CN215882887U - Composite stone crystal floor - Google Patents

Abstract

The embodiment of the application discloses compound brilliant floor of stone sets up to multilayer structure, its characterized in that includes: a co-extruded foamed substrate layer (100), the co-extruded foamed substrate layer (100) at least comprising a first structural layer (110), a second structural layer (120) anda third structural layer (130); the second structural layer (120) is located intermediate the first structural layer (110) and the third structural layer (130), and the second structural layer (120) has a foamed density of less than 1.1g/cm³. The composite stone-crystal floor has low density, good thermal stability and rigidity and simple manufacturing process.

Description

Composite stone crystal floor

Technical Field

The application relates to the technical field of floors, in particular to a composite stone crystal floor.

Background

Common floorings mainly include wood-plastic floorings and stone-plastic floorings. The wood-plastic floor has complex processing procedures, so the production efficiency is low. And the thermal stability of the wood-plastic floor is poor, and the wood-plastic floor is easy to warp and deform in the using process. Although the stone plastic floor has better stability, the density is higher and the transportation cost is higher. Therefore, it is necessary to provide a flooring having a low density and a good stability.

SUMMERY OF THE UTILITY MODEL

One of the embodiments of the present specification provides a composite stone crystal floor, including: the co-extrusion foaming base material layer at least comprises a first structural layer, a second structural layer and a third structural layer; the second structural layer is positioned between the first structural layer and the third structural layer, and the foaming density of the second structural layer is less than 1.1g/cm³。

One of the embodiments of the present specification provides a method for preparing the composite stone-crystal floor, including the following steps: and respectively pretreating the raw materials of the first structural layer, the second structural layer and the third structural layer, and then sending the pretreated raw materials into a co-extrusion extruder to form a semi-finished product of the co-extrusion foaming base material layer.

Drawings

The present description will be further explained by way of exemplary embodiments, which will be described in detail by way of the accompanying drawings. These embodiments are not intended to be limiting, and in these embodiments like numerals are used to indicate like structures, wherein:

FIG. 1 is a cross-sectional view of a coextruded foamed substrate layer of a composite stone grain floor according to some embodiments of the present application.

Fig. 2 is a cross-sectional view of a decorative layer of a composite stone grain floor panel according to some embodiments of the present application.

FIG. 3 is an exemplary block diagram of a composite stone grain floor according to some embodiments of the present application.

FIG. 4 is an exemplary flow chart of a method of manufacturing a composite stone grain floor according to some embodiments of the present application.

FIG. 5 is a block diagram illustrating an exemplary apparatus for manufacturing a composite stone floor according to some embodiments of the present disclosure.

Fig. 6 is an exemplary side view of a sizing sleeve according to some embodiments of the present application.

FIG. 7 is an exemplary block diagram illustrating the connection of a sizing sleeve to a mold according to some embodiments of the present application.

FIG. 8 is an exemplary block diagram of a cooling roller set according to some embodiments of the present application.

Detailed Description

In order to more clearly illustrate the technical solutions of the embodiments of the present disclosure, the drawings used in the description of the embodiments will be briefly described below. It is obvious that the drawings in the following description are only examples or embodiments of the present description, and that for a person skilled in the art, the present description can also be applied to other similar scenarios on the basis of these drawings without inventive effort. Unless otherwise apparent from the context, or otherwise indicated, like reference numbers in the figures refer to the same structure or operation.

It should be understood that "system", "apparatus", "unit" and/or "module" as used herein is a method for distinguishing different components, elements, parts, portions or assemblies at different levels. However, other words may be substituted by other expressions if they accomplish the same purpose.

As used in this specification and the appended claims, the terms "a," "an," "the," and/or "the" are not intended to be inclusive in the singular, but rather are intended to be inclusive in the plural, unless the context clearly dictates otherwise. In general, the terms "comprises" and "comprising" merely indicate that steps and elements are included which are explicitly identified, that the steps and elements do not form an exclusive list, and that a method or apparatus may include other steps or elements.

Flow charts are used in this description to illustrate operations performed by a system according to embodiments of the present description. It should be understood that the preceding or following operations are not necessarily performed in the exact order in which they are performed. Rather, the various steps may be processed in reverse order or simultaneously. Meanwhile, other operations may be added to the processes, or a certain step or several steps of operations may be removed from the processes.

FIG. 1 is a cross-sectional view of a coextruded foamed substrate layer of a composite stone grain floor according to some embodiments of the present application.

In some embodiments, the composite stone grain flooring may be provided as a multi-layered structure. For example, a composite stone grain floor may include a coextruded foamed substrate layer 100. For another example, the composite stone grain flooring may include a co-extruded foamed substrate layer 100 and a decorative layer 200 disposed on the co-extruded foamed substrate layer 100. For another example, the composite stone floor may include a co-extruded foamed substrate layer 100, a decorative layer 200 disposed on the co-extruded foamed substrate layer 100, and a backing layer disposed under the co-extruded foamed substrate layer 100. The composite stone-crystal floor can also comprise other structural layers. For a description of the decorative layer 200 and the backing layer, reference may be made to fig. 2, 3 and their associated description.

The coextruded foamed substrate layer 100 may include at least one first structural layer 110, at least one second structural layer 120, and at least one third structural layer 130. In some embodiments, the number of at least one first structural layer 110, at least one second structural layer 120, and at least one third structural layer 130 may include, but is not limited to, 1, 2, 3, etc. In some embodiments, the number of the at least one first structural layer 110, the at least one second structural layer 120, and the at least one third structural layer 130 may be equal or unequal.

Second structural layer 120 may be located intermediate first structural layer 110 and third structural layer 130. As shown in fig. 1, the second structural layer 120 may be located on the third structural layer 130, and the second structural layer 120 may be located under the first structural layer 110. In some embodiments, other layers may or may not be included between second structural layer 120 and third structural layer 130 and/or between second structural layer 120 and first structural layer 110.

In some embodiments, the first structural layer 110, the second structural layer 120, and the third structural layer 130 may be formed by hot pressing. For a detailed description of the hot press forming, reference may be made to fig. 4 and its related description. In some embodiments, second structural layer 120 may be disposed below first structural layer 110 by an adhesive. In some embodiments, the second structural layer 120 may be disposed on the third structural layer 130 by an adhesive. The adhesive means a substance that adheres objects to each other. For example, the binder may be a PLA resin, a phenolic resin, or the like.

Second structural layer 120 may be a foamed layer. The foaming layer can be foamed through a foaming agent, and the density of the foaming layer is reduced, so that the layer has light weight. Details regarding the blowing agent can be found in the associated description below.

In some embodiments, the foamed density of second structural layer 120 may be less than 1.1g/cm³. In some embodiments, the foamed density of second structural layer 120 may be less than 1.0g/cm³. In some embodiments, the foamed density of second structural layer 120 may be less than 0.9g/cm³. In some embodiments, the foamed density of second structural layer 120 may be less than 0.8g/cm³. In some embodiments, the foamed density of second structural layer 120 may be less than 0.7g/cm³。

In some embodiments, the foamed density of second structural layer 120 may be equal to 1.1g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 1.05g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 1.0g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 0.95g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 0.9g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 0.85g/cm³. In some embodiments, the foaming of the second structural layer 120The density may be equal to 0.8g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 0.75g/cm³. In some embodiments, the foamed density of second structural layer 120 may be equal to 0.7g/cm³。

In some embodiments, the composition of second structural layer 120 may include 90-110 parts by weight polyvinyl chloride and at least one of the following components, based on 274.25 parts by weight of second structural layer 120: 100-200 parts of inorganic filler, 0.8-1.0 part of polyethylene wax, 6.0-8.0 parts of stabilizer, 0.9-1.1 parts of stearic acid, 1.6-2.1 parts of foaming agent and 12-15 parts of foaming regulator. For example, the composition of the second structural layer 120 may include 90-110 parts by weight of polyvinyl chloride, 100-200 parts by weight of inorganic filler, 0.8-1.0 part by weight of polyethylene wax, 6.0-8.0 parts by weight of stabilizer, 0.9-1.1 parts by weight of stearic acid, 1.6-2.1 parts by weight of foaming agent, 12-15 parts by weight of foaming regulator, based on 274.25 parts by weight of the second structural layer 120.

In some embodiments, the polyvinyl chloride may be present in an amount of 91 to 109 parts by weight. In some embodiments, the polyvinyl chloride may be present in an amount of 92 to 108 parts by weight. In some embodiments, the polyvinyl chloride may be present in an amount of 93 to 107 parts by weight. In some embodiments, the polyvinyl chloride may be present in an amount of 94 to 106 parts by weight. In some embodiments, the polyvinyl chloride may be 95 to 105 parts by weight. In some embodiments, the polyvinyl chloride may be 96-104 parts by weight. In some embodiments, the polyvinyl chloride may be 97 to 103 parts by weight. In some embodiments, the polyvinyl chloride may be 98-102 parts by weight. In some embodiments, the polyvinyl chloride may be 99 to 101 parts by weight. In some embodiments, the polyvinyl chloride may be 100 parts by weight.

In some embodiments, the weight portion of inorganic filler may be 105-. In some embodiments, the weight portion of the inorganic filler may be 110-. In some embodiments, the weight portion of inorganic filler may be 115-185. In some embodiments, the weight fraction of inorganic filler may be 120-180. In some embodiments, the weight portion of inorganic filler may be 125-175. In some embodiments, the weight fraction of inorganic filler may be 130-170. In some embodiments, the weight fraction of inorganic filler may be 135-165. In some embodiments, the weight fraction of inorganic filler may be 140-160. In some embodiments, the weight portion of inorganic filler may be 145-155. In some embodiments, the weight part of the inorganic filler may be 150.

In some embodiments, the polyethylene wax may be present in an amount of 0.82 to 0.98 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.84 to 0.96 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.86 to 0.94 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.88 to 0.92 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.89 to 0.91 parts by weight.

In some embodiments, the weight parts of the stabilizer may be 6.2 to 7.8. In some embodiments, the weight parts of the stabilizer may be 6.4 to 7.6. In some embodiments, the weight parts of the stabilizer may be 6.6 to 7.4. In some embodiments, the weight parts of the stabilizer may be 6.8 to 7.2. In some embodiments, the weight parts of the stabilizer may be 6.9 to 7.1.

