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公开(公告)号：US10059054B2
公开(公告)日：2018-08-28
申请号：US14753538
申请日：2015-06-29
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Mark A. Negley , William C. Dykstra , Robert James Miller
IPC: B29C65/36 , B29C65/04 , B29C65/00 , B29C70/30 , B64C1/00 , B29L31/30 , B29K101/12 , B29K105/08
CPC classification number: B29C65/04 , B29C65/3632 , B29C65/3636 , B29C65/364 , B29C65/3668 , B29C65/3676 , B29C65/3684 , B29C66/112 , B29C66/131 , B29C66/524 , B29C66/532 , B29C66/61 , B29C66/63 , B29C66/7212 , B29C66/72141 , B29C66/73921 , B29C66/81422 , B29C66/81423 , B29C66/843 , B29C66/8432 , B29C70/30 , B29C70/46 , B29K2101/12 , B29K2105/0881 , B29L2031/3076 , B29L2031/3085 , B64C1/00 , B64F5/10 , B29K2307/04
Abstract: A method and apparatus for welding a thermoplastic structure. The apparatus comprises a base, a cover, and a channel. The base is formed of a material that is magnetically opaque to a frequency in a range of 30 KHz to 350 KHz. The cover is formed of the material. The channel extends between the base and the cover.
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公开(公告)号：US09674899B2
公开(公告)日：2017-06-06
申请号：US13909491
申请日：2013-06-04
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Brian W. Smith , Robert James Miller
IPC: H05B6/10 , B29C35/08 , B64C3/26 , B64F5/00 , B29C65/36 , B29C65/48 , B29C65/76 , B29C65/78 , B29C65/00 , B29L31/30 , B29L11/00 , B29C37/00 , B64C1/00
CPC classification number: H05B6/108 , B29C35/0805 , B29C37/0075 , B29C65/362 , B29C65/4835 , B29C65/76 , B29C65/7826 , B29C66/112 , B29C66/131 , B29C66/301 , B29C66/524 , B29C66/543 , B29C66/721 , B29C66/7212 , B29C2035/0811 , B29L2011/0075 , B29L2031/3085 , B64C3/26 , B64C2001/0072 , B64F5/10 , H05B2206/023 , Y02T50/43 , B29K2307/04
Abstract: A method for forming a shim. A liquid shim material with a magnetically permeable material is applied in a location for the shim between a plurality of composite parts. A magnetic field is applied to the magnetically permeable material in the location. The magnetic field is configured to heat the liquid shim material to a temperature to cause the liquid shim material to become solid and form the shim.
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公开(公告)号：US09610654B1
公开(公告)日：2017-04-04
申请号：US14021468
申请日：2013-09-09
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller
CPC classification number: B29C65/02 , B23K13/04 , B29C65/3632 , B29C65/3668 , B29C65/368 , B29C66/00145 , B29C66/54 , B29C66/721 , B29C66/73921 , B29C66/73941 , B29C66/81455 , B29C66/81461 , B29L2031/3085 , B29L2031/711 , B64C1/12 , B64C3/26
Abstract: A method and apparatus for joining parts. A plurality of conformable induction coils embedded in a number of elastomeric sheets is positioned relative to a first composite part of the parts and a second composite part of the parts. A magnetic field is generated with the plurality of conformable induction coils. The magnetic field is configured to generate heat in a magnetically permeable material at a joint location. The heat joins the first composite part and the second composite part to each other.
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公开(公告)号：US20160262215A1
公开(公告)日：2016-09-08
申请号：US14640217
申请日：2015-03-06
Applicant: The Boeing Company
Inventor： Robert James Miller , Christopher John Hottes , Marc Rollo Matsen , James M. Kestner , Cameron Kai-Ming Chen , Leah Gillian Glauber
CPC classification number: H05B6/105 , H05B6/40 , H05B2203/003 , H05B2206/023
Abstract: A wire conductor for receiving alternating current and generating a magnetic field in response thereto. The wire conductor comprises a plurality of wire conductors in a parallel configured circuit extending between a first side of the wire conductor towards a second side of the wire conductor. A first layer of the plurality of wire conductors running in parallel from a first edge of the wire conductor to a second edge of the wire conductor. A second layer of parallel wire conductors residing above the first layer of the plurality of wire conductors, the second layer of parallel wire conductors running in parallel from the first edge of the wire conductor to the second edge of the wire conductor. The first layer of parallel wire conductors make a 180 degree turn along the first edge of the wire conductor. The first layer of parallel wire conductors make the 180 degree turn along the first edge of the wire conductor by first turning 90 degrees towards the second side of the parallel wire conductor. The first layer of parallel wire conductors make the 180 degree turn along the first edge of the wire conductor by first turning 90 degrees towards the second side of the parallel wire conductor, and then by turning 90 degrees towards the second edge of the parallel wire conductor.
