may further include removing the fuel pebble from the first die and placing the fuel pebble within a bed of non-fueled matrix ceramic in a second die; and applying a second current and a second pressure to the second die so as to form a composite fuel pebble.

A method for producing microencapsulated fuel pebble fuel more rapidly and with a matrix that engenders added safety attributes. The method includes coating fuel particles with ceramic powder; placing the coated fuel particles in a first die; applying a first current and a first pressure to the first die so as to form a fuel pebble by direct current sintering. The method may further include removing the fuel pebble from the first die and placing the fuel pebble within a bed of non-fueled matrix ceramic in a second die; and applying a second current and a second pressure to the second die so as to form a composite fuel pebble.

In a method for manufacturing articles in the form of a slab or block, obtained by means of a procedure during which an initial mix comprising aggregates and a binder undergo vacuum vibro-compression followed by a step involving hardening of the binder, the aggregates comprise synthetic aggregates and fillers with a hardness greater than or equal to 5 Mohs, which contain silicon dioxide substantially only in amorphous form.

Device (1) for pressing a non-hardened concrete composition (12) into a desired form, whereby the device comprises an upper plate (4) with one or more first cavities (7) that run through the upper plate (4), a moulding plate (3) with one or more second cavities (9) whereby the upper plate (4) is located directly above the moulding plate (3), a bottom plate (2) located under the moulding plate (3) whereby the bottom plate closes the one or more second cavities (9) on the bottom, whereby the upper plate (4) and the moulding plate (3) can move horizontally in relation to each other between a first position in which the one or more first cavities (7) are directly and exactly above the one or more second cavities (9) and a second position in which the one or more first cavities (7) are not above the one or more second cavities (9), wherein the thickness of the upper plate (4) and not the thickness of the moulding plate (3) is decisive for the thickness of the final article (12,13

An apparatus for vacuum vibro-compression of mixes arranged on a support comprises a press (12) provided with a press ram (18) having vibratory devices (22), and a pressing surface (16). The press (12) comprises a vacuum bell (24). The apparatus is characterized in that it comprises an entry chamber (44) in the region of the inlet opening (36) of the bell (24) having a first opening (48) which can be controllably closed and opened with a first gate (50) adapted to prevent fluid communication between the outside and inside of the entry chamber (44) and a second gate (52) able to be controllably opened and closed, in the region of the inlet opening (36) of the bell (24), and adapted to prevent fluid communication between entry chamber (36) and the inside of the bell (24) or to allow the passage of the support with the mix from the entry chamber (36) to the inside of the bell (24). The apparatus also comprises an exit chamber (46) in the region of the outlet opening (38), having a third gate (54) provided in the region of the outlet opening (38), able to be controllably closed and opened and adapted to prevent fluid communication between the inside of the bell (24) and the inside of the exit chamber (46) or to allow the passage of the support with the compacted slab from inside the bell (24) to the exit chamber (46), and a second opening (56) which can be controllably closed and opened with a fourth gate (58) which is adapted to prevent fluid communication between the inside of the exit chamber and the outside. A method for vacuum vibro-compression of mixes contained inside a mould, comprising the steps of: inserting a support with the mix inside the entry chamber (44) and closing the first gate (50); generating a given vacuum value inside the entry chamber (44) with the first gate (50) and the second gate (52) closed; opening the second gate (52) and inserting the support inside the bell (24) where a given vacuum value is already present; closing the second gate (52) and performing vacuum vibro-compression of the mix with the second and third gates (52, 54) closed; once vibro-compression has been completed, opening the third gate (52) and transferring the support into the exit chamber (46) where a given vacuum value is already present; closing the third gate (54), restoring the atmospheric pressure inside the exit chamber (46); opening the fourth gate (58) and di