In some embodiments, the stearic acid may be present in an amount of 0.92 to 1.08 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.94 to 1.06 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.96 to 1.04 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.98 to 1.02 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.99 to 1.01 parts by weight.

In some embodiments, the blowing agent may be 1.6 to 2.1 parts by weight. In some embodiments, the blowing agent may be 1.7 to 2.0 parts by weight. In some embodiments, the blowing agent may be 1.8 to 1.9 parts by weight. In some embodiments, the blowing agent may be 1.85 to 1.95 parts by weight.

In some embodiments, the foaming modifier may be present in an amount of 12 to 15 parts by weight. In some embodiments, the foaming modifier may be present in an amount of 12.5 to 14.5 parts by weight. In some embodiments, the foaming modifier may be present in 13 to 14 parts by weight. In some embodiments, the foaming modifier may be present in 13.4 to 13.6 parts by weight.

In some embodiments, a stabilizer refers to an agent that maintains the structure of the polymeric compound stable. For example, the stabilizer may include calcium stearate, dibasic lead salt, zinc stearate, organotin, carboxylate or fatty acid salt of rare earth element, or the like. The stabilizer may also be other substances.

In some embodiments, a foaming agent refers to an agent that foams a substance (e.g., second structural layer 120) into pores. In some embodiments, the blowing agent may include a yellow blowing agent and a white blowing agent. In some embodiments, the yellow blowing agent may comprise azodicarbonamide and the white blowing agent may comprise sodium bicarbonate.

In some embodiments, the foaming modifier may be an acrylate. In some embodiments, the acrylates may include methyl acrylate, ethyl acrylate, methyl 2-methacrylate, or ethyl 2-methacrylate, among others.

The foaming regulator can promote the plasticizing process, improve the elasticity of the melt, enhance the elongation and strength of the melt, make the plasticizing more uniform, facilitate the covering of bubbles, prevent bubble collapse, make the foaming bubbles uniform and compact, and thus improve the foaming quality.

In some embodiments, at least one of the following components may be included based on 95 parts by weight of the inorganic filler: 81-89 parts of modified fly ash, 3-7 parts of hollow glass beads and 8-12 parts of composite calcium. For example, the following components may be included based on 95 parts by weight of the inorganic filler: 81-89 parts of modified fly ash, 3-7 parts of hollow glass beads and 8-12 parts of composite calcium.

In some embodiments, modified fly ash may refer to fly ash that has been modified. In some embodiments, the modification treatment may include, but is not limited to, pyrogenic modification, acid modification, base modification, and the like. In some embodiments, the modified fly ash may be 82 to 88 parts by weight. In some embodiments, the modified fly ash can be 83 to 87 parts by weight. In some embodiments, the modified fly ash can be 84-86 parts by weight. In some embodiments, the modified fly ash can be 84.5 to 85.5 parts by weight. In some embodiments, the modified fly ash can be 85 parts by weight.

In some embodiments, the modified fly ash can include microbeads. In some embodiments, the modified fly ash can have a bead content of 40% to 60%. In some embodiments, the modified fly ash can have a microbead content of 41% to 59%. In some embodiments, the modified fly ash can have a bead content of 42% to 58%. In some embodiments, the modified fly ash can have a microbead content of 43% to 57%. In some embodiments, the modified fly ash can have a bead content of 44% to 56%. In some embodiments, the modified fly ash can have a microbead content of 45% to 55%. In some embodiments, the modified fly ash can have a bead content of 46% to 54%. In some embodiments, the modified fly ash can have a bead content of 47% to 53%. In some embodiments, the modified fly ash can have a bead content of 48% to 52%. In some embodiments, the modified fly ash can have a bead content of 49% to 51%. In some embodiments, the modified fly ash can have a microbead content of 50%. In some embodiments, the amount of microbeads in the modified fly ash can be anywhere from 40% to 60%.

In some embodiments, the modified fly ash can have a mesh size of 325 mesh to 400 mesh. In some embodiments, the modified fly ash can have a mesh size of 330-395 mesh. In some embodiments, the modified fly ash may have a mesh size of 335-390 mesh. In some embodiments, the modified fly ash can have a mesh size of 340-385 mesh. In some embodiments, the modified fly ash may have a mesh size of 345-380. In some embodiments, the modified fly ash may have a mesh size of 350-375 mesh. In some embodiments, the modified fly ash may have a mesh size of 355-370. In some embodiments, the modified fly ash may have a mesh size of 360-365 mesh.

In some embodiments, the hollow glass beads may refer to hollow glass beads having a particle size of 10 μm to 250 μm, and spherical hollow or quasi-spherical glass beads. The embodiment of the specification adopts the hollow glass beads as the filler, so that the density of the stone crystal floor can be reduced, and the creep resistance of the floor can be improved.

In some embodiments, the hollow glass microspheres may be present in an amount of 3.2 to 6.8 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 3.5 to 6.5 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 3.8 to 6.2 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 4 to 6 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 4.2 to 5.8 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 4.5 to 5.5 parts by weight. In some embodiments, the hollow glass microspheres may be present in an amount of 4.8 to 5.2 parts by weight. In some embodiments, the hollow glass microspheres may be present in 5 parts by weight.

In some embodiments, the weight parts of the composite calcium may be 8.2-11.8. In some embodiments, the weight parts of the composite calcium may be 8.4-11.6. In some embodiments, the weight part of the composite calcium may be 8.6-11.4. In some embodiments, the weight part of the composite calcium may be 8.8-11.2. In some embodiments, the composite calcium may be 9 to 11 parts by weight. In some embodiments, the weight part of the composite calcium may be 9.2 to 10.8. In some embodiments, the calcium complex may be 9.4 to 10.6 parts by weight. In some embodiments, the weight part of the composite calcium may be 9.6-10.4. In some embodiments, the weight part of the composite calcium may be 9.8-10.2. In some embodiments, the weight part of the composite calcium may be 10.

In some embodiments, the composite calcium component comprises at least: 60 to 80 percent of heavy calcium carbonate and 20 to 40 percent of light calcium carbonate. In some embodiments, the content of ground calcium carbonate may be in the range of 62% to 78%. In some embodiments, the content of ground calcium carbonate may be in the range of 64% -76%. In some embodiments, the content of ground calcium carbonate may be in the range of 66% -74%. In some embodiments, the content of ground calcium carbonate may be in the range of 68% to 72%. In some embodiments, the content of ground calcium carbonate may be in the range of 69% -71%.

In some embodiments, the ground calcium carbonate may have a mesh size of 800 mesh to 1250 mesh. In some embodiments, the ground calcium carbonate may have a mesh size of 850 mesh to 1200 mesh. In some embodiments, the ground calcium carbonate may have a mesh size of 900 mesh to 1150 mesh. In some embodiments, the ground calcium carbonate may have a mesh size of 950 mesh to 1100 mesh. In some embodiments, the ground calcium carbonate may have a mesh size of 1000 mesh to 1050 mesh.

In some embodiments, the light calcium carbonate content may be in the range of 22% -38%. In some embodiments, the light calcium carbonate content may be in the range of 24% -36%. In some embodiments, the light calcium carbonate content may be in the range of 26% -34%, and in some embodiments, the light calcium carbonate content may be in the range of 28% -32%. In some embodiments, the light calcium carbonate content may be in the range of 29% -31%.

In some embodiments, the light calcium carbonate may have a mesh size of 800 mesh to 1250 mesh. In some embodiments, the light calcium carbonate may have a mesh size of 850 mesh to 1200 mesh. In some embodiments, the light calcium carbonate may have a mesh size of 900 mesh to 1150 mesh. In some embodiments, the light calcium carbonate may have a mesh size of 950 mesh to 1100 mesh. In some embodiments, the light calcium carbonate may have a mesh size of 1000 mesh to 1050 mesh.

In some embodiments, the mesh size of the ground calcium carbonate may be the same as or different from the mesh size of the light calcium carbonate.

The amount of the inorganic filler and other components in the second structural layer 120 needs to be controlled within a reasonable range, which is helpful for improving the performance of the stone crystal floor. For example, the proper amount of composite calcium and hollow glass beads can reduce the screw torque, improve the material fluidity and the plasticizing rate and reduce the PVC decomposition; meanwhile, 800-plus 1250-mesh composite calcium can improve the fine density of foaming cells, the hollow glass beads can reduce the density of products, the using amount of foaming agents is reduced, and the foaming multiplying power and the compactness of the cells can be effectively controlled.

The second structure layer 120 is filled with the modified fly ash, the composite calcium and the hollow glass beads, so that the defects of poor dispersibility, poor compatibility, high water absorbability and the like when organic fibers such as bamboo, rice husks, straws and the like are used as the filling materials are overcome. The density of the composite stone crystal floor can be further reduced through chemical foaming, and the sound absorption performance of the composite stone crystal floor is improved.

In some embodiments, the first structural layer 110 and/or the third structural layer 130 may be a layer of thermally stable material. The thermal stable material layer is characterized in that the material layer is not easy to deform and has good stability within a certain temperature variation range. Specifically, the degree of deformation is less than 0.065% at a temperature change of less than 80 ℃.

In some embodiments, the first structural layer 110 and/or the third structural layer 130 comprises 90-110 parts by weight polyvinyl chloride and at least one of the following components based on 425.85 parts by weight of the first structural layer 110 or the third structural layer 130: 270-330 parts of inorganic filler, 0.4-1.2 parts of polyethylene wax, 3.0-6.0 parts of stabilizer, 0.4-1.4 parts of stearic acid, 0.1-0.5 part of oxidized polyethylene wax, 8-10 parts of ABS resin, 5-15 parts of plasticizer and 0.2-0.5 part of carbon black. For example, the first structural layer 110 and/or the third structural layer 130 may include 90 to 110 parts by weight of polyvinyl chloride, 270 parts by weight of inorganic filler, 0.4 to 1.2 parts by weight of polyethylene wax, 3.0 to 6.0 parts by weight of stabilizer, 0.4 to 1.4 parts by weight of stearic acid, 0.1 to 0.5 parts by weight of oxidized polyethylene wax, 8 to 10 parts by weight of ABS resin, 5 to 15 parts by weight of plasticizer, 0.2 to 0.5 parts by weight of carbon black, based on 425.85 parts by weight of the first structural layer 110 or the third structural layer 130.

