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公开(公告)号：US20170297305A1
公开(公告)日：2017-10-19
申请号：US15292089
申请日：2016-10-12
申请人： The Boeing Company
发明人： Marc Rollo Matsen , Jeffery Lee Marcoe , Max U. Kismarton , Paul Stevenson Gregg , Lee Charles Firth
IPC分类号： B32B15/08 , B29C33/06 , B29C35/02 , B29C70/44 , B32B3/12 , B29D99/00 , B29C35/08 , B29L31/30 , B29K101/12
CPC分类号： B32B15/08 , B29C33/06 , B29C35/0272 , B29C35/0805 , B29C70/446 , B29C2035/0811 , B29D99/0014 , B29K2101/12 , B29L2031/3076 , B32B3/12 , B32B2305/024 , B32B2307/208 , B32B2311/18 , B32B2605/18 , Y10T428/1355 , Y10T428/31678
摘要： A method and apparatus for forming a sandwich structure is presented. A sandwich structure comprises a metallic core layer and a thermoplastic layer on a first side of the metallic core layer. The thermoplastic layer is consolidated against the first side of the metallic core layer.
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公开(公告)号：US09789747B2
公开(公告)日：2017-10-17
申请号：US14448305
申请日：2014-07-31
申请人： The Boeing Company
发明人： John Ralph Hull , Michael Strasik , Bret A. Voss , Mark A. Negley , William J. Sweet , Kevin R. Housen , Jason S. Damazo , Michael D. Gonzales , Michael Howard-Edward Ware , Lee Charles Firth
IPC分类号： F16L57/00 , F16L9/14 , B60H1/00 , F16L57/02 , F17D5/02 , F16L59/14 , F16L55/17 , B32B1/08 , B32B3/26 , B32B5/02 , F16L57/04
CPC分类号： B60H1/00564 , B32B1/08 , B32B3/266 , B32B5/024 , B32B2262/101 , B32B2307/304 , B32B2307/558 , B32B2605/18 , F16L55/07 , F16L55/17 , F16L57/02 , F16L57/04 , F16L59/145 , F17D5/02
摘要： Methods and systems for duct protection of a vehicle are provided. The methods and systems provided include an apparatus for containing a flow of fluid discharged from a fracture in a duct. The apparatus includes a ballistic containment layer and an insulation sheath coupled to the ballistic containment layer. The insulation sheath includes a first air containment layer, an insulation layer, and a second air containment layer.
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公开(公告)号：US11724420B2
公开(公告)日：2023-08-15
申请号：US16204260
申请日：2018-11-29
申请人： The Boeing Company
IPC分类号： B29C33/38 , B21D26/031 , B33Y10/00 , B33Y80/00 , B29C70/42
CPC分类号： B29C33/3842 , B21D26/031 , B29C70/42 , B29K2905/00 , B33Y10/00 , B33Y80/00
摘要： Systems and methods are provided for creating precursors for consolidating composite parts. One embodiment is a method for forming a metallic structure. The method includes forming a precursor for a pressure membrane that includes a contour having a linearized length corresponding with a linearized length of a surface of a forming tool. The method also includes affixing a perimeter of the precursor to a perimeter of a base member, leaving a volume between the base member and the precursor, altering a shape of the precursor at a superplastic temperature by forcing the precursor into complementary contact with the surface of the forming tool, and setting the shape of the precursor while the precursor is held in complementary contact.
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公开(公告)号：US10968497B2
公开(公告)日：2021-04-06
申请号：US15842723
申请日：2017-12-14
申请人： The Boeing Company
发明人： Marc R. Matsen , Lee Charles Firth , Luis Leon
摘要： A structure is heated in a tool. The structure is quenched in the tool such that a shape of the structure is maintained, in which quenching is performed by contacting the structure with a quenching medium.
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公开(公告)号：US10322564B2
公开(公告)日：2019-06-18
申请号：US15292089
申请日：2016-10-12
申请人： The Boeing Company
发明人： Marc Rollo Matsen , Jeffery Lee Marcoe , Max U. Kismarton , Paul Stevenson Gregg , Lee Charles Firth
IPC分类号： B32B15/08 , B29D99/00 , B29C70/44 , B29C33/06 , B29C35/02 , B29C35/08 , B32B3/12 , B29L31/30 , B29K101/12
摘要： A method and apparatus for forming a sandwich structure is presented. A sandwich structure comprises a metallic core layer and a thermoplastic layer on a first side of the metallic core layer. The thermoplastic layer is consolidated against the first side of the metallic core layer.
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公开(公告)号：US20190118415A1
公开(公告)日：2019-04-25
申请号：US15791683
申请日：2017-10-24
申请人： The Boeing Company
发明人： Marc R. Matsen , William C. Dykstra , Lee Charles Firth , Landon K. Henson , Tunde A. Olaniyan , John R. Hull
摘要： Systems and methods are provided for molding systems that have a low thermal mass. One embodiment is a first tool that includes a first frame. The first frame includes a first set of plates of magnetically permeable material, and a material disposed between plates of the first set. The first tool also includes a first set of induction coils that are disposed within the first frame and that generate a first electromagnetic field, and a first susceptor that extends from the first set of plates. The first susceptor generates heat in response to the first electromagnetic field. The first tool further includes a mold that extends from the first susceptor and receives heat via conductive heat transfer from the first susceptor. Each plate of the first set is thinner than a skin depth at which the first electromagnetic field would generate an electrical induction current.
