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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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22.发明授权Method of consolidating/molding near net-shaped components made from powders 有权由粉末制成的网状部件附近的固结/成型方法公开(公告)号：US09457404B2
公开(公告)日：2016-10-04
申请号：US13758609
申请日：2013-02-04
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark Alan Negley , Robert James Miller
CPC classification number: H05B6/101 , B21D21/00 , B22F3/03 , B22F3/087 , B22F3/105 , B22F3/14 , B22F3/16 , B22F2003/1053 , B22F2202/05 , B22F2202/07 , B22F2203/00 , C21D1/18 , C21D1/42 , C21D6/00 , C21D9/42 , H05B6/06 , H05B6/08 , H05B6/105 , H05B2206/023 , Y02P10/253
Abstract: A method for consolidating a pre-form made of powder, comprising: (a) placing the pre-form between smart susceptors; (b) heating the smart susceptors to a leveling temperature by applying a varying low-strength magnetic field having a magnetic flux that passes through surfaces of the smart susceptors; (c) applying consolidation pressure to the pre-form at least during a time period subsequent to the temperature of the smart susceptors reaching the leveling temperature; and (d) while consolidation pressure is being applied, applying a pulsed high-strength magnetic field having a magnetic flux that passes through a surface of the pre-form. The strength and pulse rate of the high-strength magnetic field are selected so that the crystallographic phase of the pre-form will rapidly oscillate at a substantially constant temperature. The pulsed high-strength magnetic field is applied sufficiently long that superplasticity of the pre-form is attained during phase oscillation.
Abstract translation: 一种用于固结由粉末制成的预制件的方法，包括：（a）将所述预成型件置于智能基座之间; （b）通过施加具有穿过所述智能基座的表面的磁通量的变化的低强度磁场，将所述智能感受器加热到平整温度; （c）至少在智能感受器的温度达到调平温度之后的一段时间内对固化压力施加固化压力; 和（d）在施加固结压力的同时，施加具有穿过预成型件表面的磁通量的脉冲高强度磁场。 选择高强度磁场的强度和脉冲速率，使得预成型体的结晶相在基本恒定的温度下快速振荡。 脉冲高强度磁场施加足够长，使得在相位振荡期间获得预制件的超塑性。
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公开(公告)号：US20160195495A1
公开(公告)日：2016-07-07
申请号：US14589343
申请日：2015-01-05
Applicant: The Boeing Company
Inventor： John R. Hull , Robert James Miller
CPC classification number: G01R33/02 , G01N27/825 , G01R33/0385
Abstract: Embodiments described herein provide magnetic permeability measurements of ferromagnetic wires. In one embodiment, an apparatus comprises a non-magnetic wire retainer having a circular groove that holds a ferromagnetic wire for measurement. The apparatus further comprises a magnetic field generator proximate to the non-magnetic wire retainer that provides a substantially uniform magnetic field along a circumference of the circular groove. The apparatus further comprises a force sensor mechanically coupled to the magnetic field generator that measures an attractive force between the magnetic field generator and the ferromagnetic wire for determining the magnetic permeability of the ferromagnetic wire.
Abstract translation: 本文所述的实施例提供了铁磁线的磁导率测量。 在一个实施例中，一种装置包括具有保持用于测量的铁磁线的圆形凹槽的非磁性线保持器。 该装置还包括靠近非磁性线保持器的磁场发生器，其沿着圆形槽的圆周提供基本上均匀的磁场。 该装置还包括机械耦合到磁场发生器的力传感器，其测量磁场发生器和铁磁线之间的吸引力，以确定铁磁线的磁导率。
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24.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：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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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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