In some embodiments, the polyvinyl chloride may be present in an amount of 91 to 109 parts by weight. In some embodiments, the polyvinyl chloride may be present in an amount of 92 to 108 parts by weight. In some embodiments, the polyvinyl chloride may be present in an amount of 94 to 106 parts by weight. In some embodiments, the polyvinyl chloride may be 96-104 parts by weight. In some embodiments, the polyvinyl chloride may be 98-102 parts by weight. In some embodiments, the polyvinyl chloride may be 100 parts by weight.

In some embodiments, the weight fraction of inorganic filler may be 275-. In some embodiments, the weight fraction of inorganic filler may be 280-320. In some embodiments, the weight portion of inorganic filler may be 285-. In some embodiments, the weight fraction of inorganic filler may be 290-310. In some embodiments, the weight fraction of inorganic filler may be 295-305. In some embodiments, the weight part of the inorganic filler may be 300.

In some embodiments, the polyethylene wax may be present in an amount of 0.4 to 1.2 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.5 to 1.1 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.6 to 1.0 parts by weight. In some embodiments, the polyethylene wax may be present in an amount of 0.7 to 0.9 parts by weight. In some embodiments, the polyethylene wax may be 0.8 parts by weight.

In some embodiments, the weight parts of the stabilizer may be 3.2 to 5.8. In some embodiments, the weight parts of the stabilizer may be 3.4 to 5.6. In some embodiments, the weight parts of the stabilizer may be 3.6 to 5.4. In some embodiments, the weight parts of the stabilizer may be 3.8 to 5.2. In some embodiments, the weight parts of the stabilizer may be 4.0 to 5.0. In some embodiments, the weight parts of the stabilizer may be 4.2 to 4.8. In some embodiments, the weight parts of the stabilizer may be 4.4 to 4.6. In some embodiments, the weight part of the stabilizer may be 4.5.

In some embodiments, the stearic acid may be present in an amount of 0.5 to 1.3 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.6 to 1.2 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.7 to 1.1 parts by weight. In some embodiments, the stearic acid may be present in an amount of 0.8 to 1.0 parts by weight. In some embodiments, the weight part of stearic acid may be 0.9.

In some embodiments, the oxidized polyethylene wax can be present in an amount of 0.1 to 0.5 parts by weight. In some embodiments, the oxidized polyethylene wax can be present in an amount of 0.15 to 0.45 parts by weight. In some embodiments, the oxidized polyethylene wax can be present in an amount of 0.2 to 0.4 parts by weight. In some embodiments, the oxidized polyethylene wax can be present in an amount of 0.25 to 0.35 parts by weight. In some embodiments, the oxidized polyethylene wax can be 0.3 parts by weight.

In some embodiments, the ABS resin may be 8.2 to 9.8 parts by weight. In some embodiments, the ABS resin may be 8.4 to 9.6 parts by weight. In some embodiments, the ABS resin may be 8.6 to 9.4 parts by weight. In some embodiments, the ABS resin may be 8.8 to 9.2 parts by weight. In some embodiments, the ABS resin may be 9 parts by weight.

In some embodiments, the plasticizer may be present in an amount of 6 to 14 parts by weight. In some embodiments, the plasticizer may be present in an amount of 7 to 13 parts by weight. In some embodiments, the plasticizer may be present in an amount of 8 to 12 parts by weight. In some embodiments, the plasticizer may be 9 to 11 parts by weight. In some embodiments, the plasticizer may be 10 parts by weight.

In some embodiments, the carbon black may be present in an amount of 0.22 to 0.48 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.24 to 0.46 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.26 to 0.44 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.28 to 0.42 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.3 to 0.4 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.32 to 0.38 parts by weight. In some embodiments, the carbon black may be present in an amount of 0.34 to 0.36 parts by weight. In some embodiments, the weight part of carbon black may be 0.35.

The stabilizer is an agent for keeping the structure of the polymer compound stable and preventing the decomposition and aging thereof. In some embodiments, the stabilizer may be calcium stearate. In some embodiments, the stabilizer may be a dibasic lead salt. The stabilizer may also be other substances.

In some embodiments, the oxidized polyethylene wax can be a high density oxidized wax having an acid number of 30 and a viscosity of 25000cps at 180 ℃. The high-density oxidized wax has excellent external lubricity, strong internal lubrication effect and coupling effect, has good compatibility with polyolefin resin and the like, and can improve the plasticizing speed and reduce the processing temperature when being applied to a polyvinyl chloride high-filling formula system.

The plasticizer is a substance added to the polymer to increase the plasticity and flexibility of the polymer. For example, the plasticizer may be one or more of dibutyl phthalate (DBP), dioctyl phthalate (DOP), epoxidized soybean oil, tricresyl phosphate, triphenyl phosphate, dioctyl sebacate, or chlorinated paraffin. The plasticizer may also be other substances which meet the definition of plasticizer.

In some embodiments, the ABS resin may be an acrylonitrile-butadiene-styrene copolymer. Because the ABS resin has a rigid chain segment and a flexible rubber chain segment, the blending of ABS/PVC (polyvinyl chloride) can improve the Vicat softening point and the shock resistance of the composite stone-crystal floor.

In some embodiments, first structural layer 110 and/or third structural layer 130 may include an inorganic filler.

In some embodiments, the inorganic filler may include at least one of ground calcium carbonate, hollow glass microspheres. For example, the inorganic filler may include ground calcium carbonate and hollow glass microspheres.

In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be no greater than 35%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 1% to 33%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 3% to 31%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 5% to 29%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 7% to 27%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 9% to 25%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 11% -23%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 13% to 21%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 15% to 19%. In some embodiments, the ratio of parts by weight of the hollow glass microspheres to parts by weight of the inorganic filler may be in the range of 16% to 18%.

In some embodiments, the heavy calcium carbonate has a skeleton function, can improve the hardness and the heat resistance of the composite stone crystal floor, is low in price and can save the cost.

In some embodiments, the hollow glass microspheres may be spherical and flow-like as compared to other irregularly shaped fillersThe mobility is better. In some embodiments, the hollow glass microspheres may have a density of 0.40g/cm³-0.75g/cm³Within the range. The hollow glass beads can reduce the density of the composite stone-crystal floor, and can effectively improve the rigidity, creep resistance and thermal stability of the composite stone-crystal floor, so that the composite stone-crystal floor is not easy to deform in the using process.

Fig. 2 is a cross-sectional view of the structure of the decorative layer of a composite stone grain floor according to some embodiments of the present application.

In some embodiments, a decorative layer 200 may be disposed over the coextruded foamed substrate layer 100. In some embodiments, decorative layer 200 may include at least one of UV coating 210, wear layer 220, or color film layer 230.

In some embodiments, the UV coating 210 includes at least one of a primer layer, a topcoat layer, and a surface cured film. The primer layer refers to a first base coating layer applied directly to the surface of the object. The surface paint layer is a paint layer coated on the primer layer of the object and close to the surface of the object. The surface cured film is a film obtained by subjecting the top coat layer to a press curing treatment. For example, the surface-cured film may be a PET polyester film, a polymer polyester skin-touch film, or the like.

In some embodiments, the wear layer 220 may comprise a wear resistant material. In some embodiments, the wear resistant material may include alumina, zirconia, silicon carbide, wear resistant steel, wear resistant cast iron, and the like. For example, the wear layer 220 may be made of an overlay paper of aluminum oxide impregnated with melamine resin. The wear layer 220 has wear resistance, scratch resistance, burning resistance, pollution resistance, corrosion resistance, moisture resistance and the like.

The color film layer 230 is a part having a decorative function. Such as a textured or patterned structure.

In some embodiments, UV coating 210 may be disposed over abrasion resistant layer 220. In some embodiments, the wear layer 220 may be disposed over the color film layer 230. In some embodiments, the UV coating 210, the wear layer 220, and the color film layer 230 may be provided as a unitary structure. In some embodiments, the color film layer 230 may be disposed on the first structural layer 110 by an adhesive. The adhesive means a substance that adheres objects to each other. For example, the binder may be a PLA resin, a phenolic resin, or the like.

In some embodiments, the decorative layer 200 may also include at least one of a wood veneer, a bamboo veneer, or a melamine paper.

In some embodiments, the UV coating 210 may be disposed on the upper layer of the wear layer 220 by thermal lamination, and the wear layer 220 may also be disposed on the upper layer of the color film layer 230 by thermal lamination. In some embodiments, the UV coating layer 210, the wear layer 220, and the color film layer 230 may also be formed by one-time thermal compounding in order from top to bottom. Thermal compounding refers to a process of compounding objects with each other by a certain temperature.

FIG. 3 is an exemplary block diagram of a composite stone grain floor according to some embodiments of the present application. The composite stone-crystal floor comprises a co-extruded foaming base material layer 100 and a decoration layer 200.

The coextruded foamed substrate layer 100 may include at least a first structural layer 110, a second structural layer 120, and a third structural layer 130, which are sequentially formed in a stacking order from top to bottom. For the specific composition and connection manner of the co-extruded foamed substrate layer 100 and the decoration layer 200, reference can be made to the related contents of fig. 1-2.

In some embodiments, additional structural layers may be disposed between first structural layer 110, second structural layer 120, and third structural layer 130.

In some embodiments, the composite stone floor may further include a backing layer (not shown). The backing layer may include at least one of a cork pad, an IXPE mute pad, an EVA mute pad, or a rubber mute pad. The backing layer may be disposed below the coextruded foamed substrate layer 100, or other suitable location.

FIG. 4 is an exemplary flow chart of a method of manufacturing a composite stone grain floor according to some embodiments of the present application. The composite stone-crystal floor comprises a co-extrusion foaming base material layer 100. In some embodiments, the composite stone grain flooring may also include a decorative layer 200, such as a UV coating 210, a color film layer 230, an abrasion resistant layer 220, and the like.

As shown in fig. 4, the method for manufacturing the composite stone floor may include the following steps.

Step 410, respectively preprocessing the raw materials of the first structural layer 110, the second structural layer 120 and the third structural layer 130, and then sending the preprocessed raw materials into a co-extrusion extruder to form a semi-finished product of a co-extrusion foaming substrate layer.

