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公开(公告)号：US20160375629A1
公开(公告)日：2016-12-29
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
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 , B29C66/843 , B29C66/8432 , B29C70/30 , B29C70/46 , B29K2101/12 , B29K2105/0881 , B29L2031/3076 , B29L2031/3085 , B64C1/00 , 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.
Abstract translation: 一种用于焊接热塑性结构的方法和装置。 该装置包括底座，盖子和通道。 底座由对30KHz至350KHz范围内的频率具有不透磁性的材料形成。 盖由材料形成。 通道在基座和盖子之间延伸。
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公开(公告)号：US20160195062A1
公开(公告)日：2016-07-07
申请号：US14873684
申请日：2015-10-02
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc Rollo Matsen , Mark Alan Negley
CPC classification number: F03D1/0675 , B29C35/0805 , B29C64/129 , B29C70/446 , B29C2035/0811 , B29D99/0028 , B29L2031/08 , Y02E10/721 , Y02P70/523
Abstract: A method of fabricating a thermoplastic composite tubular structure for use as a wind turbine blade is presented using a combination of induction heating with smart susceptors to consolidate a wrapped mandrel. The method can include overbraiding the mandrel with a continuous fiber thermoplastic composite material to form an overbraided mandrel that is then installed in a ceramic induction oven where the mandrel is pressurized internally to consolidate the thermoplastic overbraid during heating
Abstract translation: 使用感应加热与智能基座的组合来形成用作风力涡轮机叶片的热塑性复合管状结构的方法，以固结包裹的心轴。 该方法可以包括用连续的纤维热塑性复合材料覆盖心轴以形成一个过量的心轴，然后安装在陶瓷感应炉中，其中心轴在内部被加压以在加热过程中固结热塑性超支架
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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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34.发明申请CURING COMPOSITES OUT-OF-AUTOCLAVE USING INDUCTION HEATING WITH SMART SUSCEPTORS 审中-公开使用智能断路器的感应加热固化复合材料公开(公告)号：US20160157302A1
公开(公告)日：2016-06-02
申请号：US15012843
申请日：2016-02-01
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , Mark Alan Negley , Jennifer Sue Noel
Abstract: A composite part is cured out-of-autoclave using an inductively heated, stand-alone tooling. The part in placed on a tool and is covered by a heating blanket. One side of the part is heated by inductive coil circuits in the tool, and the other side of the part is heated by inductive coil circuits in the blanket.
Abstract translation: 使用电感加热的独立工具将复合部件固化在高压釜外。 放在工具上的部件被加热毯覆盖。 该部件的一侧由工具中的感应线圈电路加热，并且部件的另一侧被毯中的感应线圈电路加热。
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公开(公告)号：US20160136879A1
公开(公告)日：2016-05-19
申请号：US14546184
申请日：2014-11-18
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , Donald K. Dabelstein , Lee Charles Firth , Flint Matthew Jamison , Patrice K. Ackerman
CPC classification number: B29C65/3676 , B29C65/3632 , B29C65/3668 , B29C65/4815 , B29C65/5057 , B29C66/112 , B29C66/131 , B29C66/343 , B29C66/3494 , B29C66/524 , B29C66/532 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/73115 , B29C66/73921 , B29C66/8432 , B29C66/91421 , B29C66/91933 , B29L2031/3076 , H05B6/105 , B29K2307/04 , B29K2071/00 , B29K2063/00
Abstract: A susceptor welding tape for use in thermoplastic welding. The susceptor welding tape comprising a thermoplastic film and a plurality of non-continuous susceptor conductors imbedded within the thermoplastic film. The plurality of non-continuous susceptor conductors allow a resulting thermoplastic weld formed by the susceptor weld tape to be tuned to a desired engineering characteristic. For example, the plurality of conductors allow the resulting thermoplastic weld formed by the susceptor weld tape to be tuned to a desired conductivity, a desired residual stress and/or a desired moisture barrier of the resulting thermoplastic weld.
Abstract translation: 用于热塑性焊接的基座焊接带。 包含热塑性薄膜和嵌入在热塑性薄膜内的多个非连续感受体导体的基座焊带。 多个不连续的感受体导体允许由基座焊接带形成的所得到的热塑性焊接被调谐到期望的工程特性。 例如，多个导体允许由感受器焊接带形成的所得到的热塑性焊接被调谐到所需的导电性，所需的残余应力和/或所得的热塑性焊接的所需的湿气屏障。
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Patent Agency Ranking
公开(公告)号：US09277594B2
公开(公告)日：2016-03-01
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
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：US20140353305A1
公开(公告)日：2014-12-04
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
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.
Abstract translation: 一种形成垫片的方法。 将具有导磁材料的液体垫片材料施加在用于多个复合部件之间的垫片的位置。 在该位置将磁场施加到导磁材料上。 磁场被配置为将液体垫片材料加热到使液体垫片材料变得固体并形成垫片的温度。
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公开(公告)号：US11272582B2
公开(公告)日：2022-03-08
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：US10827566B2
公开(公告)日：2020-11-03
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
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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公开(公告)号：US09868249B2
公开(公告)日：2018-01-16
申请号：US13942055
申请日：2013-07-15
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , William C. Dykstra
IPC: H05B6/10 , B29C65/36 , B29C65/48 , B29C65/50 , B29C65/00 , B64F5/10 , B29L31/30 , B64C1/12 , B64C3/26
CPC classification number: B29C65/3668 , B29C65/3632 , B29C65/368 , B29C65/4815 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/003 , B29C66/112 , B29C66/131 , B29C66/474 , B29C66/49 , B29C66/712 , B29C66/721 , B29C66/7212 , B29C66/73921 , B29C66/8122 , B29C66/8432 , B29C66/91411 , B29C66/91651 , B29C66/959 , B29L2031/3076 , B64C1/12 , B64C3/26 , B64F5/10 , B29K2309/08 , B29K2909/02
Abstract: A method and apparatus for performing induction welding. A number of protective layers are positioned between a susceptor layer and at least one of a plurality of workpieces at a weld location. An undesired current path is prevented from forming at the weld location during induction heating of the plurality of workpieces by the number of protective layers.
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