Natural stone facing composite laminate

Claim 2

A composite laminate comprising a polymeric sheet-like core having a pair of surfaces, a pair of metal foils uniformly bonded to said pair of surfaces of said polymeric sheet-like core so as to form a sandwich-type structure and a lamina comprising 70 to 80% of a natural facing stone and 20 to 30% of a matrix material uniformly bonded to at least one of said pair of metal foils.

Claim 3

A composite laminate according to claim 1 wherein the thickness of said polymeric sheet-like core is between 0.118 to 0.197 inches.

Claim 4

A composite laminate according to claim 2 wherein the thickness of each of said metal foils is between 0.019 to 0.020 inches.

Claim 5

A composite laminate according to claim 3 wherein the thickness of said lamina of natural facing stone is between 0.125 to 0.187 inches.

Claim 6

A composite laminate according to claim 4 wherein the ratio of the thickness of lamina of natural facing stone to the total thickness of said pair of metal foils is between 3:1 to 3.5:1.

Claim 7

A composite laminate according to claim 5 wherein the ratio of the thickness of lamina of natural facing stone to the thickness of said sandwich-type structure is between 1:1.2 to 1:1.4.

Claim 8

A composite laminate according to claim 5 wherein the ratio of the thickness of said polymeric sheet-like core to the thickness of each of said metal foils is between 6:1 to 8:1.

Claim 9

A composite laminate according to claim 7 wherein the ratio of the thickness of lamina of natural facing stone to the thickness of said sandwich-type structure is between 1:1.2 to 1:1.4.

Claim 10

A process for manufacturing a composite laminate comprising a polymeric sheet-like core having a pair of surfaces, a pair of metal foils uniformly bonded to said pair of surfaces of said polymeric sheet-like core so as to form a sandwich-type structure and a lamina of natural facing stone uniformly bonded to at least one of said pair of metal foils, comprising the steps of: (a) forming said sandwich-type structure by bonding said pair of metal foils to said pair of surfaces of said po1ymeric sheet-like core; (b) roughening the exposed surface of at least one of said pair of metal foils so as to remove any metal oxide coating and increase bonding area; (c) preparing a slurry comprising 70 to 80% natural facing stone and 20 to 30% of a matrix material selected from the group consisting of polyester, epoxy and or acrylics; (d) pouring and smoothing said slurry on said exposed surface of said at least one of said pair of metal foils; and (e) curing said poured and smoothed matrix in air so as to set same.

Claim 11

A process for manufacturing a composite laminate comprising a polymeric sheet-like core having a pair of surfaces, a pair of metal foils uniformly bonded to said pair of surfaces of said polymeric sheet-like core so as to form a sandwich-type structure and a lamina of natural facing stone uniformly bonded to at least one of said pair of metal foils, comprising the steps of: (a) forming said sandwich-type structure by bonding said pair of metal foils to said pair of surfaces of said po1ymeric sheet-like core; (b) roughening the exposed surface of at least one of said pair of metal foils so as to remove any metal oxide coating and increase bonding area; (c) preparing a slurry comprising 70 to 80% natural facing stone and 20 to 30% of a matrix material selected from the group consisting of polyester, epoxy and or acrylics; (d) pouring and smoothing said slurry on said exposed surface of said at least one of said pair of metal foils; and (e) curing said poured and smoothed matrix in air so as to set same.

Claim 12

A process according to claim 9 including the steps of priming said exposed surface of said at least one of said pairs of metal foils with an acrylic primer to a thickness of between 0.0005 to 0.0015 inches prior to pouring and smoothing said slurry.

Claim 13

A process according to claim 9 including the steps of pouring and smoothing said slurry in a reduced pressure environment of less than 3/4 atmospheric pressure.

Claim 14

A process according to claim 11 including the steps of curing said matrix in air at a temperature of between 60° to 75° F. at a humidity of between 40% to 60% for between 18 to 24 hours.

Claim 15

A composite laminate according to claim 1 wherein said matrix material is selected from the group consisting of polyester, epoxy, acrylics or mixtures thereof.