In some embodiments, the pre-processing may include: mixing and stirring the raw materials of the first structural layer 110 or the third structural layer 130, and heating to a first preset temperature to obtain a first ingredient; and mixing and stirring the raw materials of the second structural layer 120, and heating to a second preset temperature to obtain a second ingredient.

The first predetermined temperature may be used to pretreat the starting materials of the first structural layer 110 and/or the third structural layer 130. The first preset temperature may include a first stirring temperature-increasing stage and a first temperature-decreasing cooling stage.

In some embodiments, the maximum temperature of the first agitation ramp stage may be set at 90-115 ℃. In some embodiments, the maximum temperature of the first agitation ramp stage may be set at 95-110 ℃. In some embodiments, the maximum temperature of the first stirred ramp-up stage may be set at 100-.

In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 55 ℃. In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 56 ℃. In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 57 ℃. In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 58 ℃. In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 59 ℃. In some embodiments, the minimum temperature of the first desuperheating cooling stage may be set to exceed 60 ℃.

In some embodiments, the temperature of the first stirring ramp may not exceed 115 ℃ after the plasticizer is added in order to prevent premature plasticization of the components. In some embodiments, the temperature of the first stirred warming stage may not exceed 110 ℃. In some embodiments, the temperature of the first stirred warming stage may not exceed 105 ℃. In some embodiments, the temperature of the first stirred warming stage may not exceed 100 ℃.

In some embodiments, the raw materials of the first structural layer 110 and the third structural layer 130 are weighed according to the component ratio and then stirred at a high speed. Heating the raw materials to 90-115 ℃ under high-speed stirring, cooling the raw materials to 55 ℃ under low-speed stirring, and obtaining the ingredient I.

In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 30 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 28 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 25 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 23 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 20 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 18 min. In some embodiments, the feedstock is stirred at high speed for a temperature rise time of no more than 15 min.

In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 30 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 28 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 25 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 23 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 20 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 18 min. In some embodiments, the time for cooling the raw materials by low-speed stirring can be no more than 15 min.

The second predetermined temperature is used for pre-treating the raw material of the second structural layer 120. The second preset temperature may include a second stirring temperature-increasing stage and a second temperature-decreasing cooling stage.

In order to prevent the foaming agent from decomposing in advance and avoid the loss of the foaming agent, the highest temperature of the second stirring temperature rise stage needs to be controlled. In some embodiments, the maximum temperature of the second agitation ramp stage may be set to not exceed 110 ℃. In some embodiments, the maximum temperature of the second agitation ramp stage may be set to not exceed 105 ℃. In some embodiments, the maximum temperature of the second agitation ramp stage may be set to not exceed 100 ℃. In some embodiments, the maximum temperature of the second agitation ramp stage may be set to not exceed 95 ℃. In some embodiments, the maximum temperature of the second agitation ramp stage may be set to not exceed 90 ℃.

In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 55 ℃. In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 56 ℃. In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 57 ℃. In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 58 ℃. In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 59 ℃. In some embodiments, the minimum temperature of the second desuperheating cooling stage may be set to exceed 60 ℃.

In some embodiments, the raw materials of the second structural layer 120 are weighed according to the component proportions and stirred, after the temperature of the raw materials is raised to 110 ℃ under high-speed stirring, the raw materials are cooled to 55 ℃ under low-speed stirring, and then the second ingredient is obtained. In some embodiments, weighing may be performed by an automated metering system or weighing instrument.

From the foregoing, the batch materials are pre-treated with the raw materials of the first structural layer 110 and/or the third structural layer 130. The second ingredient is prepared by pretreating the raw materials of the second structural layer 120.

For the definition of the first structural layer 110, the raw material of the first structural layer 110, the second structural layer 120, the raw material of the third structural layer 130 and the raw material of the third structural layer 130, reference may be made to the description of fig. 1-2.

In some embodiments, the extrusion process of the ingredient may include: feeding the first ingredient into a first extruder through a feeding machine for plasticizing and extruding, and feeding the second ingredient into a second extruder through the feeding machine for plasticizing and extruding; a batch one plasticating extrusion enters the dispenser to extrude the first structural layer 110 and the third structural layer 130 and a batch two plasticating extrusion enters the dispenser to extrude the second structural layer 120.

The co-extrusion extruder is a device which makes the heated raw material in a viscous flow state pass through an extrusion molding die to form a die body with a cross section similar to the shape of the die. The viscous flow state refers to the mechanical state of the amorphous high molecular polymer under the action of higher temperature and larger external force for a long time. In some embodiments, the co-extruder may include a main extruder, a co-extruder, a blanking device, a PLC control system, a dispenser, and a die. In some embodiments, the blanking device may be disposed on the extruder. The main extruder and the distributor can be connected by a confluence core passage. The co-extruder and the distributor can also be connected through a confluence core channel. The dispenser may be associated with the mold. In some embodiments, the die may have a cross-sectional shaped channel. In some embodiments, a PLC control system may be used to control the operation of the various components of the co-extruder (e.g., the main extruder, the co-extruder, the blanking device, the dispenser, and/or the die).

In some embodiments, the raw materials for the first structural layer 110 and the third structural layer 130 are pre-treated and fed into one of a main extruder and a co-extruder, plasticized and extruded into a dispenser, and the dispenser extrudes the first structural layer 110 and the third structural layer 130 into a mold. Then, the raw material of the second structural layer 120 is pretreated and then put into one of the main extruder and the co-extruder, plasticized and extruded to the distributor, and the distributor extrudes the second structural layer 120 to the same die. And finally, foaming and forming the material in a mould to obtain a semi-finished product of the co-extruded foamed substrate layer.

The semi-finished product of the co-extruded foamed substrate layer is an intermediate product which is partially processed and is not manufactured into the final co-extruded foamed substrate layer.

After the foaming molding, because the temperature of the semi-finished product of the co-extruded foaming substrate layer is higher, the cells are broken for preventing the secondary foaming with overhigh temperature, and therefore the semi-finished product of the co-extruded foaming substrate layer needs to be cooled. In some embodiments, the process 400 may further include a cooling pre-shaping process and a cooling shaping process. In some embodiments, a shaping sleeve can be used for carrying out cooling and pre-shaping treatment on the semi-finished product of the co-extruded foamed substrate layer, so that preparation is made for subsequent cooling and shaping treatment, the whole cooling and shaping treatment is more efficient, and the co-extruded foamed substrate layer and the composite stone floor with better performance (for example, better thermal stability and the like) can be further prepared. For the cooling and setting process, reference may be made to the following description, which is not repeated herein.

In some embodiments, the foaming thickness can be controlled by the die lip gap, and a 5cm-15cm conduction oil sizing sleeve can be arranged in front of the die lip. The heat conducting oil is sleeved in the shaping sleeve and can be used for carrying out cooling and pre-shaping treatment on the semi-finished product of the co-extruded foamed substrate layer. In some embodiments, the temperature of the calibrator may be set to 90 ℃ to 180 ℃. In some embodiments, the temperature of the calibrator may be set to 100 ℃ to 170 ℃. In some embodiments, the temperature of the calibrator may be set to 110 ℃ to 160 ℃. In some embodiments, the temperature of the calibrator may be set to 120 ℃ to 150 ℃. In some embodiments, the temperature of the calibrator may be set to 130 ℃ to 140 ℃.

And step 420, carrying out calender roll group treatment on the semi-finished product of the co-extruded foamed base material layer to obtain the co-extruded foamed base material layer 100.

The rollers may comprise cylindrical rotatable assemblies. The set of rollers may consist of one or more rollers.

In some embodiments, the rolls and sets of rolls may be used to perform one or more of roll calendering, printing, and cooling. The roll stack can be named as a calender roll stack, a cooling roll stack or a printing roll stack depending on the function of the roll stack.

The cooling roller group is one or more groups of roller assemblies for cooling and shaping functions. After the rolling roller group is separated, the rolled product begins to gradually cool. Because through the foaming shaping back, the temperature of crowded foaming substrate layer semi-manufactured goods still is higher altogether, for preventing that the high temperature secondary from foaming, leads to the cell to break, consequently needs make crowded foaming substrate layer semi-manufactured goods cooling down through a set of cooling roller set and cools off altogether.

The roller body of the cooling roller may include a cavity. In some embodiments, the cavity may be filled with cooling water to cool the product passing through the cooling drum.

In some embodiments, a cooling roller set may be used to perform a cooling and shaping process on the semi-finished product of the co-extruded foamed substrate layer. In some embodiments, the temperature of the cooling water in the cooling roller set may be set to 15 ℃ to 30 ℃. In some embodiments, the temperature of the cooling water in the cooling roller set may be set to 17 ℃ to 28 ℃. In some embodiments, the temperature of the cooling water in the cooling roller set may be set to 19 ℃ to 26 ℃. In some embodiments, the temperature of the cooling water in the cooling roller set may be set to 21 ℃ to 24 ℃.

In some embodiments, the cooling roll stack may be fixed before the calender roll stack. In some embodiments, the cooling roller set and the calender roller set may be controlled by the same or different control systems. For example, the speed adjustment of the cooling roll stack can be controlled by the same PLC control system as the calender roll stack to achieve speed synchronization. For another example, a certain set of rolls may be individually speed-regulated. In some embodiments, the cooling roll spacing may be controlled and adjusted by pneumatic hydraulic means or servo motor lead screw lifting means.

In some embodiments, the roll set treatment may be performed on the semi-finished product of the co-extruded foamed substrate layer by using a roll set group to obtain the co-extruded foamed substrate layer.

The calender roll stack may be one or more sets of roll assemblies that perform the function of roll calendering.

In some embodiments, the calender roll stack can include at least one calender roll stack. As shown in fig. 5, the roll stack can include a first roll stack and a second roll stack.

Roll calendering refers to the application of pressure to a material with a roll to cause it to stretch. For example, plasticized thermoplastic materials close to the viscous regime temperature are passed through a series of horizontal roll gaps rotating in opposite directions, which subject the material to compression and expansion, to a sheet-like semifinished or finished sheet having a certain thickness, width and surface finish. The viscous state refers to the mechanical state of the amorphous high molecular polymer under the action of high temperature and large external force for a long time.

