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公开(公告)号：US20210101316A1
公开(公告)日：2021-04-08
申请号：US17117760
申请日：2020-12-10
发明人： Yung-Chun LEE , Yi-Chun TSAI , Chun-Ying WU , Wei-Hsiang SU , Shao-Hsuan HUANG , Ke-Chaung LU
摘要： A flexible mold has a mold body having a nanoimprinting microstructure and is gradually thickened from its periphery to the middle. Also, a resist spreading nanoimprinting method that integrates a soft mold into a dovetailed meal ring and then deforms it to form a point contact with a substrate before an imprinting process is followed and then convert a loading force into a specific distributed contact pressure for driving the resist flow by using an elastomer cushion pad with a pre-designed convex surface.
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公开(公告)号：US20200238578A1
公开(公告)日：2020-07-30
申请号：US16843596
申请日：2020-04-08
申请人： The Boeing Company
摘要： 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：US10654199B2
公开(公告)日：2020-05-19
申请号：US15841918
申请日：2017-12-14
申请人： The Boeing Company
摘要： 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：US10464240B2
公开(公告)日：2019-11-05
申请号：US14945615
申请日：2015-11-19
申请人： The Boeing Company
发明人： Marc R. Matsen , David S. Nansen , Lee C. Firth , Carey E. Wilkinson , Gregory J. Hickman , William C. Dykstra
摘要： Provided are induction heating cells including pressure bladders used for supporting dies and methods of using these induction heating cells. A pressure bladder may be disposed between a die and a bolster of the cell. Even when the bolster is deformed during operation of the cell, the pressure bladder continues to provide uniform support to the die thereby preserving integrity of the die and prevents its cracking or braking. As such, the cell may be operated at a higher processing pressure inside the cavity formed by the die without further strengthening the bolster. The bolster is allowed to deform without compromising the integrity of the die. The deformation of the bolster is compensated by the shape change of the pressure bladder. The number and/or position of the bladders in the cell may depend on the shape of processed parts.
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公开(公告)号：US20190168432A1
公开(公告)日：2019-06-06
申请号：US16098859
申请日：2017-05-10
申请人： ROCTOOL
发明人： JOSÉ FEIGENBLUM
摘要： A mold, particularly for injection molding, includes a shell defining a cavity delimiting a molding surface, a heat accumulator and inductor heater, configured to heat the heat accumulator. A receiving surface, which is a part of a surface of the shell other than the molding surface, is either exposed to or shielded from the heat of heat accumulator, to bring the entire molding surface to a predetermined temperature to inject the material into the cavity.
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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
申请人： The Boeing Company
CPC分类号： B29C43/52 , B29C33/06 , B29C2035/0811 , H05B6/105 , H05B2206/023
摘要： 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：US10052803B2
公开(公告)日：2018-08-21
申请号：US14976203
申请日：2015-12-21
申请人： ROCTOOL
CPC分类号： B29C45/7312 , B22C9/065 , B29C33/06 , B29C33/38 , B29C45/27 , B29C45/38 , B29C45/73 , B29C45/7331 , B29C2045/7368 , B29K2827/18 , B29K2905/08 , B29K2905/10 , B29K2907/04 , B29K2909/00 , H05B6/42
摘要： A mold having a first part with a carcass with a molding zone added thereto to provide a mechanical interface between the molding zone and the carcass. Inductors of the mold extend along a longitudinal direction in cavities between the mechanical interface and the molding zone. A cooling device of the mold extends at the mechanical interface between the molding zone and the carcass.
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公开(公告)号：US10035286B2
公开(公告)日：2018-07-31
申请号：US14655659
申请日：2013-12-18
申请人： TCTech Sweden AB
发明人： Jan Jäderberg , Lars Jäderberg
IPC分类号： B29C35/12 , B29C35/08 , B29C43/52 , B29C33/06 , B29C45/73 , B29C35/02 , B29C59/02 , B29C33/02 , B29C33/38
摘要： The present disclosure relates to a tool such as an injection molding tool or an embossing tool. A heating device including a stack of layers is provided for heating a tool surface. The stack may include a coil carrier layer with a number of wound coils for generating a magnetic field, and a conductive top layer, being adjacent to the tool surface currents are induced in the top layer to heat the surface. Efficient heating may be provided by solutions involving low resistivity layers that lead currents to the top layer without themselves developing heat to any greater extent. A conduction frame device can be provided beneath the top layer and around the perimeter thereof to provide reliable contact with a backing layer. A thermal resistance layer may placed between the intermediate layer and the top layer, and may comprise a heat resistive plastic material such as a polyimide.
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9.发明申请公开(公告)号：US20170036310A1
公开(公告)日：2017-02-09
申请号：US14818997
申请日：2015-08-05
申请人： The Boeing Company
CPC分类号： B29C33/06 , B29C70/44 , B29K2105/12 , B29K2105/256 , B29K2905/00 , B29K2905/12
摘要： Described herein is a method of forming tooling used to form a material. The method includes positioning a first susceptor made from a first susceptor material between first and second dies. At least one of the first and second dies includes a forming surface having a desired shape. The method further includes positioning a second susceptor made from a second susceptor material between the first and second dies such that the first susceptor is interposed between the second susceptor and the forming surface. Additionally, the method includes positioning a first bladder between the first and second dies such that the second susceptor is interposed between the first bladder and the first susceptor. Also, the method includes inflating the first bladder to concurrently deform the first susceptor and second susceptor into the desired shape.
摘要翻译： 这里描述的是形成用于形成材料的模具的方法。 该方法包括将由第一基座材料制成的第一基座定位在第一和第二管芯之间。 第一和第二模具中的至少一个包括具有期望形状的成形表面。 该方法还包括将由第二基座材料制成的第二基座定位在第一和第二模具之间，使得第一基座插入在第二基座和成形表面之间。 此外，该方法包括将第一气囊定位在第一和第二模具之间，使得第二感受器插入在第一气囊和第一感受器之间。 而且，该方法还包括使第一气囊膨胀以使第一感受器和第二感受器同时变形成所需形状。
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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
申请人： The Boeing Company
IPC分类号： B29C70/34 , B29C43/52 , B29C51/42 , B29C70/42 , B29C33/06 , B29C43/58 , B29C43/56 , B29C35/08
CPC分类号： 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
摘要： 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.
摘要翻译： 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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