Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
105 words
An article having enhanced insulative properties from repeated thermal gradients and transients consisting essentially of: a substrate selected from the group consisting of aircraft skin, electronic component packages, foams, roadway surfaces, concrete, asphalt, bridge structures, and building materials; a coating covering at least a portion of the surface of said substrate and comprising: a polymeric binder, and a plurality of microcapsules dispersed throughout and submerged within said polymeric binder so as to be surrounded thereby, said microcapsules containing a temperature stabilizing means selected from the group consisting of phase change materials and plastic crystals, whereby the article exhibits enhanced insulation from thermal gradients and transients.
Claim 2
Dependent Claim
105 words
An article having enhanced insulative properties from repeated thermal gradients and transients consisting essentially of: a substrate selected from the group consisting of aircraft skin, electronic component packages, foams, roadway surfaces, concrete, asphalt, bridge structures, and building materials; a coating covering at least a portion of the surface of said substrate and comprising: a polymeric binder, and a plurality of microcapsules dispersed throughout and submerged within said polymeric binder so as to be surrounded thereby, said microcapsules containing a temperature stabilizing means selected from the group consisting of phase change materials and plastic crystals, whereby the article exhibits enhanced insulation from thermal gradients and transients.
Claim 3
Dependent Claim
21 words
An article according to claim 1 wherein said phase change materials comprise a material selected from the group of paraffinic hydrocarbons.
Claim 4
Dependent Claim
34 words
The article according to claim 2 wherein the paraffinic hydrocarbon is selected from the group consisting of n-Octacosane, n-Heptacosane, n-Hexacosane, n-Pentacosane, n-Tetracosane, n-Tricosane, n-Docosane, n-Heneicosane, n-Eicosane, n-Nonadecane, n-Octadecane, h-Heptadecane, n-Hexadecane, n-Pentadecane, n-Tetradecane, and n-Tridecane.
Claim 5
Dependent Claim
22 words
The article according to claim 2 wherein the paraffinic hydrocarbon has a melting point between -5.5 degrees Centigrade and 61.4 degrees Centigrade.
Claim 6
Dependent Claim
18 words
An article according to claim 1 wherein said microcapsules range in diameter from about 0.5 to 1,000 microns.
Claim 7
Dependent Claim
32 words
An article according to claim 1 wherein a first preselected portion of said microcapsules contain a first temperature stabilizing means and the remainder of said microcapsules contain a second temperature stabilizing means.
Claim 8
Dependent Claim
30 words
An article according to claim 1 wherein said polymeric binder is selected from the group consisting of polyurethane, nitrile rubber, chloroprene rubber, polyvinyl alcohol, silicone, ethylene/vinyl acetate copolymer, and acrylic.
Claim 9
Dependent Claim
79 words
An aircraft skin consisting essentially of, in combination: (a) a substantially rigid structural skin substrate; and (b) a polymer directly coating and covering at least a portion of said structural skin substrate, a plurality of microcapsules dispersed throughout said polymer so as to be covered and surrounded thereby, said microcapsules containing a temperature stabilizing means selected from the group consisting of phase change materials and plastic crystals, whereby the aircraft skin exhibits enhanced insulation from thermal gradients and transients.
Claim 10
Dependent Claim
79 words
An aircraft skin consisting essentially of, in combination: (a) a substantially rigid structural skin substrate; and (b) a polymer directly coating and covering at least a portion of said structural skin substrate, a plurality of microcapsules dispersed throughout said polymer so as to be covered and surrounded thereby, said microcapsules containing a temperature stabilizing means selected from the group consisting of phase change materials and plastic crystals, whereby the aircraft skin exhibits enhanced insulation from thermal gradients and transients.