The calender roll stack may be one or more sets of roll assemblies that perform a roll printing function.

In some embodiments, the same set of rollers may function as one or more of a calender set, a cooling set, and a printing set.

In some embodiments, the location between the sets of rolls and the operating temperature may be set according to actual requirements in the production process.

And 430, rolling and calendering the co-extruded foamed base material layer, the color film layer and the wear-resistant layer for one-time forming to obtain the composite stone-crystal floor.

In some embodiments, the co-extruded foamed substrate layer may be infrared-heated to a third preset temperature by using an infrared heating cover, so that the co-extruded foamed substrate layer is formed by laminating with the color film layer and the wear-resistant layer. In some embodiments, the third predetermined temperature may facilitate co-extruding the foamed substrate layer 100 with the decorative layer 200 (e.g., the color film layer 230, the wear layer 220) to form a composite stone grain floor.

The third preset temperature may be a preset temperature range in which different structural layers are thermally compounded and a bonding effect is achieved. The temperature interval is set according to the type of the structural layer. In some embodiments, the third predetermined temperature may be 155 ℃ to 175 ℃. In some embodiments, the third predetermined temperature may be 158 ℃ to 172 ℃. In some embodiments, the third predetermined temperature may be 160 ℃ to 170 ℃. In some embodiments, the third predetermined temperature may be 162 ℃ to 168 ℃. In some embodiments, the third preset temperature may be 165 ℃.

The infrared heating mantle may be a component that raises the temperature of the object to a certain temperature by using an infrared heating technique. For example, the infrared heating dome may include an infrared heating dome lamp.

Infrared heating may include radiant heating. For example, energy can be transmitted through electromagnetic waves, molecules and atoms in the object generate strong vibration and rotation, and the vibration and the rotation raise the temperature of the object to achieve the purpose of heating.

The roller printing is a printing process which continuously transfers printing paste to the surface of a material through patterns or patterns concavely engraved on a printing roller and through mechanical continuous rotation.

Combining the step 420 and the step 430, the semi-finished product of the co-extruded foamed base material layer can enter two groups of cooling roller sets to cool and shape the surface of the semi-finished product, and the water temperature can be set to be 15-30 ℃. And then the semi-finished product of the co-extruded foamed substrate layer enters a first calender roll group and a second calender roll group for heat preservation and fixed-thickness forming treatment to obtain the co-extruded foamed substrate layer. The roll temperature of the calender roll group can be set to be 130-180 ℃. An infrared heating cover can be arranged above the co-extrusion foaming base material layer after the extrusion roller group is discharged, and the temperature rise treatment is carried out on the extrusion roller group. The surface temperature of the co-extrusion foaming base material layer can be utilized to thermally compound the base material layer with the color film layer 230 and the wear-resistant layer 220, and the embossing roller set is used for carrying out plate pattern pressing and one-step forming to obtain the composite stone-crystal floor.

It should be noted that the above description related to the flow 400 is only for illustration and description, and does not limit the applicable scope of the present specification. Various modifications and changes to flow 400 will be apparent to those skilled in the art in light of this description. However, such modifications and variations are intended to be within the scope of the present description. For example, the process 400 may further include that a back-up layer may be compounded under the co-extruded foamed substrate layer 100.

FIG. 5 is a block diagram illustrating an exemplary apparatus for manufacturing a composite stone floor according to some embodiments of the present disclosure.

The apparatus 500 for manufacturing a composite stone-crystal floor may include a first extruder 502, a second extruder 504, a distributor 506, a mold 508, a cooling roller set 510, a calender roller set 512, an embossing roller set 516, and the like. In some embodiments, the cooling roll stack 510 and/or the calendar roll stack 512 can be provided in multiple sets. For example, the cooling roller set 510 can include a first cooling roller set 5101 and a second cooling roller set 5102. For example, the roll group 512 may include a first roll group 5121 and a second roll group 5122, and the like.

In some embodiments, the components of the preparation device 500 may be connected in series as shown in fig. 5. The connection order of the components of the preparation apparatus 500 may be adjusted according to the need. The present specification does not set any limit to the order of the components of the manufacturing apparatus 500.

The first extruder 502 may be used to extrude a compound-plasticating agent. The ingredients, once plasticated and extruded, may enter the dispenser 506 to form the first structural layer 110 and the third structural layer 130. For a description of ingredient one, reference may be made to fig. 4 and its associated description.

Second extruder 504 may be used to plasticize and extrude a second ingredient, which may then enter dispenser 506 to form second structural layer 120. For the related description of ingredient two, refer to fig. 4 and the related description thereof in this specification.

In some embodiments, the temperatures of the first extruder 502 and the second extruder 504 may be set in zones. For example, the temperatures in the various zones of the first extruder 502 may be set as: first 200 ℃, second 195 ℃, third 190 ℃, fourth 185 ℃, fifth 180 ℃ and a confluence core of 170 ℃.

In some embodiments, the temperature of the second extruder 504 may be set in zones. For example, the temperatures in the various zones of the second extruder 504 may be set as: first zone 165 ℃, second zone 170 ℃, third zone 190 ℃, fourth zone 180 ℃, fifth zone 180 ℃, core 170 ℃.

In some embodiments, the first extruder 502 and the second extruder 504 can be commercially available twin-cone twin-screw extruders. In some embodiments, a twin-cone twin-screw extruder may include a blanking system, an evacuation system, a main machine barrel, a linkage, a power unit, and a control system. In some embodiments, the first extruder 502 and the second extruder 504 may be piped into the distributor 506 through a connector.

In some embodiments, dispenser 506 may include three layers for first structural layer 110, second structural layer 120, and third structural layer 130, respectively. In some embodiments, the distributor 506 may include flow channels that may be used to connect the first extruder 502 and the second extruder 504, respectively.

In some embodiments, the mold 508 may be used for foam molding. The die lip gap of the die can be adjusted to control the foaming thickness.

In some embodiments, the cooling roller set 510 can cool and shape the surface of the material entering the gap. As shown in fig. 5, the cooling roller set 510 may include a first cooling roller set 5101 and a second cooling roller set 5102. In some embodiments, the roll spacing of the first and/or second sets of cooling rolls 5101, 5102 can be adjusted by pneumatic hydraulic means or servo motor lead screw lifting control. In some embodiments, the rollers of the first and/or second sets of cooling rollers 5101 and 5102 can include cavities. In some embodiments, the cavities may be treated with cooling water to cool material passing through the first and/or second sets of cooling rollers 5101 and 5102. In some embodiments, the cooling water temperature of the first cooling roll set 5101 and/or the second cooling roll set 5102 may be set as desired. For example, the cooling water temperature may be set to 15 ℃ to 30 ℃. For a description of the cooling roller set 510, reference may be made to fig. 8 and its associated description.

In some embodiments, the calender roll stack 512 may be used to perform a roll calendering operation on the material. In some embodiments, the roll stack 512 can include a first roll stack 5121 and a second roll stack 5122. In some embodiments, the temperatures of the first and second roll sets 5121, 5122 can be set the same or different as desired. For example, the temperature of the first calender roll group 5121 may be set to 90 ℃ to 130 ℃. The temperature of the second calender roll group 5122 may be set to 140 ℃ to 160 ℃.

In some embodiments, the control system for the calender roll stack 512 and the chill roll stack 510 may be the same or different. In some embodiments, the speed of the calender roll stack 512 and the chill roll stack 510 can be controlled to be the same or different. In some embodiments, the speed of the first and/or second sets of cooling rolls 5101, 5102 can be the same or different. In some embodiments, the speeds of the first and second roll sets 5121, 5122 can be the same or different.

In some embodiments, the preparation device 500 may also include an infrared heating hood 514. An infrared heating jacket 514 can be disposed over the roll stack 512 (e.g., the second roll stack 5122) to heat treat the roll stack 512 (e.g., the second roll stack 5122). For example, the infrared heating hood 514 can heat the co-extruded foamed substrate layer to thermally compound the color film layer and the wear layer. In some embodiments, the temperature of the infrared heating mask 514 can be greater than the temperature of the roll set 512 (e.g., the second roll set 5122). For example, the temperature of the infrared heating mantle 514 may be set to 165 ℃.

In some embodiments, an embossing roller set 516 may be used to emboss and press form the material. In some embodiments, the nip roll temperature of the set of nip rolls 516 may be set as desired. For example, the temperature of the embossing roll set 516 may be set to 25 ℃ to 35 ℃.

In some embodiments, the preparation device 500 may further comprise a sizing sleeve. A sizing sleeve may be disposed at the lip exit of the die 508. The sizing sleeve can cool and pre-shape the material in a heat conduction oil mode. In some embodiments, the temperature of the sizing sleeve may be set as desired. For example, the temperature of the calibrator may be set to 90 ℃ to 180 ℃. For another example, the temperature of the calibrator may be set to 100 ℃ to 170 ℃. For another example, the temperature of the calibrator may be set to 110 ℃ to 160 ℃. For another example, the temperature of the calibrator may be set to 120 ℃ to 150 ℃. For another example, the temperature of the calibrator may be set to 130 ℃ to 140 ℃. The related description of the sizing sleeve can be seen in fig. 6 and the related description thereof.

In some embodiments, the preparation device 500 may further include a PLC control system. A PLC control system may be used to control the operation of the various components of the production apparatus 500 (e.g., the first extruder 502, the second extruder 504, the dispenser 506, the die 508, the cooling roller set 510, the calendar roller set 512, the infrared heating mantle 514, the embossing roller set 516, and/or the sizing sleeve). For example, a PLC control system can be used to control the speed of the chill roll stack 510, the calender roll stack 512, and/or the embossing roll stack 516. As another example, a PLC control system may be used to control the heating power of infrared heating jacket 514. Also for example, the PLC control system may be used to control the spacing, etc., of the sizing dies 602.

Fig. 6 is an exemplary side view of a sizing sleeve according to some embodiments of the present application.

In some embodiments, the sizing sleeve 600 may include a sizing sleeve die 602 and a heat transfer oil inlet and outlet. In some embodiments, the spacing of the sizing dies 602 may be adjusted according to the lip thickness of the die 508.