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公开(公告)号：US20150137427A1
公开(公告)日：2015-05-21
申请号：US14606331
申请日：2015-01-27
申请人： The Boeing Company
发明人： Marc Rollo Matsen , Jeffery Lee Marcoe , Gregory James Schoepen Hickman , Alexander M. Rubin , Lee Charles Firth , Randall Dow Wilkerson , James R. Fox , Charles Richard Prebil
CPC分类号： B29C35/0805 , B21D26/033 , B23K20/12 , B23K20/1255 , B23K20/129 , B23K20/2336 , B23K2101/18 , B23K2101/28 , B23K2103/10 , B29C33/505 , B29C70/342 , B29C70/345 , B29C2035/0811 , B29C2035/0816 , B29C2791/009 , B29D99/0014 , B29K2101/12 , B29K2105/0827 , B29K2905/00
摘要： A method and apparatus for forming a stiffened thermoplastic panel is presented. The method may comprise placing a number of forming tools within a number of concave areas of a thermoplastic preform. The method may also place the thermoplastic preform with the number of forming tools within the number of concave areas on a thermoplastic lay-up to form a workpiece. The method may also position the workpiece within a tool. The tool may have a number of die liners configured to generate heat in response to a magnetic field. The method may also consolidate the workpiece to form the stiffened thermoplastic panel. Consolidating may comprise applying a magnetic field to the number of die liners to heat the workpiece to a consolidation temperature.
摘要翻译： 提出了一种用于形成加强型热塑性面板的方法和装置。 该方法可以包括将许多成形工具放置在热塑性预制件的多个凹入区域内。 该方法还可以将具有多个成型工具的热塑性预成型件放置在热塑性叠层的凹陷区域的数量内以形成工件。 该方法还可以将工件定位在工具内。 工具可以具有多个管芯衬套，其被配置为响应于磁场产生热量。 该方法还可以固结工件以形成加强的热塑性面板。 固结可以包括将磁场施加到模具衬套的数量以将工件加热到固结温度。
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公开(公告)号：US10792842B2
公开(公告)日：2020-10-06
申请号：US15791683
申请日：2017-10-24
申请人： The Boeing Company
发明人： Marc R. Matsen , William C. Dykstra , Lee Charles Firth , Landon K. Henson , Tunde A. Olaniyan , John R. Hull
摘要： Systems and methods are provided for molding systems that have a low thermal mass. One embodiment is a first tool that includes a first frame. The first frame includes a first set of plates of magnetically permeable material, and a material disposed between plates of the first set. The first tool also includes a first set of induction coils that are disposed within the first frame and that generate a first electromagnetic field, and a first susceptor that extends from the first set of plates. The first susceptor generates heat in response to the first electromagnetic field. The first tool further includes a mold that extends from the first susceptor and receives heat via conductive heat transfer from the first susceptor. Each plate of the first set is thinner than a skin depth at which the first electromagnetic field would generate an electrical induction current.
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公开(公告)号：US10029398B2
公开(公告)日：2018-07-24
申请号：US14606331
申请日：2015-01-27
申请人： The Boeing Company
发明人： Marc Rollo Matsen , Jeffery Lee Marcoe , Gregory James Schoepen Hickman , Alexander M. Rubin , Lee Charles Firth , Randall Dow Wilkerson , James R. Fox , Charles Richard Prebil
IPC分类号： B29C35/08 , B29C70/34 , B21D26/033 , B23K20/12 , B23K20/233 , B29D99/00 , B29K105/08 , B29K101/12 , B29C33/50 , B23K101/18 , B23K101/28 , B23K103/10
摘要： A method and apparatus for forming a stiffened thermoplastic panel is presented. The method may comprise placing a number of forming tools within a number of concave areas of a thermoplastic preform. The method may also place the thermoplastic preform with the number of forming tools within the number of concave areas on a thermoplastic lay-up to form a workpiece. The method may also position the workpiece within a tool. The tool may have a number of die liners configured to generate heat in response to a magnetic field. The method may also consolidate the workpiece to form the stiffened thermoplastic panel. Consolidating may comprise applying a magnetic field to the number of die liners to heat the workpiece to a consolidation temperature.
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公开(公告)号：US09469087B2
公开(公告)日：2016-10-18
申请号：US13937285
申请日：2013-07-09
申请人： The Boeing Company
发明人： Marc Rollo Matsen , Jeffery Lee Marcoe , Max U. Kismarton , Paul Stevenson Gregg , Lee Charles Firth
IPC分类号： B32B15/08 , B29D99/00 , B29C70/44 , B29C33/06 , B29C35/02 , B32B3/12 , B29L31/30 , B29K101/12 , B29C35/08
CPC分类号： B32B15/08 , B29C33/06 , B29C35/0272 , B29C35/0805 , B29C70/446 , B29C2035/0811 , B29D99/0014 , B29K2101/12 , B29L2031/3076 , B32B3/12 , B32B2305/024 , B32B2307/208 , B32B2311/18 , B32B2605/18 , Y10T428/1355 , Y10T428/31678
摘要： A method and apparatus for forming a sandwich structure is presented. A sandwich structure comprises a metallic core layer and a thermoplastic layer on a first side of the metallic core layer. The thermoplastic layer is consolidated against the first side of the metallic core layer.
摘要翻译： 提出了一种用于形成夹层结构的方法和装置。 夹层结构包括在金属芯层的第一侧上的金属芯层和热塑层。 热塑性层被固定在金属芯层的第一面上。
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