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1.发明申请THERMOPLASTIC COMPOSITE STRUCTURES EMBEDDED WITH AT LEAST ONE LOAD FITTING AND METHODS OF MANUFACTURING SAME 有权具有至少一个负载配件的热塑复合结构及其制造方法公开(公告)号：US20150321441A1
公开(公告)日：2015-11-12
申请号：US14465911
申请日：2014-08-22
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
CPC classification number: B32B1/08 , B29C33/52 , B29C70/205 , B29C70/462 , B29C2035/0811 , B32B5/024 , B32B2262/106 , B32B2605/08 , B32B2605/12 , B32B2605/18 , D04C1/06
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
Abstract translation: 制造嵌入有第一负载配件的热塑性复合管状结构，其包括在可溶性可扩张心轴周围编织第一组多个热塑性复合材料内层的步骤。 第一负载配件位于热塑性复合材料的第一多个内层上。 围绕第一负载配件和心轴编织第二多个热塑性复合材料外层，以便形成嵌入第一负载配件的外包芯。 将所覆盖的心轴安装到匹配的模具组件中并以特定的加热轮廓加热，以便将第一多个热塑性复合材料的内层和第二多个热塑性复合材料的外层与第一负载配件固结，以便 形成嵌入第一负载配件的热塑性复合管状结构。 第二负载配件可以被定位在热塑性复合材料的第一多个内层上。
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2.发明申请公开(公告)号：US20170190137A1
公开(公告)日：2017-07-06
申请号：US15465029
申请日：2017-03-21
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
CPC classification number: B32B1/08 , B29C33/52 , B29C70/205 , B29C70/462 , B29C2035/0811 , B32B5/024 , B32B2262/106 , B32B2605/08 , B32B2605/12 , B32B2605/18 , D04C1/06
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
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公开(公告)号：US09358703B2
公开(公告)日：2016-06-07
申请号：US13937269
申请日：2013-07-09
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Jeffery Lee Marcoe , Aaron William Bartel , John B. Moser , Brett I. Lyons
CPC classification number: B29C35/0805 , B29C70/446 , B29C2035/0811 , B29D24/004 , B29D99/0014 , B29K2101/12 , B29L2031/3085 , Y02T50/43
Abstract: An apparatus and method are presented. An apparatus comprises a composite structure, a plurality of cavities extending into the composite structure, and a plurality of mandrels located within the plurality of cavities. The composite structure comprises a thermoplastic material that is consolidated. The plurality of mandrels comprises a first material that is configured to generate heat in response to a magnetic field.
Abstract translation: 提出了一种装置和方法。 一种装置包括复合结构，延伸到复合结构中的多个空腔和位于多个空腔内的多个心轴。 复合结构包括被固结的热塑性材料。 多个心轴包括被配置为响应于磁场产生热量的第一材料。
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公开(公告)号：US10265923B2
公开(公告)日：2019-04-23
申请号：US15465029
申请日：2017-03-21
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
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Patent Agency Ranking
公开(公告)号：US09956718B2
公开(公告)日：2018-05-01
申请号：US13621991
申请日：2012-09-18
Applicant: The Boeing Company
Inventor： Aaron W. Bartel , John B. Moser
IPC: B29C53/04 , B29C53/42 , B29L31/30 , B29C65/08 , B29C65/36 , B29C65/50 , B29C65/56 , B29L23/00 , B29C65/00 , B29K79/00 , B29C53/38 , B29C53/84 , B29K101/12 , B29L9/00 , B29C65/48
CPC classification number: B29C53/04 , B29C53/385 , B29C53/42 , B29C53/84 , B29C65/08 , B29C65/36 , B29C65/48 , B29C65/5071 , B29C65/5085 , B29C65/56 , B29C66/1142 , B29C66/1222 , B29C66/1224 , B29C66/1226 , B29C66/4322 , B29C66/49 , B29C66/53243 , B29C66/547 , B29C66/71 , B29C66/721 , B29C66/723 , B29C66/72523 , B29C66/72525 , B29C66/727 , B29C66/73921 , B29C66/81455 , B29C2791/006 , B29K2079/085 , B29K2101/12 , B29L2009/00 , B29L2023/22 , B29L2031/3076 , Y10T156/1038
Abstract: A method of forming a structural tube may include urging a substantially flat thermoplastic sandwich sheet against a mandrel and heating the thermoplastic sandwich sheet to a temperature below a glass transition temperature. The method may further include allowing the thermoplastic sandwich sheet to cool and removing the mandrel, thereby forming a tube portion.
