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公开(公告)号：US10239235B2
公开(公告)日：2019-03-26
申请号：US15346701
申请日：2016-11-08
IPC分类号： B29B11/00 , B29C65/00 , B29C70/00 , B33Y10/00 , B33Y30/00 , B29C64/00 , B29B11/16 , B29C65/62 , B29C70/54 , B29C70/24 , B29C70/30 , B29C64/141 , B29C64/147 , B29K29/00 , B29K105/08 , B29K307/04
摘要： A system fabricating composite preforms includes a layer assembly stage with a first stage for receiving new layers, such as layer N; and a second stage for holding up to K layers, such as layers N−1 to N−K. An interlayer reinforcement insertion mechanism inserts interlayer reinforcements Q through layer N and the layers N−1 to N−K, using a first layer spacing between layer N−K and layer N-K−1 in a completed layer stage. Following the interlayer reinforcements Q insertion, the layer assembly stage transfers the layer N−K to the completed layer stage; closes the first layer spacing, bringing layers N−K and N−K−1 into contact; and transfers the layer N to the second stage. The system repeats this cycle of receiving new layers, inserting interlayer reinforcements using layer spacings between the second and completed layer stages, closing these layer spacings, and transferring layers to construct composite preforms with arbitrary numbers of layers.
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公开(公告)号：US09381702B2
公开(公告)日：2016-07-05
申请号：US14216406
申请日：2014-03-17
IPC分类号： B29C65/62 , B29C70/02 , B29C70/54 , B29C67/00 , B29C70/24 , B29C70/30 , B33Y10/00 , B29B11/16
CPC分类号： B29B11/16 , B29C64/141 , B29C65/62 , B29C70/24 , B29C70/30 , B29C70/543 , B29C70/545 , B29K2029/04 , B29K2105/089 , B29K2307/04 , B33Y10/00 , B33Y30/00 , Y10T156/1074 , Y10T156/1075 , Y10T156/1093 , Y10T156/13 , Y10T156/1322
摘要： Methods creating composite preforms with a three-dimensional weaving pattern include stacking material layers and then connecting them with interlayer reinforcements. First and second layers are aligned and separated by a first layer spacing. First interlayer reinforcements are then inserted through at least the first and the second layers. At least a third layer is aligned with at least the first and second layers. Second interlayer reinforcements are inserted through at least the second and third layers, using the first layer spacing between the first and second layers to manipulated the second interlayer reinforcements during insertion. Following the insertion of at least the second interlayer reinforcement, this layer spacing is closed to bring the first and second layers into contact. Further layers and interlayer reinforcements may be added, using additional layer spacings to manipulate additional interlayer reinforcements to form complex three-dimensionally woven composite preforms.
摘要翻译： 创建具有三维织造图案的复合预成型件的方法包括堆叠材料层，然后将其与层间增强材料连接。 第一和第二层被对准和分隔第一层间距。 然后，将至少第一和第二层插入第一层间增强物。 至少第三层与至少第一层和第二层对准。 第二层增强件通过至少第二层和第三层插入，使用第一层和第二层之间的第一层间隔，以在插入期间操纵第二层增强件。 在插入至少第二层间加强件之后，将该层间隔封闭以使第一和第二层接触。 可以添加另外的层和层间增强物，使用附加的层间距来操纵附加的层间增强物以形成复合的三维编织的复合预制件。
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公开(公告)号：US20190211646A1
公开(公告)日：2019-07-11
申请号：US15864998
申请日：2018-01-08
CPC分类号： E21B33/129 , B32B1/00 , B32B5/06 , B32B9/007 , B32B9/04 , B32B17/00 , B32B17/067 , B32B2307/542 , B32B2313/04 , B32B2315/085 , E21B33/1204 , E21B33/1243
摘要： A slip ring segment, used as a part of a downhole tool placeable within a well casing, includes a stack of fabric layers, the fabric layers comprising fibers, such as carbon fiber and glass fiber, the stack having first and second surfaces, which can be axially tapering surfaces, and stitching passing through the stack. The stitching can conform to ASTM D6193, 205 hand stitching. The stitching includes first stitching portions passing through the stack, and second stitching portions connecting selected first stitching portions and extending along the first and second surfaces without knots, crimps or loops, with the first and second surfaces and the fabric layers substantially un-deformed by the stitching. The slip ring segment also includes a matrix binding the stack of fabric layers and the stitching, and well casing-engaging elements extending from the interior of the stack out past first surface.
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公开(公告)号：US20160059513A1
公开(公告)日：2016-03-03
申请号：US14836563
申请日：2015-08-26
IPC分类号： B32B5/02 , B32B5/26 , G05B19/4097 , D03D25/00
CPC分类号： B32B5/024 , B32B5/26 , B32B2262/101 , B32B2262/106 , B32B2305/07 , D03D25/005 , D10B2505/02
摘要： Systems and methods fabricate composite preforms in a flat or unfolded format. Following fabrication, the preform is folded and placed in or around a mold for curing. To facilitate folding and produce strong parts, the preform is fabricated with integrated, 3D woven joints at preform edges. These joints connect the folded preform portions to other parts of the preform, such as other unfolded or folded preform portions or internal features. Integrated joints may be flexible to facilitate assembly prior to curing. The unfolded preform design may be generated from a preform model by splitting the preform model at an initial joint location, unfolding the preform model into an unfolded preform, creating joint connectors in the unfolded preform at the initial joint location, determining a fiber layup of the unfolded preform, and generating fabrication data.