In order to be able to pre-shape the material, the width of the sizing sleeve 600 may be set as desired. In some embodiments, the width d of the sizing sleeve 600 may be set to 5cm to 15 cm. In some embodiments, the width d of the sizing sleeve 600 may be set to 6cm to 14 cm. In some embodiments, the width d of the sizing sleeve 600 may be set to 7cm-13 cm. In some embodiments, the width d of the sizing sleeve 600 may be set to 8cm-12 cm. In some embodiments, the width d of the sizing sleeve 600 may be set to 9cm-11 cm. In some embodiments, the width d of the sizing sleeve 600 may be set to 10 cm.

In some embodiments, the sizing sleeve 600 may be provided with a plurality of hot oil ports. As shown in fig. 6, there may be 4 hot oil ports. For example, the hot oil inlet and outlet can include a first hot oil outlet 604, a fourth hot oil inlet 606, a second hot oil inlet 608, and a third hot oil outlet 610.

In some embodiments, the sizing sleeve 600 may be provided with screw fixing locations 612. FIG. 7 is an exemplary block diagram illustrating the connection of a sizing sleeve to a mold according to some embodiments of the present application. As shown in fig. 7, screw retaining locations 612 may be used to secure the sizing sleeve 600 to the die 508 via screws such that the lip outlet 5081 of the die 508 corresponds to the sizing sleeve die 602.

In the embodiment of the specification, the heat conduction oil shaping sleeve 600 is matched with the cooling roller group 510 and the calender roller group 512, so that the bubble holes are not broken, the co-extrusion substrate surface is not subjected to temperature loss while the substrate is shaped, one-time thermal composite pressing forming can be realized, the composite stone crystal floor is more convenient to process, and the production cost is further reduced.

FIG. 8 is an exemplary block diagram of a cooling roller set according to some embodiments of the present application.

The cooling roller set 510 may include a first cooling roller 5103 and a second cooling roller 5104. In some embodiments, the spacing b between the first and second chill rolls 5103, 5104 can be adjusted as desired. For example, the spacing b between the first and second cooling rolls 5103 and 5104 may be determined according to the thickness of the target material. The target material may refer to the material after passing through the cooling roller set 510.

In some embodiments, the cooling roller set 510 may further include a first securing member 5105 and a second securing member 5106. The first and second fixing members 5105 and 5106 may be used to adjust a distance b between the first and second cooling rollers 5103 and 5104. The first and second fixing members 5105 and 5106 may also serve to fix the first and second cooling rollers 5103 and 5104, so as to fix the interval b between the adjusted first and second cooling rollers 5103 and 5104.

In some embodiments, the configuration of the calender roll set 512 and the embossing roll set 516 can be similar or identical to the configuration of the cooling roll set 510.

Example one

The content of the modified fly ash in the second structural layer 120 is selected differently, which has different influences on the performance detection result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the compositions in the first structural layer 110 and the third structural layer 130 were set as: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground calcium carbonate, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of a stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 0.4 part by weight of carbon black, and 15 parts by weight of a plasticizer (dibutyl phthalate).

The components in second structural layer 120 are set as: 100 parts by weight of polyvinyl chloride, 40 parts by weight of composite calcium (the content of heavy calcium carbonate is 70%, and the content of light calcium carbonate is 30%), 10 parts by weight of hollow glass microspheres, 1.0 part by weight of polyethylene wax, 8.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of yellow foaming agent (azodicarbonamide), 1.2 parts by weight of white foaming agent (sodium bicarbonate), 15 parts by weight of a foaming regulator (ethyl acrylate), and different parts by weight of modified fly ash.

The test results include the performance of the composite stone floor in terms of density (ISO23996), normal temperature warping (ISO23999), thermal deformation Vicat, static bending strength (GB/T17657), heating dimensional change rate (ISO23999) and hardness (GB/T2411) of the second structural layer 120. Wherein, the hardness of second structure layer 120 refers to the ability of second structure layer 120 to resist hard objects pressed into its surface.

(1) When the content of the modified fly ash isWhen the weight is set to 50 parts, the obtained performance test result is as follows: the density was 1.306g/cm²The normal temperature warping degree is 0.50mm, the thermal deformation Vicat is 60 ℃, the static bending strength is 25MPa, the heating size change is 0.13%, and the hardness is 75 HD.

(2) When the content of the modified fly ash is set as 100 parts by weight, the obtained performance test result is as follows: the density was 1.330g/cm²The normal temperature warping degree is 0.35mm, the thermal deformation Vicat is 60 ℃, the static bending strength is 33MPa, the heating size change is 0.08%, and the hardness is 77 HD.

(3) When the content of the modified fly ash is set to 150 parts by weight, the obtained performance test result is as follows: the density is 1.380g/cm²The normal temperature warping degree is 0.20mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 35MPa, the heating size change is 0.10%, and the hardness is 81 HD.

Experimental data show that under the condition that the components of the first structural layer 110 and the third structural layer 130 are the same and the other components in the second structural layer 120 are the same, when the content of the modified fly ash is 100 parts by weight and 150 parts by weight, the material has better normal-temperature warping resistance, static bending strength and hardness, and the performance is obviously better than that of the modified fly ash with the content of 50 parts by weight. These experimental data for the modified fly ash content of second structural layer 120 may be the basis for the relevant examples.

Example two

The content of the hollow glass beads in the second structure layer 120 is selected differently, which has different influences on the performance detection result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the compositions in the first structural layer 110 and the third structural layer 130 were set as: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground calcium carbonate, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of a stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 0.4 part by weight of carbon black, and 15 parts by weight of a plasticizer (dibutyl phthalate).

The components in second structural layer 120 are set as: 100 parts by weight of polyvinyl chloride, 150 parts by weight of modified fly ash, 40 parts by weight of composite calcium (the content of heavy calcium carbonate is 70%, and the content of light calcium carbonate is 30%), 1.0 part by weight of polyethylene wax, 8.0 parts by weight of stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of yellow foaming agent (azodicarbonamide), 1.2 parts by weight of white foaming agent (sodium bicarbonate), 15 parts by weight of foaming regulator (ethyl acrylate) and different parts by weight of hollow glass microspheres.

The test results include the performance of the composite stone floor in terms of density (ISO23996), normal temperature warping (ISO23999), thermal deformation Vicat, static bending strength (GB/T17657) and heating dimensional change rate (ISO 23999).

(1) When the hollow glass beads are set to 5 parts by weight, the obtained performance test result is as follows: the density is 1.390g/cm²The normal temperature warping degree is 0.23mm, the thermal deformation Vicat is 65 ℃, the static bending strength is 31MPa, and the heating size change is 0.11%.

(2) When the hollow glass microspheres are set to 7.5 parts by weight, the obtained performance test result is as follows: the density was 1.382g/cm²The normal temperature warping degree is 0.25mm, the thermal deformation Vicat is 69 ℃, the static bending strength is 32MPa, and the heating size change is 0.10%.

(3) When the hollow glass beads are set to 10 parts by weight, the obtained performance test result is as follows: the density is 1.380g/cm²The normal temperature warping degree is 0.20mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 35MPa, and the heating size change is 0.10%.

Experimental data show that under the condition that the components of the first structural layer 110 and the third structural layer 130 are the same and other components of the second structural layer 120 are the same, when the content of the hollow glass beads is 5-10 parts by weight, the material has good normal-temperature warping resistance and static bending strength and good thermal stability. These experimental data of the hollow glass beads of the second structural layer 120 may be used as a basis for the related examples.

EXAMPLE III

The content of the composite calcium in the second structure layer 120 is selected differently, which has different effects on the performance test result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the compositions in the first structural layer 110 and the third structural layer 130 were set as: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground calcium carbonate, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of a stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 0.4 part by weight of carbon black, and 15 parts by weight of a plasticizer (dibutyl phthalate).

The components in second structural layer 120 are set as: 100 parts by weight of polyvinyl chloride, 150 parts by weight of modified fly ash, 10 parts by weight of hollow glass beads, 1.0 part by weight of polyethylene wax, 8.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of a yellow foaming agent (azodicarbonamide), 1.2 parts by weight of a white foaming agent (sodium bicarbonate), 15 parts by weight of a foaming regulator (ethyl acrylate) and different parts by weight of composite calcium.

The test results include the performance of the composite stone floor in terms of density (ISO23996), normal temperature warpage (ISO23999), thermal deformation Vicat, static bending strength (GB/T17657) and cell diameter.

(1) When the composite calcium is set to 20 parts by weight (the content of heavy calcium carbonate is 70 percent, and the content of light calcium carbonate is 30 percent), the obtained performance test result is as follows: the density was 1.392g/cm²The normal temperature warping degree is 0.33mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 30MPa, and the diameter of the foam hole is 180 mu m.

(2) When the composite calcium is set to 30 parts by weight (the content of heavy calcium carbonate is 70 percent, and the content of light calcium carbonate is 30 percent), the obtained performance test result is as follows: the density is 1.383g/cm²The normal temperature warping degree is 0.27mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 31.8MPa, and the diameter of the foam hole is 160 mu m.

(3) When the composite calcium is set to 40 parts by weight (the content of heavy calcium carbonate is 70 percent, and the content of light calcium carbonate is 30 percent), the obtained performance test result is as follows: the density is 1.380g/cm²At normal temperatureWarpage of 0.20mm, thermal deformation Vicat of 70 deg.C, static bending strength of 35MPa, and cell diameter of 150 μm.

The experimental data show that under the condition that the components of the first structural layer 110 and the third structural layer 130 are the same and the other components of the second structural layer 120 are the same, when the composite calcium content of the second structural layer 120 is 40 parts by weight, the material has better normal temperature buckling resistance and static bending strength, the cell diameter is relatively smaller, and the performance is better than the performance of the material when the composite calcium content is 20 parts by weight and 30 parts by weight. These experimental data of the composite calcium content of second structural layer 120 may be used as a basis for the related examples.

Example four

The proportion of the composite calcium in the second structure layer 120 is selected differently (or the weight parts of the light calcium and the heavy calcium in the composite calcium are selected differently), which has different effects on the performance detection result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the compositions in the first structural layer 110 and the third structural layer 130 were set as: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground calcium carbonate, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of a stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 0.4 part by weight of carbon black, and 15 parts by weight of a plasticizer (dibutyl phthalate).