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公开(公告)号：US20140076479A1
公开(公告)日：2014-03-20
申请号：US13621991
申请日：2012-09-18
Applicant: The Boeing Company
Inventor： Aaron W. Bartel , John B. Moser
CPC classification number: B29C53/04 , B29C53/385 , B29C53/42 , B29C53/84 , B29C65/08 , B29C65/36 , B29C65/48 , B29C65/5071 , B29C65/5085 , B29C65/56 , B29C66/1142 , B29C66/1222 , B29C66/1224 , B29C66/1226 , B29C66/4322 , B29C66/49 , B29C66/53243 , B29C66/547 , B29C66/71 , B29C66/721 , B29C66/723 , B29C66/72523 , B29C66/72525 , B29C66/727 , B29C66/73921 , B29C66/81455 , B29C2791/006 , B29K2079/085 , B29K2101/12 , B29L2009/00 , B29L2023/22 , B29L2031/3076 , Y10T156/1038
Abstract: A method of forming a structural tube may include urging a substantially flat thermoplastic sandwich sheet against a mandrel and heating the thermoplastic sandwich sheet to a temperature below a glass transition temperature. The method may further include allowing the thermoplastic sandwich sheet to cool and removing the mandrel, thereby forming a tube portion.
Abstract translation: 形成结构管的方法可以包括将基本上平坦的热塑性夹层板推向心轴并将热塑性夹层板加热到低于玻璃化转变温度的温度。 该方法还可以包括允许热塑性夹层板冷却并移除芯棒，从而形成管部分。
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公开(公告)号：US10058950B1
公开(公告)日：2018-08-28
申请号：US13660376
申请日：2012-10-25
Applicant: THE BOEING COMPANY
Inventor： Noel T. Gerken , Robert James Miller , Jeffery L. Marcoe , John B. Moser , Aaron W. Bartel , Marc R. Matsen
CPC classification number: B23K13/015 , B23K13/01 , B23K13/04 , B23K35/001
Abstract: An induction welding system is provided. The system includes at least one induction coil configured to generate an alternating magnetic field, and a smart susceptor film sized to be positioned between a first component and a second component to be welded to the first component. The smart susceptor film includes a thermoplastic resin, and a plurality of metal alloy wires disposed in the thermoplastic resin such that the plurality of metal alloy wires are oriented substantially parallel to the generated alternating magnetic field.
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公开(公告)号：US09718248B2
公开(公告)日：2017-08-01
申请号：US14465911
申请日：2014-08-22
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , John B. Moser , Brett I. Lyons , Moushumi Shome , Kay Y. Blohowiak
CPC classification number: B32B1/08 , B29C33/52 , B29C70/205 , B29C70/462 , B29C2035/0811 , B32B5/024 , B32B2262/106 , B32B2605/08 , B32B2605/12 , B32B2605/18 , D04C1/06
Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.
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公开(公告)号：US20150013883A1
公开(公告)日：2015-01-15
申请号：US13937269
申请日：2013-07-09
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Jeffery Lee Marcoe , Aaron William Bartel , John B. Moser , Brett I. Lyons
IPC: B29C70/02
CPC classification number: B29C35/0805 , B29C70/446 , B29C2035/0811 , B29D24/004 , B29D99/0014 , B29K2101/12 , B29L2031/3085 , Y02T50/43
Abstract: An apparatus and method are presented. An apparatus comprises a composite structure, a plurality of cavities extending into the composite structure, and a plurality of mandrels located within the plurality of cavities. The composite structure comprises a thermoplastic material that is consolidated. The plurality of mandrels comprises a first material that is configured to generate heat in response to a magnetic field.
Abstract translation: 提出了一种装置和方法。 一种装置包括复合结构，延伸到复合结构中的多个空腔和位于多个空腔内的多个心轴。 复合结构包括被固结的热塑性材料。 多个心轴包括被配置为响应于磁场产生热量的第一材料。
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