Coating for environmental protection and indication
A composition for coating a surface comprises an adhesive cementitious material such as a geopolymer, a kaolin, or mixtures thereof, and a filler material. Various filler materials are disclosed, with which the coating composition may be used for thermal mapping, oxygen protection to organic dopants, thermal protection, radiation protection, anti-tamper protection, mechanical abrasion protection, or high emission of electromagnetic radiation. With certain fillers, the coating composition remains thermally stable up to 1200° C., and/or remains thermally operable for brief periods up to about 1400° C. When the coating composition includes a wetting agent, and the filler is between 0.01 micrometer and 10 micrometers in size, the coating composition can take the form of an aqueous spray. With certain fillers, the coating composition can cure at a temperature below 100° C. The coating composition can also be a thick film which provides resistance to cracking and peeling during severe thermal exposure.
1 . A composition for coating a surface, the composition comprising:
an adhesive cementitious material selected from the group consisting of geopolymer, kaolin, and mixtures thereof; and
up to 70% by final volume of a filler material.
2 . The coating composition of claim 1 , wherein said filler material is selected from the group consisting of calcium silicate, titania, zirconia, alumina, silicon carbide, luminophores, carbon and mixtures thereof.
3 . A method of thermal mapping, the method comprising:
applying the coating composition of claim 2 to a surface to form a coated article,
curing said coated article,
allowing the temperature of said surface to change, and
observing changes in the coating composition as said surface changes temperature.
4 . The method of claim 3 , wherein said coating composition further comprises at least one organic dopant, and wherein said adhesive cementitious material is selected to provide environmental stability, thermal stability, or oxidization prevention to said organic dopants.
5 . The coating composition of claim 1 ,
wherein said filler material is selected from the group consisting of titanium, zirconium, aluminum, silicon, iron, copper, nickel, cobalt, silicon, hafnium, oxides thereof, carbides thereof, nitrides thereof and mixtures thereof, and
wherein said coating composition remains thermally operable for brief periods at temperatures up to about 1400° C.
6 . The coating composition of claim 1 , wherein said filler material is selected from the group consisting of silica, alumina, titania, zirconia, glass micro spheres, carbon and mixtures thereof.
7 . A method of providing thermal protection, the method comprising:
applying the coating composition of claim 6 to an article to form a coated article, and
curing said coated article,
thereby providing thermal protection for said coated article.
8 . The coating composition of claim 1 , wherein said filler material is selected from the group consisting of tungsten, titanium, gadolinium, hafnium, lead, boron, oxides thereof, carbides thereof, nitrides thereof, and mixtures thereof.
9 . A method of providing radiation protection to military or medical components, the method comprising:
applying the coating composition of claim 8 to said military or medical components to form a coated article, and
curing said coated article,
thereby providing radiation protection for said coated article.
10 . The coating composition of claim 1 , wherein said filler material is selected from the group consisting of silicon, aluminum, titanium, zirconium, oxides thereof, carbides thereof, nitrides thereof, carbon nanotubes and mixtures thereof.
11 . A method of providing anti-tamper protection, the method comprising:
applying the coating composition of claim 10 to an article to form a coated article, and
curing said coated article,
thereby providing anti-tamper protection for said coated article.
12 . The coating composition of claim 1 , wherein said filler material is selected from the group consisting of calcium silicate, titania, zirconia, alumina, silicon carbide, luminophores, silica, silicates, ceramics, iron, copper, nickel, cobalt, silicon, aluminum, titanium, oxides thereof, carbides thereof, nitrides thereof, and mixtures thereof.
13 . A method of providing mechanical abrasion protection, the method comprising:
applying the coating composition of claim 12 to an article to form a coated article, and
curing said coated article,
thereby providing mechanical abrasion protection for said coated article.
14 . The coating composition of claim 1 , wherein said filler material has high emissivity.
15 . The coating composition of claim 14 , wherein said filler material is selected from the group consisting of calcium silicate, silicon carbide, zirconia, alumina, titania, and mixtures thereof.
16 . A method of providing high emission of electromagnetic radiation, the method comprising:
applying the coating composition of claim 15 to an article to form a coated article, and
curing said coated article,
thereby providing high emission of electromagnetic radiation for said coated article.
17 . The coating composition of claim 1 , wherein the composition is thermally stable up to 1200° C.
18 . The coating composition of claim 1 , said composition further comprising:
no more than 0.5% of a wetting agent by weight, and wherein
said filler is between 0.01 micrometer and 10 micrometers in size, such that
the composition is in the form of an aqueous spray.
19 . A method of curing the coating composition of claim 1 , said method comprising:
depositing the composition on a surface at a thickness of no more than 0.010 inches, and
allowing the composition to cure at ambient temperatures, or at a temperature of no more than 100° C.
20 . The coating composition of claim 1 , wherein said coating composition is a thick film which provides resistance to cracking and peeling during severe thermal exposure.
21 . The coating composition of claim 2 , wherein said coating composition is a thick film which provides resistance to cracking and peeling during severe thermal exposure.
22 . The coating composition of claim 3 , wherein said coating composition is a thick film which provides resistance to cracking and peeling during severe thermal exposure.
23 . The coating composition of claim 5 , wherein said coating composition is a thick film which provides resistance to cracking and peeling during severe thermal exposure.
24 . The coating composition of claim 6 , wherein said coating composition is a thick film which provides resistance to cracking and peeling during severe thermal exposure.