The components in second structural layer 120 are set as: 100 parts by weight of polyvinyl chloride, 150 parts by weight of modified fly ash, 10 parts by weight of hollow glass beads, 1.0 part by weight of polyethylene wax, 8.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of a yellow foaming agent (azodicarbonamide), 1.2 parts by weight of a white foaming agent (sodium bicarbonate), 15 parts by weight of a foaming regulator (ethyl acrylate) and 40 parts by weight of composite calcium. Wherein, the content ratio of heavy calcium carbonate and light calcium carbonate in the composite calcium is different.

The test results include the performance of the composite stone-crystal floor in terms of density (ISO23996), normal temperature warpage (ISO23999) and cell diameter.

(1) When the content of heavy calcium carbonate in the composite calcium is 80% and the content of light calcium carbonate is 20% (the weight portion of heavy calcium carbonate is 32 parts and the weight portion of light calcium carbonate is 8 parts), the obtained performance test result is as follows: the density is 1.383g/cm²The normal temperature warping degree is 0.10mm, and the diameter of the foam hole is 160 mu m.

(2) When the content of the heavy calcium carbonate in the composite calcium is 70% and the content of the light calcium carbonate in the composite calcium is 30% (the weight parts of the heavy calcium carbonate are 28 parts and the weight parts of the light calcium carbonate are 12 parts), the obtained performance test result is as follows: the density is 1.381g/cm²The normal temperature warping degree is 0.15mm, and the diameter of the foam hole is 155 mu m.

(3) When the content of the heavy calcium carbonate in the composite calcium is 60% and the content of the light calcium carbonate in the composite calcium is 40% (the weight parts of the heavy calcium carbonate are 24 parts and the weight parts of the light calcium carbonate are 16 parts), the obtained performance test result is as follows: the density is 1.380g/cm²The normal temperature warping degree is 0.28mm, and the diameter of the foam hole is 150 mu m.

Experimental data show that under the condition that the components of the first structural layer 110 and the third structural layer 130 are the same and the other components of the second structural layer 120 are the same, when the light calcium carbonate and the heavy calcium carbonate in the composite calcium of the second structural layer 120 are respectively set to be 8 parts by mass and 32 parts by weight or the content of the heavy calcium carbonate is 80% and the content of the light calcium carbonate is 20%, the material has better normal-temperature warping resistance. These experimental data of calcium complex of second structural layer 120 may be the basis of the related examples.

EXAMPLE five

The content of the ground limestone and the hollow glass beads in the inorganic filler in the first structural layer 110 or the third structural layer 130 is selected differently, and different influences are caused on the performance detection result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the composition in second structural layer 120 was set as: 120 parts by weight of polyvinyl chloride, 120 parts by weight of modified fly ash, 20 parts by weight of composite calcium (the content of heavy calcium carbonate is 70%, and the content of light calcium carbonate is 30%), 10 parts by weight of hollow glass beads, 1.0 part by weight of polyethylene wax, 6.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of a yellow foaming agent (azodicarbonamide), 1.2 parts by weight of a white foaming agent (sodium bicarbonate), and 15 parts by weight of a foaming regulator (ethyl acrylate).

The composition of the first structural layer 110 and the third structural layer 130 are set to: 90 parts by weight of polyvinyl chloride, 330 parts by weight of inorganic filler, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 15 parts by weight of plasticizer (dibutyl phthalate), 0.4 part by weight of carbon black. Wherein, 330 parts by weight of the inorganic filler contains heavy calcium carbonate and hollow glass beads in different parts by weight.

The test results include the performance of the composite stone floor in terms of density (ISO23996), normal temperature warpage (ISO23999), thermal deformation Vicat temperature, static bending strength (GB/T17657), elongation at break displacement and heating dimensional change rate (ISO 23999).

Wherein, the normal temperature warping degree refers to the degree of object distortion when the object is at 23 +/-2 ℃.

The heat distortion vicat temperature is understood here to be the temperature measured by a heat distortion vicat temperature measuring instrument.

The static bending strength is a ratio of a bending moment and a bending section modulus at the time of maximum load application of a test piece. For example, the compressive strength that the first structural layer 110 or the third structural layer 130 can withstand when it is bent under a force until it breaks is expressed in Mpa.

The heating dimension change rate is how much the dimension of the object changes when the object is restored to 23 ± 2 ℃ after being heated at 80 ℃ for 6 hours.

The elongation at break displacement is the amount of displacement that an object undergoes when it is crushed.

The test results were as follows:

(1) when the heavy calcium carbonate is set to 312 parts by weight and the hollow glass beads are set to 18 parts by weight, the obtained performance test result is as follows: density ofIs 1.312g/cm²The normal temperature warping degree is 0.30mm, the thermal deformation Vicat is 65 ℃, the static bending strength is 33MPa, the elongation at break displacement is 10mm, and the heating size change is 0.085%.

(2) When the heavy calcium carbonate is set to 330 parts by weight and the hollow glass beads are set to 0 part by weight, the obtained performance test result is as follows: the density was 1.350g/cm²The normal temperature warping degree is 0.50mm, the thermal deformation Vicat is 55 ℃, the static bending strength is 27MPa, the elongation at break displacement is 11mm, and the heating size change is 0.10%.

(3) When the weight of the heavy calcium carbonate is set to 295 parts by weight and the weight of the hollow glass beads is set to 35 parts by weight, the obtained performance test result is as follows: the density was 1.290g/cm²The normal temperature warping degree is 0.20mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 38MPa, the elongation at break displacement is 5.5mm, and the heating size change is 0.065%.

(4) When the heavy calcium carbonate is set to 290 parts by weight and the hollow glass beads are set to 40 parts by weight, the obtained performance test result is as follows: the density is 1.285g/cm²The normal temperature warping degree is 0.18mm, the thermal deformation Vicat is 70 ℃, the static bending strength is 37MPa, the elongation at break displacement is 4.5mm, and the heating size change is 0.15%.

The experimental data show that under the condition that the components of the second structure layer 120 are the same, and the other components of the first structure layer 110 and the third structure layer 130 are the same, when the weight ratio of the ground limestone is 295 parts by weight and the content of the hollow glass beads is 35 parts by weight, the material has better normal temperature warping resistance and static bending strength, the heating size change rate is lower, and the performance is better than that of other experimental groups. These experimental data for the inorganic fillers (ground calcium carbonate and hollow glass microspheres) can be used as the basis for the relevant examples.

EXAMPLE six

The content of the ABS resin in the first structural layer 110 and/or the third structural layer 130 is selected differently, which has different effects on the performance test results of the composite stone crystal flooring. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the composition in second structural layer 120 was set as: 120 parts by weight of polyvinyl chloride, 120 parts by weight of modified fly ash, 20 parts by weight of composite calcium (the content of heavy calcium carbonate is 70%, and the content of light calcium carbonate is 30%), 10 parts by weight of hollow glass beads, 1.0 part by weight of polyethylene wax, 6.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 0.9 part by weight of a yellow foaming agent, 1.2 parts by weight of a white foaming agent, and 15 parts by weight of a foaming regulator (ethyl acrylate).

The composition of the first structural layer 110 and the third structural layer 130 are set to: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground calcium carbonate, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of a stabilizer (calcium stearate), 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 15 parts by weight of a plasticizer (dibutyl phthalate), 0.4 part by weight of carbon black, different parts by weight of ABS resin, and the same parts by weight of ABS resin and Acrylates (ACR).

The test results included the performance of the composite stone floor in terms of heat distortion vicat, static flexural strength (GB/T17657) and elongation at break displacement.

The test results were as follows:

(1) when the ABS resin was set to 8 parts by weight, the obtained performance test results were: the heat distortion Vicat is 70 ℃, the static bending strength is 33MPa, and the elongation displacement at break is 10 mm.

(2) When the ABS resin was set to 9 parts by weight, the obtained performance test results were: the thermal deformation Vicat is 70 ℃, the static bending strength is 35MPa, and the elongation displacement at break is 10.3 mm.

(3) When the ABS resin was set to 10 parts by weight, the obtained performance test results were: the Vicat of thermal deformation is 70 ℃, the static bending strength is 38MPa, and the elongation displacement at break is 10.5 mm.

(4) When the ABS resin was replaced with the Acrylate (ACR), i.e., the Acrylate (ACR) was set to 10 parts by weight, the obtained performance test results were: the Vicat of thermal deformation is 55 ℃, the static bending strength is 28MPa, and the elongation displacement at break is 12 mm.

The experimental data show that under the condition that the components of the second structural layer 120 are the same and the other components of the first structural layer 110 or the third structural layer 130 are the same, the material has better static bending strength and higher thermal deformation vicat temperature when the content of the ABS resin is 8-10 parts by weight. Meanwhile, the performance of the composite stone-crystal floor formed by blending the ABS resin and the polyvinyl chloride is obviously superior to that of the composite stone-crystal floor formed by blending the Acrylate (ACR) and the polyvinyl chloride. These experimental data of the ABS resin can be used as a basis for the relevant examples.

EXAMPLE seven

The selection of the matching content of the inorganic filler and the foaming agent in the second structural layer 120 is different, and different influences are caused on the performance detection result of the composite stone-crystal floor. Specifically, the specific influence on the performance test result can be embodied by the following set of experiments.

In this set of experiments, the compositions in the first structural layer 110 and the third structural layer 130 were set as: 90 parts by weight of polyvinyl chloride, 312 parts by weight of ground limestone, 18 parts by weight of hollow glass microspheres, 0.4 part by weight of polyethylene wax, 3.0 parts by weight of stabilizer, 0.4 part by weight of stearic acid, 0.1 part by weight of oxidized polyethylene wax, 8 parts by weight of ABS resin, 0.4 part by weight of carbon black and 15 parts by weight of plasticizer.

The components in second structural layer 120 are set as: 100 parts by weight of polyvinyl chloride, 1.0 part by weight of polyethylene wax, 8.0 parts by weight of a stabilizer (calcium stearate), 1.1 parts by weight of stearic acid, 15 parts by weight of a foaming regulator (ethyl acrylate), and various parts by weight of inorganic fillers and foaming agents.

