Patents Assigned to GKN Aerospace Transparency Systems, Inc.
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Patent number: 11649375Abstract: A polyurethane composition suitable for coating a surface of a substrate. The polyurethane composition can include an aliphatic polyester urethane matrix and a fluorinated ionic antistatic additive. The aliphatic polyester urethane matrix can comprise an aliphatic diisocyanate, a polyester polyol having a polyester diol and a polyester triol, and sulfonated polyester urethane polyol.Type: GrantFiled: September 10, 2021Date of Patent: May 16, 2023Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
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Publication number: 20220098436Abstract: A polyurethane composition suitable for coating a surface of a substrate. The polyurethane composition can include an aliphatic polyester urethane matrix and a fluorinated ionic antistatic additive. The aliphatic polyester urethane matrix can comprise an aliphatic diisocyanate, a polyester polyol having a polyester diol and a polyester triol, and sulfonated polyester urethane polyol.Type: ApplicationFiled: September 10, 2021Publication date: March 31, 2022Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
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Patent number: 11118086Abstract: A polyurethane composition suitable for coating a surface of a substrate. The polyurethane composition can include an aliphatic polyester urethane matrix and a fluorinated ionic antistatic additive. The aliphatic polyester urethane matrix can comprise an aliphatic diisocyanate, a polyester polyol having a polyester diol and a polyester triol, and sulfonated polyester urethane polyol.Type: GrantFiled: November 22, 2017Date of Patent: September 14, 2021Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
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Patent number: 11053163Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a substrate. The method includes applying a coating composition to the surface and heating the coated surface at a cure temperature from about 300° C. to about 600° C. for a time from about 2 hours to about 48 hours. The coating composition is applied to the surface by an application method selected from the group consisting of flowing, dipping, and spraying. The coating composition comprises a yttrium compound, an additive selected from the group consisting of a cerium compound and a dispersion of yttrium oxide nanoparticles, a water-soluble polymer, and a solvent solution of de-ionized water and a water-soluble alcohol.Type: GrantFiled: December 30, 2019Date of Patent: July 6, 2021Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Christopher Rankin
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Publication number: 20200255328Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a substrate. The method includes applying a coating composition to the surface and heating the coated surface at a cure temperature from about 300° C. to about 600° C. for a time from about 2 hours to about 48 hours. The coating composition is applied to the surface by an application method selected from the group consisting of flowing, dipping, and spraying. The coating composition comprises a yttrium compound, an additive selected from the group consisting of a cerium compound and a dispersion of yttrium oxide nanoparticles, a water-soluble polymer, and a solvent solution of de-ionized water and a water-soluble alcohol.Type: ApplicationFiled: December 30, 2019Publication date: August 13, 2020Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Christopher Rankin
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Publication number: 20200224316Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a metallic substrate. The method can include anodizing a nanoporous layer of anodic metal oxide on the surface; cathodizing yttrium oxide nanoparticles onto the surface; applying a hydrophobic ceramic coating composition to the surface by an application method selected from the group consisting of: flowing, dipping, and spraying; and heating the coated surface at a cure temperature from about 150° C. to about 300° C. for at least 2 hours.Type: ApplicationFiled: January 13, 2020Publication date: July 16, 2020Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Christopher Rankin, Marlowe Moncur
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Patent number: 10533256Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a metallic substrate. The method can include anodizing a nanoporous layer of anodic metal oxide on the surface; cathodizing yttrium oxide nanoparticles onto the surface; applying a hydrophobic ceramic coating composition to the surface by an application method selected from the group consisting of: flowing, dipping, and spraying; and heating the coated surface at a cure temperature from about 150° C. to about 300° C. for at least 2 hours.Type: GrantFiled: October 9, 2017Date of Patent: January 14, 2020Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Christopher Rankin, Marlowe Moncur
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Patent number: 10519063Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a substrate. The method includes applying a coating composition to the surface and heating the coated surface at a cure temperature from about 300° C. to about 600° C. for a time from about 2 hours to about 48 hours. The coating composition is applied to the surface by an application method selected from the group consisting of flowing, dipping, and spraying. The coating composition comprises a yttrium compound, an additive selected from the group consisting of a cerium compound and a dispersion of yttrium oxide nanoparticles, a water-soluble polymer, and a solvent solution of de-ionized water and a water-soluble alcohol.Type: GrantFiled: August 18, 2017Date of Patent: December 31, 2019Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Christopher Rankin
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Publication number: 20190153259Abstract: A polyurethane composition suitable for coating a surface of a substrate. The polyurethane composition can include an aliphatic polyester urethane matrix and a fluorinated ionic antistatic additive. The aliphatic polyester urethane matrix can comprise an aliphatic diisocyanate, a polyester polyol having a polyester diol and a polyester triol, and sulfonated polyester urethane polyol.Type: ApplicationFiled: November 22, 2017Publication date: May 23, 2019Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
