Patents Assigned to GKN Aerospace Transparency Systems, Inc.
  • Patent number: 11649375
    Abstract: 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: Grant
    Filed: September 10, 2021
    Date of Patent: May 16, 2023
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
  • Publication number: 20220098436
    Abstract: 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: Application
    Filed: September 10, 2021
    Publication date: March 31, 2022
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
  • Patent number: 11118086
    Abstract: 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: Grant
    Filed: November 22, 2017
    Date of Patent: September 14, 2021
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
  • Patent number: 11053163
    Abstract: 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: Grant
    Filed: December 30, 2019
    Date of Patent: July 6, 2021
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Christopher Rankin
  • Publication number: 20200255328
    Abstract: 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: Application
    Filed: December 30, 2019
    Publication date: August 13, 2020
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Christopher Rankin
  • Publication number: 20200224316
    Abstract: 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: Application
    Filed: January 13, 2020
    Publication date: July 16, 2020
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Christopher Rankin, Marlowe Moncur
  • Patent number: 10533256
    Abstract: 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: Grant
    Filed: October 9, 2017
    Date of Patent: January 14, 2020
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Christopher Rankin, Marlowe Moncur
  • Patent number: 10519063
    Abstract: 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: Grant
    Filed: August 18, 2017
    Date of Patent: December 31, 2019
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Christopher Rankin
  • Publication number: 20190153259
    Abstract: 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: Application
    Filed: November 22, 2017
    Publication date: May 23, 2019
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Jieming Li, Stephen Sandlin, Marlowe Moncur
  • Publication number: 20190106794
    Abstract: 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: Application
    Filed: October 9, 2017
    Publication date: April 11, 2019
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Christopher Rankin, Marlowe Moncur
  • Patent number: 10059623
    Abstract: 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: Grant
    Filed: August 19, 2016
    Date of Patent: August 28, 2018
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Christopher Rankin
  • Publication number: 20180050957
    Abstract: 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: Application
    Filed: August 18, 2017
    Publication date: February 22, 2018
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Christopher Rankin
  • Patent number: 9580564
    Abstract: 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: Grant
    Filed: July 22, 2010
    Date of Patent: February 28, 2017
    Assignee: GKN Aerospace Transparency Systems, Inc.
    Inventors: Marlowe Moncur, Lin Hoo, Stephen Sandlin
  • Publication number: 20130313366
    Abstract: 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: Application
    Filed: May 24, 2013
    Publication date: November 28, 2013
    Applicant: GKN Aerospace Transparency Systems Inc.
    Inventors: Thomas S. Hoffa, Kelvin B. Hsieh
  • Publication number: 20120021209
    Abstract: 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: Application
    Filed: July 22, 2010
    Publication date: January 26, 2012
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: MARLOWE MONCUR, Lin Hoo, Stephen Sandlin
  • Publication number: 20110072961
    Abstract: 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: Application
    Filed: November 20, 2008
    Publication date: March 31, 2011
    Applicant: GKN Aerospace Transparency Systems, Inc.
    Inventors: David Jungkuist, Marlowe Moncur