The test results included the performance of the composite stone floor in terms of density (ISO23996) and cell diameter.

(1) When the inorganic filler is 100 parts by weight, the modified fly ash is set to be 50 parts by weight, the composite calcium (the heavy calcium carbonate content is 70%, and the light calcium carbonate content is 30%) is 40 parts by weight, the hollow glass beads are 10 parts by weight, and the foaming agent is 1.8 parts by weight (the yellow foaming agent is 0.6 part by weight, and the white foaming agent is 1.2 parts by weight), the obtained performance test result is as follows: the density is 1.450g/cm²The cell diameter was 140. mu.m.

(2) When inorganic fillerThe weight portion is 150, wherein when the modified fly ash is set as 100 weight portions, the composite calcium (the content of heavy calcium carbonate is 70%, the content of light calcium carbonate is 30%) is 40 weight portions, the hollow glass beads are 10 weight portions, and the foaming agent is 1.95 weight portions (the yellow foaming agent is 0.75 weight portion, and the white foaming agent is 1.2 weight portions), the obtained performance test result is as follows: the density was 1.430g/cm²The cell diameter was 145. mu.m.

(3) When the inorganic filler weight portion is 200, wherein the modified fly ash is set as 150 weight portions, the composite calcium (the heavy calcium carbonate content is 70%, the light calcium carbonate content is 30%) is 40 weight portions, the hollow glass bead is 10 weight portions, and the foaming agent weight portion is 2.1 (the yellow foaming agent is 0.9 weight portion, and the white foaming agent is 1.2 weight portions), the obtained performance test result is: the density is 1.380g/cm²The cell diameter was 150. mu.m.

(4) When the inorganic filler is 200 parts by weight, wherein the modified fly ash is set to be 200 parts by weight, the composite calcium is 0 part by weight, the hollow glass beads are 0 part by weight, and the foaming agent is 2.0 parts by weight (the yellow foaming agent is 0.9 part by weight, and the white foaming agent is 1.1 part by weight), the obtained performance test result is as follows: the density was 1.392g/cm²The cell diameter was 149 μm.

(5) When the weight part of the inorganic filler is 200, wherein the weight parts of the modified fly ash are set to 200, the composite calcium is 0, the hollow glass beads are 0, and the weight parts of the foaming agent is 1.9 (the weight parts of the yellow foaming agent is 0.9, and the weight parts of the white foaming agent is 1.0), the obtained performance test result is as follows: the density was 1.425g/cm²The cell diameter was 149 μm.

(6) When the weight part of the inorganic filler is 300, wherein the weight parts of the modified fly ash are 300, the composite calcium is 0, the hollow glass beads are 0, and the weight parts of the foaming agent are 2.0 (the weight parts of the yellow foaming agent is 0.9, and the weight parts of the white foaming agent is 1.1), the second structural layer is not foamed, which indicates that the amount of the foaming agent is not enough to play a foaming role.

(7) When the weight part of the inorganic filler is 200, wherein the weight parts of the modified fly ash are 200, the composite calcium is 0, the hollow glass beads are 0, and the weight part of the foaming agent is 3.0 (the weight parts of the yellow foaming agent is 1.9, and the weight parts of the white foaming agent is 1.1), bubbles are formed and gas escapes in the foaming process, which indicates that the second structural layer with a better structure cannot be obtained due to too much consumption of the foaming agent.

Experimental data indicate that the amount of inorganic filler in second structural layer 120 needs to be matched to the amount of blowing agent in the case where first structural layer 110 and third structural layer 130 are the same composition and the other components of second structural layer 120 are the same. If the amount of the foaming agent is insufficient, the second structural layer 120 may not be foamed. If the amount of the foaming agent is too large, the foam collapse and gas escape in the foaming process can be caused, and a second structural layer with a better structure cannot be obtained.

The modified fly ash content of second structural layer 120 affects density and cell diameter. For example, when the contents of the composite calcium, the hollow glass beads and the white foaming agent are controlled for a certain time, the amount of the yellow foaming agent needs to be increased while the amount of the modified fly ash is increased. For example, when the content of the modified fly ash is controlled, the density of the resulting stone-crystal flooring decreases as the parts by mass of the yellow foaming agent and the white foaming agent increase. These experimental data of the contents of inorganic filler and blowing agent can be taken as the basis for the relevant examples.

The beneficial effects that may be brought by the embodiments of the present description may also include but are not limited to: (1) the first structural layer and/or the third structural layer comprise hollow glass beads and heavy calcium carbonate, so that the thermal stability and rigidity of the composite stone-crystal floor can be improved, and the composite stone-crystal floor has better creep resistance; (2) the second structure layer comprises modified fly ash, hollow glass beads and composite calcium, so that the density of the composite stone-crystal floor can be reduced, and the thermal stability of the composite stone-crystal floor is improved; (3) the preparation device adopts the heat-conducting oil sizing sleeve to be matched with the cooling roller group and the calender roller group, so that the bubble holes can be prevented from being broken, the co-extruded substrate surface is not subjected to temperature loss while the substrate is sized, one-time thermal composite pressing forming can be realized, the composite stone-crystal floor is more convenient to process, and the production cost is further reduced.

It is to be noted that different embodiments may produce different advantages, and in different embodiments, the advantages that may be produced may be any one or combination of the above, or any other advantages that may be obtained.

Having thus described the basic concept, it will be apparent to those skilled in the art that the foregoing detailed disclosure is to be regarded as illustrative only and not as limiting the present specification. Various modifications, improvements and adaptations to the present description may occur to those skilled in the art, although not explicitly described herein. Such modifications, improvements and adaptations are proposed in the present specification and thus fall within the spirit and scope of the exemplary embodiments of the present specification.

Also, the description uses specific words to describe embodiments of the description. Reference throughout this specification to "one embodiment," "an embodiment," and/or "some embodiments" means that a particular feature, structure, or characteristic described in connection with at least one embodiment of the specification is included. Therefore, it is emphasized and should be appreciated that two or more references to "an embodiment" or "one embodiment" or "an alternative embodiment" in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, some features, structures, or characteristics of one or more embodiments of the specification may be combined as appropriate.

Additionally, the order in which the elements and sequences of the process are recited in the specification, the use of alphanumeric characters, or other designations, is not intended to limit the order in which the processes and methods of the specification occur, unless otherwise specified in the claims. While various presently contemplated embodiments of the invention have been discussed in the foregoing disclosure by way of example, it is to be understood that such detail is solely for that purpose and that the appended claims are not limited to the disclosed embodiments, but, on the contrary, are intended to cover all modifications and equivalent arrangements that are within the spirit and scope of the embodiments herein. For example, although the system components described above may be implemented by hardware devices, they may also be implemented by software-only solutions, such as installing the described system on an existing server or mobile device.

Similarly, it should be noted that in the preceding description of embodiments of the present specification, various features are sometimes grouped together in a single embodiment, figure, or description thereof for the purpose of streamlining the disclosure aiding in the understanding of one or more of the embodiments. This method of disclosure, however, is not intended to imply that more features than are expressly recited in a claim. Indeed, the embodiments may be characterized as having less than all of the features of a single embodiment disclosed above.

Numerals describing the number of components, attributes, etc. are used in some embodiments, it being understood that such numerals used in the description of the embodiments are modified in some instances by the use of the modifier "about", "approximately" or "substantially". Unless otherwise indicated, "about", "approximately" or "substantially" indicates that the number allows a variation of ± 20%. Accordingly, in some embodiments, the numerical parameters used in the specification and claims are approximations that may vary depending upon the desired properties of the individual embodiments. In some embodiments, the numerical parameter should take into account the specified significant digits and employ a general digit preserving approach. Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the range are approximations, in the specific examples, such numerical values are set forth as precisely as possible within the scope of the application.

For each patent, patent application publication, and other material, such as articles, books, specifications, publications, documents, etc., cited in this specification, the entire contents of each are hereby incorporated by reference into this specification. Except where the application history document does not conform to or conflict with the contents of the present specification, it is to be understood that the application history document, as used herein in the present specification or appended claims, is intended to define the broadest scope of the present specification (whether presently or later in the specification) rather than the broadest scope of the present specification. It is to be understood that the descriptions, definitions and/or uses of terms in the accompanying materials of this specification shall control if they are inconsistent or contrary to the descriptions and/or uses of terms in this specification.

Finally, it should be understood that the embodiments described herein are merely illustrative of the principles of the embodiments of the present disclosure. Other variations are also possible within the scope of the present description. Thus, by way of example, and not limitation, alternative configurations of the embodiments of the specification can be considered consistent with the teachings of the specification. Accordingly, the embodiments of the present description are not limited to only those embodiments explicitly described and depicted herein.

Claims (7)

1. A composite stone crystal floor is provided with a multilayer structure, and is characterized by comprising: the structure comprises a co-extrusion foaming base material layer (100), wherein the co-extrusion foaming base material layer (100) at least comprises a first structure layer (110), a second structure layer (120) and a third structure layer (130); wherein the content of the first and second substances,

the second structural layer (120) is a foamed layer, the first structural layer (110) and the third structural layer (130) are layers of thermally stable material;

the second structural layer (120) is located intermediate the first structural layer (110) and the third structural layer (130), and the second structural layer (120) has a foamed density of less than 1.1g/cm³。

2. The composite stone grain flooring of claim 1, wherein the first structural layer (110) and the third structural layer (130) deform less than 0.065% when the temperature change is less than 80 ℃.

3. The composite stone crystal floor as claimed in claim 1, characterized in that the composite stone crystal floor further comprises a decorative layer (200) arranged on the co-extruded foamed substrate layer (100).

4. The composite stone grain flooring of claim 3, wherein the decorative layer (200) comprises at least one of a UV coating (210), a wear layer (220), or a color film layer (230).

5. The composite stone grain flooring as recited in claim 3, characterized in that the decorative layer (200) comprises at least one of a wood veneer, a bamboo veneer or a melamine paper.

6. The composite stone grain flooring as recited in claim 1, further comprising a backing layer; the back cushion layer is arranged below the co-extrusion foaming base material layer (100).

7. The composite stone grain flooring of claim 6 wherein the backing layer comprises at least one of a cork mat, IXPE mute mat, EVA mute mat or rubber mute mat.

Images