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Publication number: 20190106794Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a metallic substrate. The method can include anodizing a nanoporous layer of anodic metal oxide on the surface; cathodizing yttrium oxide nanoparticles onto the surface; applying a hydrophobic ceramic coating composition to the surface by an application method selected from the group consisting of: flowing, dipping, and spraying; and heating the coated surface at a cure temperature from about 150° C. to about 300° C. for at least 2 hours.Type: ApplicationFiled: October 9, 2017Publication date: April 11, 2019Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Christopher Rankin, Marlowe Moncur
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Patent number: 10059623Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a substrate. The method includes applying a coating composition to the surface and heating the coated surface at a cure temperature from about 450° C. to about 600° C. for a time from about 8 hours to about 48 hours. The coating composition is applied to the surface by an application method selected from the group consisting of flowing, dipping, and spraying. The coating composition comprises a yttrium compound, an additive selected from the group consisting of a cerium compound and a dispersion of yttrium oxide nanoparticles, a water-soluble polymer, and a solvent solution of de-ionized water and a water-soluble alcohol.Type: GrantFiled: August 19, 2016Date of Patent: August 28, 2018Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Christopher Rankin
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Publication number: 20180050957Abstract: A hydrophobic coating and a method for applying such a coating to a surface of a substrate. The method includes applying a coating composition to the surface and heating the coated surface at a cure temperature from about 300° C. to about 600° C. for a time from about 2 hours to about 48 hours. The coating composition is applied to the surface by an application method selected from the group consisting of flowing, dipping, and spraying. The coating composition comprises a yttrium compound, an additive selected from the group consisting of a cerium compound and a dispersion of yttrium oxide nanoparticles, a water-soluble polymer, and a solvent solution of de-ionized water and a water-soluble alcohol.Type: ApplicationFiled: August 18, 2017Publication date: February 22, 2018Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Christopher Rankin
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Patent number: 9580564Abstract: The present invention is embodied in a transparent, polyurethane laminate or multi-layer coating comprising a first transparent polyurethane layer, a middle conductive material layer disposed on the first transparent polyurethane layer, and a second transparent polyurethane layer disposed on the conductive layer. In one embodiment, the subject invention addresses the problem of static charge buildup on aircraft transparencies by allowing charge to drain through the second transparent polyurethane layer to the conductive material layer and then to the edge of the conductive material layer, where it is mated to the airframe. The present invention is also embodied in a method for forming a transparent polyurethane laminate on a transparent substrate and a method for forming a free-standing laminate.Type: GrantFiled: July 22, 2010Date of Patent: February 28, 2017Assignee: GKN Aerospace Transparency Systems, Inc.Inventors: Marlowe Moncur, Lin Hoo, Stephen Sandlin
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Publication number: 20130313366Abstract: A low drag passenger-cabin window for use on an aircraft fuselage having a generally cylindrical shape, in which the as-manufactured geometry of the window is modified so that the shape of the window at cruise altitudes is aerodynamically optimized. The window comprises a pane of transparent material. The inner and outer surfaces of the peripheral portion of the pane as manufactured conform to a generally cylindrical shape, while the inner and outer surfaces of the medial portion of the pane as manufactured are depressed inwardly in a prescribed manner relative to the peripheral portion. The surfaces of the medial portion are adapted to deflect outwardly to conform to a generally cylindrical shape in response to a predetermined air pressure differential and/or a predetermined temperature gradient experienced at cruise altitude.Type: ApplicationFiled: May 24, 2013Publication date: November 28, 2013Applicant: GKN Aerospace Transparency Systems Inc.Inventors: Thomas S. Hoffa, Kelvin B. Hsieh
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Publication number: 20120021209Abstract: The present invention is embodied in a transparent, polyurethane laminate or multi-layer coating comprising a first transparent polyurethane layer, a middle conductive material layer disposed on the first transparent polyurethane layer, and a second transparent polyurethane layer disposed on the conductive layer. In one embodiment, the subject invention addresses the problem of static charge buildup on aircraft transparencies by allowing charge to drain through the second transparent polyurethane layer to the conductive material layer and then to the edge of the conductive material layer, where it is mated to the airframe. The present invention is also embodied in a method for forming a transparent polyurethane laminate on a transparent substrate and a method for forming a free-standing laminate.Type: ApplicationFiled: July 22, 2010Publication date: January 26, 2012Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: MARLOWE MONCUR, Lin Hoo, Stephen Sandlin
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Publication number: 20110072961Abstract: The present invention is embodied in environmental seal technology incorporated into a double-paned window, the environmental seal technology comprising an inner desiccant seal and a structural spacer. The subject invention solves the problem of moisture between the window panes by keeping the internal gap dry using a desiccant system. The invention also incorporates a durable structural spacer that will not rupture under normal military vehicle loads and environmental conditions. The spacer is bonded to the window panes using pressure-sensitive adhesives, thus allowing for easy manufacture.Type: ApplicationFiled: November 20, 2008Publication date: March 31, 2011Applicant: GKN Aerospace Transparency Systems, Inc.Inventors: David Jungkuist, Marlowe Moncur