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1.发明申请公开(公告)号：US20160304729A1
公开(公告)日：2016-10-20
申请号：US15187147
申请日：2016-06-20
Applicant: THE BOEING COMPANY
Inventor： Terrell D. Riley , Alexandra E. Corona , Christopher Lamar Broadbent , Shahnaz Shokri , Quynhgiao Nguyen Le
IPC: C09D5/24 , B60R16/06 , B64D45/02 , H01B1/22 , C09D175/04
CPC classification number: C09D5/24 , B05D5/12 , B60R16/06 , B64D45/02 , C08K3/10 , C08K2201/001 , C08K2201/011 , C08L81/08 , C09D175/04 , H01B1/22 , C08L65/00
Abstract: The present disclosure is directed to conductive, translucent water-borne conductive coatings comprising a water-borne lubricant coating base material, an amount of PEDOT:PSS solution, and an amount of metal-containing nanowire, methods for making the same, and articles coated with such coatings.
Abstract translation: 本公开涉及导电的半透明水性导电涂层，其包含水性润滑剂涂层基材，一定量的PEDOT：PSS溶液和一定量的含金属的纳米线，其制备方法和涂覆的制品 与这样的涂层。
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公开(公告)号：US11161334B2
公开(公告)日：2021-11-02
申请号：US16874352
申请日：2020-05-14
Applicant: The Boeing Company
Inventor： Anthony M. Westren , Mark Richard Brei , Thomas G. Lawton , Terrell D. Riley , Caitlin Elizabeth Kerr
IPC: B32B38/00 , B64C1/00 , B44C1/10 , B64F5/40 , B44C1/16 , B41J13/10 , B41J3/407 , B29C70/54 , B32B27/12 , B32B27/34 , B32B27/36 , B32B27/38 , B32B27/40 , B32B37/15 , B41J11/00 , B41M3/12 , B41M5/00 , B29K105/24 , B29C37/00 , B29L31/30
Abstract: Methods for placing an indicia on a composite structure generally include printing the indicia on a first film surface of a coating film, with the coating film being in a partially cured state at the time the printing the indicia is performed, and positioning the coating film on a partially cured composite structure such that a second film surface of the coating film faces and is positioned against a surface of the composite structure, with the second film surface being opposite the first film surface. Finally, the coating film and the composite structure may then be co-cured. Systems for printing an indicia on a composite structure generally include the coating film, a printer configured to print the indicia on the first film surface of the coating film, a securement configured to secure the coating film during printing, and a curing device for co-curing the coating film and the composite structure.
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公开(公告)号：US20240253339A1
公开(公告)日：2024-08-01
申请号：US18160057
申请日：2023-01-26
Applicant: The Boeing Company
Inventor： Kjersta Larson-Smith , Terrell D. Riley , Christopher Garnier , Alexandra E. Corona , Jessica O. Fry , Kevin D. Gordon , Mark R. Brei
CPC classification number: B32B27/40 , B32B7/10 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/38 , B32B37/1018 , B32B38/08 , B32B2038/0076 , B32B2260/021 , B32B2260/046 , B32B2307/71 , B32B2363/00 , B32B2375/00
Abstract: A method of manufacturing a resin-infused part, may include: preparing a laminate by layering a curable protective film onto a fibrous preform; infusing resin into the laminate under a vacuum, such that the resin impregnates the fibrous preform and the protective film adheres to the fibrous preform; and curing the laminate at a curing temperature.
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公开(公告)号：US10668738B1
公开(公告)日：2020-06-02
申请号：US16226045
申请日：2018-12-19
Applicant: The Boeing Company
Inventor： Terrell D. Riley , Alexandra E. Corona , Bennett M. Moriarty , Ryan M. Trumbo , Kjersta L. Larson-Smith , Jill E. Seebergh
Abstract: A method of treating a contoured surface with surface treatment layer includes applying a surface preparation layer along the contoured surface and applying a basecoat layer on top of the surface preparation layer. The method further includes stabilizing the basecoat layer to prepare a basecoat surface along the basecoat layer for one or more subsequent layers of the surface treatment coating and jetting a decorative livery layer along the contoured surface using one or more ink jet print heads. The method further includes applying an adhesion promoter on top of the decorative livery layer and stabilizing the adhesion promoter layer to produce a desired bonding surface along the adhesion promoter layer. Additionally, the method includes applying a clear coat layer to cover the underlying decorative livery layer, the basecoat layer and the surface preparation layer.
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公开(公告)号：US10000644B2
公开(公告)日：2018-06-19
申请号：US15187147
申请日：2016-06-20
Applicant: THE BOEING COMPANY
Inventor： Terrell D. Riley , Alexandra E. Corona , Christopher Lamar Broadbent , Shahnaz Shokri , Quynhgiao Nguyen Le
IPC: H01B1/00 , C09D5/24 , H01B1/22 , B05D5/12 , C09D175/04 , C08K3/10 , C08L81/08 , B60R16/06 , B64D45/02
CPC classification number: C09D5/24 , B05D5/12 , B60R16/06 , B64D45/02 , C08K3/10 , C08K2201/001 , C08K2201/011 , C08L81/08 , C09D175/04 , H01B1/22 , C08L65/00
Abstract: The present disclosure is directed to conductive, translucent water-borne conductive coatings comprising a water-borne lubricant coating base material, an amount of PEDOT:PSS solution, and an amount of metal-containing nanowire, methods for making the same, and articles coated with such coatings.
