Method and Apparatus of Forming Cracks as Masks for the Fabrication of Micro-Metal Mesh
Abstract
Methods and systems for forming cracks as masks for the fabrication of micro-metal mesh are disclosed, including depositing a composite film onto a substrate wherein the composite film comprises a brittle layer, a brittle layer atop a mediate layer, or a brittle layer atop a sacrificial layer; generating a tensile stress in the substrate and/or the composite film in order to form micro-cracks in the brittle layer; tuning widths of the micro-cracks; transferring pattern of the micro-cracks onto the sacrificial layer; depositing a conductive material onto the brittle layer and the area of the substrate or mediate layer exposed by the pattern of the micro-cracks; and performing a lift-off of the brittle layer and if present the sacrificial layer from the substrate or mediate layer, resulting in the micro-metal mesh atop the substrate or mediate layer. Other embodiments are described and claimed.
Claims
exact text as granted — not AI-modified1 . A method for fabricating a micro-metal mesh, the method comprising:
depositing a mediate layer onto a substrate; depositing a brittle layer onto the mediate layer; generating a tensile stress in the substrate, the mediate layer, and/or the brittle layer in order to form micro-cracks in the brittle layer; tuning widths of the micro-cracks; depositing a conductive material onto the brittle layer and the area of the mediate layer exposed by the pattern of the micro-cracks; and performing a lift-off of the brittle layer from the mediate layer, resulting in the micro-metal mesh atop the mediate layer.
2 . The method of claim 1 , wherein tuning the widths of the micro-cracks comprises etching the brittle layer or annealing the substrate, the mediate layer, and the brittle layer.
3 . The method of claim 2 , wherein the annealing comprises a temperature ranging from about 40° C. to about 180° C.
4 . The method of claim 2 , wherein the annealing comprises a time ranging from about 10 seconds to about 1 hour.
5 . The method of claim 1 , wherein the substrate comprises a transparent and flexible film having a material selected from the group consisting of polyethylene terephthalate, polyimide, cellulose, polyester, polyethylene, polyolefin, polycarbonate, glass, or a combination or lamination thereof.
6 . The method of claim 1 , wherein the brittle layer comprises spin-on-glass, liquid glass, ceramic, salt, carbon, and/or PMMA.
7 . The method of claim 1 , wherein the mediate layer comprises a material selected from the group consisting of PMMA, PS, PVC, rubber, silicone, PDMS, nylon, or a combination thereof.
8 . The method of claim 1 , wherein the conductive material comprises a metal, alloy, and/or doped semiconductor having a material selected from the group consisting of silver, copper, gold, iron, nickel, cobalt, platinum, palladium, titanium, aluminum, chromium, molybdenum, or a combination thereof.
9 . The method of claim 1 , wherein the micro-cracks comprise a width ranging from about 20 nm to about 5 μm.
10 . The method of claim 1 , wherein generating a tensile stress comprises mechanical bending, stretching, squeezing, pressing, thermal shock, quenching, and/or adding nanoparticles in the brittle layer.
11 . The method of claim 10 , wherein the nanoparticles comprise silver, copper, gold, iron, nickel, cobalt, platinum, palladium, titanium, aluminum, chromium, and/or molybdenum.
12 . The method of claim 1 , wherein the method is roll-to-roll compatible.
13 . A method for fabricating a micro-metal mesh, the method comprising:
depositing a sacrificial layer onto a substrate; depositing a brittle layer onto the sacrificial layer; generating a tensile stress in the substrate, the sacrificial layer, and/or the brittle layer in order to form micro-cracks in the brittle layer; tuning widths of the micro-cracks; transferring pattern of the micro-cracks onto the sacrificial layer; depositing a conductive material onto the brittle layer and the area of the substrate exposed by the pattern of the micro-cracks transferred onto the sacrificial layer; and performing a lift-off of the sacrificial layer and the brittle layer from the substrate, resulting in the micro-metal mesh atop the substrate.
14 . The method of claim 13 , wherein tuning the widths of the micro-cracks comprises etching the brittle layer or annealing the substrate, the sacrificial layer, and the brittle layer.
15 . The method of claim 14 , wherein the annealing comprises a temperature ranging from about 40° C. to about 180° C.
16 . The method of claim 14 , wherein the annealing comprises a time ranging from about 10 seconds to about 1 hour.
17 . The method of claim 13 , wherein transferring the pattern of the micro-cracks onto the sacrificial layer comprises dissolving and/or reaction ion etching the sacrificial layer exposed by the pattern of the micro-cracks in the brittle layer.
18 . The method of claim 13 , wherein the substrate comprises a transparent and flexible film having a material selected from the group consisting of polyethylene terephthalate, polyimide, cellulose, polyester, polyethylene, polyolefin, polycarbonate, glass, or a combination or lamination thereof.
19 . The method of claim 13 , wherein the brittle layer comprises spin-on-glass, liquid glass, ceramic, salt, carbon, and/or PMMA.
20 . The method of claim 13 , wherein the sacrificial layer comprises a polymer selected from the group consisting of PMMA, PS, PVC, rubber, silicone, PDMS, nylon, and photo resist.
21 . The method of claim 13 , wherein the conductive material comprises a metal, alloy, and/or doped semiconductor having a material selected from the group consisting of silver, copper, gold, iron, nickel, cobalt, platinum, palladium, titanium, aluminum, chromium, molybdenum, or a combination thereof.
22 . The method of claim 13 , wherein the micro-cracks comprise a width ranging from about 20 nm to about 5 μm.
23 . The method of claim 13 , wherein generating a tensile stress comprises mechanical bending, stretching, squeezing, pressing, thermal shock, quenching, and/or adding nanoparticles in the brittle layer.
24 . The method of claim 23 , wherein the nanoparticles comprise silver, copper, gold, iron, nickel, cobalt, platinum, palladium, titanium, aluminum, chromium, and/or molybdenum.
25 . The method of claim 13 , wherein the method is roll-to-roll compatible.
26 . An apparatus for forming micro-cracks in a brittle layer, the apparatus comprising:
a roller having a diameter; the apparatus configured to:
drive a composite film around the roller to generate a tensile stress in the composite film, wherein the composite film comprises the brittle layer atop a substrate; and
form cracks in the brittle layer, wherein the cracks are parallel to the axis of the roller and have a period dependent on the diameter of the roller.
27 . The apparatus of claim 26 , wherein the composite film further comprises a mediate layer or a sacrificial layer between the brittle layer and the substrate.
28 . The apparatus of claim 26 , wherein the roller the diameter ranges from about 1.6 mm to about 30 mm.Join the waitlist — get patent alerts
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