Abstract translation: 一种用于接收交流电并响应于此产生磁场的导线。 电线导体包括多个线状导体，并联配置的电路，其在导体导体的第一侧向导线导体的第二侧延伸。 所述多个导线导体的第一层从所述导线导体的第一边缘平行地延伸到所述导线导体的第二边缘。 位于多个导线导体的第一层之上的第二层平行导线导体，第二层平行导线导体从导线导体的第一边缘平行延伸到导线导体的第二边缘。 第一层平行线导体沿导线导体的第一边缘转180度。 第一层平行导线通过首先向平行导线导体的第二侧转动90度，沿导线导体的第一边缘转动180度。 第一层平行线导体通过首先向平行导线导体的第二侧转动90度，然后朝向平行导线导体的第二边缘转动90度，沿着导线导体的第一边缘180度转动 。
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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
Applicant: The Boeing Company
Inventor： 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 classification number: 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
Abstract: 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.
Abstract translation: 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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Patent Agency Ranking
公开(公告)号：US20140231402A1
公开(公告)日：2014-08-21
申请号：US13770235
申请日：2013-02-19
Applicant: THE BOEING COMPANY
Inventor： Marc Rollo Matsen , Robert James Miller , Brian W. Smith , Geoffrey Allen Butler , Karl Marius Nelson
IPC: H05B1/00
CPC classification number: H05B1/00 , B29C35/0227 , B29C35/0805 , B29C2035/0811 , B29C2035/0816
Abstract: The thermal cycle time for curing a thermoset composite part in an autoclave is reduced by placing a heating blanket in proximity to an area of the composite part that is slow-to-heat, and inductively heating the area of the composite part that is slow-to-heat using the heating blanket.
Abstract translation: 通过在加热缓慢的复合部件的区域附近放置加热毯来减少在高压釜中固化热固性复合部件的热循环时间，并感应加热复合部件的慢速加热区域， 使用加热毯进行加热。
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公开(公告)号：US20200053841A1
公开(公告)日：2020-02-13
申请号：US16658053
申请日：2019-10-19
Applicant: The Boeing Company
Inventor： Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , James M. Kestner , Christopher John Hottes
Abstract: A coaxially arranged smart susceptor conductor, comprising a smart susceptor core comprising an alloy having a first Curie temperature point and a first smart susceptor shell coaxially arranged around the smart susceptor core. The first smart susceptor shell comprising a second Curie temperature point that is different than the first Curie temperature point of the smart susceptor core. In one arrangement, the second Curie temperature point of the first smart susceptor shell is lower than the first Curie temperature point of the smart susceptor core. In another arrangement, the smart susceptor conductor further comprises a second smart susceptor shell disposed about the first smart susceptor shell. The second smart susceptor shell comprising a third Curie temperature point.
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公开(公告)号：US10470253B2
公开(公告)日：2019-11-05
申请号：US14548045
申请日：2014-11-19
Applicant: The Boeing Company
Inventor： Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , James M. Kestner , Christopher John Hottes
Abstract: A coaxially arranged smart susceptor conductor, comprising a smart susceptor core comprising an alloy having a first Curie temperature point and a first smart susceptor shell coaxially arranged around the smart susceptor core. The first smart susceptor shell comprising a second Curie temperature point that is different than the first Curie temperature point of the smart susceptor core. In one arrangement, the second Curie temperature point of the first smart susceptor shell is lower than the first Curie temperature point of the smart susceptor core. In another arrangement, the smart susceptor conductor further comprises a second smart susceptor shell disposed about the first smart susceptor shell. The second smart susceptor shell comprising a third Curie temperature point.
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19.发明授权公开(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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公开(公告)号：US20180359818A1
公开(公告)日：2018-12-13
申请号：US16105766
申请日：2018-08-20
Applicant: The Boeing Company
Inventor： James M. Kestner , Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , Christopher John Hottes
CPC classification number: H05B6/105 , H05B6/40 , H05B2206/023
Abstract: A susceptor wire array. The array includes a first susceptor wire comprising an alloy having a first Curie temperature point and a second susceptor wire comprising an alloy having a second Curie temperature point, the second Curie temperature point is different than the first Curie temperature point of the first susceptor wire. In one susceptor wire arrangement, the second Curie temperature point of the second susceptor wire is lower than the first Curie temperature point of the first susceptor wire. In another susceptor wire arrangement, the array further comprises a third susceptor wire, the third susceptor wire comprising an alloy having a third Curie temperature point. The third Curie temperature point of the third susceptor wire may be different than the first Curie temperature point of the first susceptor wire.
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