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Patent Agency Ranking
6.发明申请公开(公告)号：US20150008375A1
公开(公告)日：2015-01-08
申请号：US13934862
申请日：2013-07-03
Applicant: The Boeing Company
Inventor： Terrell D. Riley , Alexandra E. Corona , Christopher Lamar Broadbent , Shahnaz Shokri , Quynhgiao N. Le
IPC: C09D5/24
CPC classification number: C09D5/24 , B05D5/12 , B60R16/06 , B64D45/02 , C08K3/10 , C08K2201/001 , C08K2201/011 , C08L81/08 , C09D175/04 , H01B1/22 , C08L65/00
Abstract: The present disclosure is directed to conductive, translucent water-borne conductive coatings comprising a water-borne lubricant coating base material, an amount of PEDOT:PSS solution, and an amount of metal-containing nanowire, methods for making the same, and articles coated with such coatings.
Abstract translation: 本公开涉及导电的半透明水性导电涂层，其包含水性润滑剂涂层基材，一定量的PEDOT：PSS溶液和一定量的含金属的纳米线，其制备方法和涂覆的制品 与这样的涂层。
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公开(公告)号：US11577275B2
公开(公告)日：2023-02-14
申请号：US16551374
申请日：2019-08-26
Applicant: The Boeing Company
Inventor： Mark R. Brei , Terrell D. Riley , Kevin D. Gordon , Meredith P. Nix
Abstract: The present disclosure is directed to a method for applying a multi-colored coating to a composite structure comprising applying a first co-curable film layer comprising a first color marking to a composite tool, applying a second co-curable film layer comprising a second color marking over the composite tool and at least partially over the first co-curable film layer to create a lay-up of a multi-colored marking, applying a composite structure over the lay-up of the multi-colored marking, and curing the lay-up of the multi-colored marking and the composite structure in a single curing step to create a cured multi-colored coating on the composite structure. A multi-colored coating for marking a composite structure and an aircraft part having a multi-colored marking are also provided.
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公开(公告)号：US20210060607A1
公开(公告)日：2021-03-04
申请号：US16551374
申请日：2019-08-26
Applicant: The Boeing Company
Inventor： Mark R. Brei , Terrell D. Riley , Kevin D. Gordon , Meredith P. Nix
Abstract: The present disclosure is directed to a method for applying a multi-colored coating to a composite structure comprising applying a first co-curable film layer comprising a first color marking to a composite tool, applying a second co-curable film layer comprising a second color marking over the composite tool and at least partially over the first co-curable film layer to create a lay-up of a multi-colored marking, applying a composite structure over the lay-up of the multi-colored marking, and curing the lay-up of the multi-colored marking and the composite structure in a single curing step to create a cured multi-colored coating on the composite structure. A multi-colored coating for marking a composite structure and an aircraft part having a multi-colored marking are also provided.
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公开(公告)号：US20200269562A1
公开(公告)日：2020-08-27
申请号：US16874352
申请日：2020-05-14
Applicant: The Boeing Company
Inventor： Anthony M. Westren , Mark Richard Brei , Thomas G. Lawton , Terrell D. Riley , Caitlin Elizabeth Kerr
IPC: B32B38/00 , B64C1/00 , B44C1/10 , B64F5/40 , B44C1/16 , B41J13/10 , B41J3/407 , B29C70/54 , B32B27/12 , B32B27/34 , B32B27/36 , B32B27/38 , B32B27/40 , B32B37/15 , B41J11/00
Abstract: Methods for placing an indicia on a composite structure generally include printing the indicia on a first film surface of a coating film, with the coating film being in a partially cured state at the time the printing the indicia is performed, and positioning the coating film on a partially cured composite structure such that a second film surface of the coating film faces and is positioned against a surface of the composite structure, with the second film surface being opposite the first film surface. Finally, the coating film and the composite structure may then be co-cured. Systems for printing an indicia on a composite structure generally include the coating film, a printer configured to print the indicia on the first film surface of the coating film, a securement configured to secure the coating film during printing, and a curing device for co-curing the coating film and the composite structure.
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公开(公告)号：US10682840B2
公开(公告)日：2020-06-16
申请号：US15611552
申请日：2017-06-01
Applicant: The Boeing Company
Inventor： Anthony M. Westren , Mark Richard Brei , Thomas G. Lawton , Terrell D. Riley , Caitlin Elizabeth Kerr
IPC: B32B38/00 , B64C1/00 , B44C1/10 , B64F5/40 , B44C1/16 , B41J13/10 , B41J3/407 , B29C70/54 , B32B27/12 , B32B27/34 , B32B27/36 , B32B27/38 , B32B27/40 , B32B37/15 , B41J11/00 , B41M3/12 , B41M5/00 , B29K105/24 , B29C37/00 , B29L31/30
Abstract: Methods for placing an indicia on a composite structure generally include printing the indicia on a first film surface of a coating film, with the coating film being in a partially cured state at the time the printing the indicia is performed, and positioning the coating film on a partially cured composite structure such that a second film surface of the coating film faces and is positioned against a surface of the composite structure, with the second film surface being opposite the first film surface. Finally, the coating film and the composite structure may then be co-cured. Systems for printing an indicia on a composite structure generally include the coating film, a printer configured to print the indicia on the first film surface of the coating film, a securement configured to secure the coating film during printing, and a curing device for co-curing the coating film and the composite structure.
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