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公开(公告)号:US11865809B2
公开(公告)日:2024-01-09
申请号:US16548657
申请日:2019-08-22
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley , Landon K. Henson , John R. Hull
IPC: B23K15/04 , B32B15/04 , B32B7/05 , B32B5/16 , B32B7/08 , B23K9/23 , B23K20/02 , B23K20/18 , B23K20/00 , B32B18/00
CPC classification number: B32B15/04 , B23K9/23 , B23K20/008 , B23K20/02 , B23K20/18 , B32B5/16 , B32B7/05 , B32B7/08 , B32B18/00 , B32B2307/304 , B32B2307/54 , Y10S228/00
Abstract: Disclosed herein is a method of forming a multi-layered metallic part. The method comprises stacking at least two metallic layers, each made of a metallic material having a ductility, to form a multi-layered metallic assembly. The method also comprises interposing a diffusion-bond preventing element directly between adjacent ones of the at least two metallic layers of the multi-layered metallic assembly. The method further comprises diffusion bonding the at least two metallic layers to each other at locations other than a location contiguous with the diffusion-bond preventing element to produce a multi-layered metallic part having a non-bonded region between the at least two metallic layers at the location of the diffusion-bond preventing element.
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公开(公告)号:US11077625B2
公开(公告)日:2021-08-03
申请号:US15411589
申请日:2017-01-20
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley , William Preston Geren , Robert Miller
Abstract: Thermoplastic welding apparatus and related methods are disclosed. An example method includes providing a smart susceptor between composite parts that are to be joined via thermoplastic welding. The example method includes positioning the composite parts and the smart susceptor on a tooling surface within a cavity of a tooling apparatus and applying a seal to the composite parts and the tooling surface to form a vacuum chamber between the composite parts and the tooling surface at a welding joint of the composite parts; producing a magnetic field at the welding joint. The example method includes providing a vacuum in the vacuum chamber during a welding operation.
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公开(公告)号:US10701767B2
公开(公告)日:2020-06-30
申请号:US15841964
申请日:2017-12-14
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Lee C. Firth , Mark A. Negley
Abstract: Disclosed herein are induction heating cells and methods of using these cells for processing. An induction heating cell may be used for processing (e.g., consolidating and/or curing a composite layup having a non-planar portion. The induction heating cell comprises a caul, configured to position over and conform to this non-planar portion. Furthermore, the cell comprises a mandrel, configured to position over the caul and force the caul again the surface of the feature. The CTE of the caul may be closer to the CTE of the composite layup than to the CTE of the mandrel. As such, the caul isolates the composite layup from the dimensional changes of the mandrel, driven by temperature fluctuations. At the same time, the caul may conform to the surface of the mandrel, which can be used to define the shape and transfer pressure to the non-planar portion.
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公开(公告)号:US20190134863A1
公开(公告)日:2019-05-09
申请号:US14599475
申请日:2015-01-17
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley , William Preston Geren
CPC classification number: B29C43/52 , B29C33/06 , B29C2035/0811 , H05B6/105 , H05B2206/023
Abstract: A system for inductively heating a workpiece may include an induction coil, at least one susceptor face sheet, and a current controller coupled. The induction coil may be configured to conduct an alternating current and generate a magnetic field in response to the alternating current. The susceptor face sheet may be configured to have a workpiece positioned therewith. The susceptor face sheet may be formed of a ferromagnetic alloy having a Curie temperature and being inductively heatable to an equilibrium temperature approaching the Curie temperature in response to the magnetic field. The current controller may be coupled to the induction coil and may be configured to adjust the alternating current in a manner causing a change in at least one heating parameter of the susceptor face sheet.
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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:US20160332501A1
公开(公告)日:2016-11-17
申请号:US14448305
申请日:2014-07-31
Applicant: The Boeing Company
Inventor: 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
CPC classification number: 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
Abstract: 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.
Abstract translation: 提供了用于车辆的风道保护的方法和系统。 提供的方法和系统包括用于容纳从管道中的裂缝排出的流体流的装置。 该装置包括弹道防护层和耦合到弹道防护层的绝缘护套。 绝缘护套包括第一空气容纳层,绝缘层和第二空气容纳层。
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公开(公告)号:US09314975B1
公开(公告)日:2016-04-19
申请号:US13870111
申请日:2013-04-25
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley , William C. Dykstra , Glen L. Smith , Robert J. Miller
CPC classification number: B29C70/345 , B29C33/06 , B29C35/0805 , B29C43/18 , B29C43/52 , B29C51/082 , B29C51/421 , B29C70/42 , B29C70/46 , B29C70/54 , B29C2035/0811 , B29C2043/568 , B29C2043/5816 , B29K2105/06 , B29K2105/0872
Abstract: A method for fabricating a thermoplastic composite component comprises inductively heating a thermoplastic pre-form with a first induction coil by inducing current to flow in susceptor wires disposed throughout the pre-form, inductively heating smart susceptors in a molding tool to a leveling temperature with a second induction coil by applying a high-strength magnetic field having a magnetic flux that passes through surfaces of the smart susceptors, shaping the magnetic flux that passes through surfaces of the smart susceptors to flow substantially parallel to a molding surface of the smart susceptors, placing the heated pre-form between the heated smart susceptors; and applying molding pressure to the pre-form to form the composite component.
Abstract translation: 一种制造热塑性复合材料组件的方法包括:通过将设置在整个预成型件中的基座导线中的电流感应电流流动到具有第一感应线圈的热塑性预成型件,将模制工具中的智能感应器感应加热至具有调平温度的 通过施加具有穿过所述智能基座的表面的磁通量的高强度磁场,使穿过所述智能基座的表面的磁通量成形为基本上平行于所述智能基座的模制表面流动的第二感应线圈,放置 加热的智能感受器之间的加热预成型件; 并将成型压力施加到预成型件以形成复合部件。
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公开(公告)号:US20190274194A1
公开(公告)日:2019-09-05
申请号:US16414268
申请日:2019-05-16
Applicant: THE BOEING COMPANY
Inventor: William P. GEREN , Stephen G. Moore , Robert J. Miller , Mark A. Negley , Scott Billings
Abstract: A heating system includes a structure to be heated, and a heating apparatus disposed to heat the structure. The heating apparatus includes a housing member, a plurality of resonant frequency power sources, and a plurality of associated controls. The plurality of resonant frequency power sources are attached to the housing member. The plurality of associated controllers is configured to separately operate the plurality of resonant frequency power sources at resonant frequencies matching heating requirements of the structure.
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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:US09930729B2
公开(公告)日:2018-03-27
申请号:US14697418
申请日:2015-04-27
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley
IPC: H05B6/10 , B22F3/16 , B22F3/03 , B22F3/087 , B22F3/105 , B22F3/14 , H05B6/06 , B21D21/00 , C21D1/18 , C21D1/42 , C21D6/00 , C21D9/42 , H05B6/08
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: Described herein is a method of forming a heat-treated material includes positioning the heat-treated material between first and second susceptors. Each of the first and second susceptors includes a tool face shaped according to a desired shape of the heat-treated material. The method also includes applying a low-strength magnetic field to the first and second susceptors to heat the first and second susceptors. Further, the method includes compressing the heat-treated material between the first and second susceptors to form the heat-treated material into the desired shape. The method additionally includes applying a high-strength magnetic field to the heat-treated material before compressing the heat-treated material between the first and second susceptors.
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