摘要翻译： 系统和方法以平面或展开形式制造复合预制件。 在制造之后，将预成型件折叠并放置在模具中或周围用于固化。 为了便于折叠和生产强力部件，预成型件在预制件边缘处由集成的3D编织接缝制成。 这些接头将折叠的预制件部分连接到预成型件的其它部分，例如其它未折叠或折叠的预制件部分或内部特征。 集成接头可以是柔性的，以便于在固化之前组装。 展开的预成型件设计可以通过在初始接合位置处分割预成型件模型从预成型件模型生成，将预成型件模型展开成展开的预成型件，在初始接合位置处在展开的预成型件中产生接合连接器，确定纤维叠层 展开的预成型件，以及生成制造数据。
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公开(公告)号：US10239281B2
公开(公告)日：2019-03-26
申请号：US15400638
申请日：2017-01-06
摘要： A process to create composite preforms and parts by stacking layers of two-dimensional fiber material (e.g., fiber cloth, fiber reinforced fabric, etc.) having pin-receiving holes and/or gaps disposed between the fibers of the fiber material is described. The stack is pinned together using a subset of pins, such as fiber reinforcing pins, inserted into a subset of the pin receiving holes and/or gaps, leaving at least some of the pin receiving holes and/or gaps available for pinning other layers, as layers of fiber material are added to the stack. As additional layers are added to the stack, different subsets of pins connect the additional layers to the stack, thereby building up the stack. Each layer of fiber material may have a different shape than the other layers and any arbitrary topology, potentially including non-convex and/or disjoint shapes. Furthermore, implementations may produce composite preforms having an arbitrary number of interconnected layers.
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6.发明申请SYSTEMS FOR THREE-DIMENSIONAL WEAVING OF COMPOSITE PREFORMS AND PRODUCTS WITH VARYING CROSS-SECTIONAL TOPOLOGY 审中-公开用于三维复合材料预制件和产品的系统，具有不同的跨部门拓扑公开(公告)号：US20170050340A1
公开(公告)日：2017-02-23
申请号：US15346701
申请日：2016-11-08
CPC分类号： B29B11/16 , B29C64/141 , B29C64/147 , B29C65/62 , B29C70/24 , B29C70/30 , B29C70/543 , B29C70/545 , B29K2029/04 , B29K2105/089 , B29K2307/04 , B33Y10/00 , B33Y30/00 , Y10T156/1074 , Y10T156/1075 , Y10T156/1093 , Y10T156/13 , Y10T156/1322
摘要： A system fabricating composite preforms includes a layer assembly stage with a first stage for receiving new layers, such as layer N; and a second stage for holding up to K layers, such as layers N−1 to N−K. An interlayer reinforcement insertion mechanism inserts interlayer reinforcements Q through layer N and the layers N−1 to N−K, using a first layer spacing between layer N−K and layer N−K−1 in a completed layer stage. Following the interlayer reinforcements Q insertion, the layer assembly stage transfers the layer N−K to the completed layer stage; closes the first layer spacing, bringing layers N−K and N−K−1 into contact; and transfers the layer N to the second stage. The system repeats this cycle of receiving new layers, inserting interlayer reinforcements using layer spacings between the second and completed layer stages, closing these layer spacings, and transferring layers to construct composite preforms with arbitrary numbers of layers.
摘要翻译： 制造复合预成型件的系统包括具有用于接收诸如层N的新层的第一阶段的层组装台; 以及用于保持K层的第二级，例如层N-1至N-K。 层间加强插入机构通过层N和层N-1至N-K使用层N-K和层N-K-1之间的第一层间隔在完成的层阶段中插入层间增强层Q。 在层间增强Q插入之后，层组装阶段将层N-K转移到完成的层阶段; 封闭第一层间距，使层N-K和N-K-1接触; 并将层N传送到第二阶段。 该系统重复接收新层的这个循环，在第二层和完成层之间使用层间隔插入层间增强层，封闭这些层间距，以及转移层以构造具有任意数量层的复合预制件。
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7.发明申请公开(公告)号：US20180236733A1
公开(公告)日：2018-08-23
申请号：US15900566
申请日：2018-02-20
申请人： Seriforge, Inc.
CPC分类号： B29C70/228 , B29C70/24 , B29C70/382 , B29C70/543 , B29C70/545 , D04H3/05 , D04H3/12
摘要： Various embodiments provide an apparatus, method, and/or system by which fiber, e.g., in the form of tow or tow, is used to create a shaped ply by facilitating drawing fiber from a supply along a fiber axis between two sets of pins; moving the pins across the fiber axis to form a fiber web in the desired ply shape; fixing the fiber web to form the shaped ply; and releasing the shaped ply. By enabling formation of shaped plies (including plies with doubly curved surfaces and simultaneous sequences of strategically shaped plies) directly from a single piece of fiber tow, various embodiments discussed herein enable substantial reductions in labor and materials costs that are conventionally associated with construction of composite preforms and accompanying composite products.
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公开(公告)号：US20180126598A1
公开(公告)日：2018-05-10
申请号：US15805068
申请日：2017-11-06
申请人： Jonathan Worthy Hollander , Eric Gregory , Ashish A. Choudhari , Jesica E. Ferro , Gregory E. James , Maxwell Shimshak , Benjamin D. Voiles
发明人： Jonathan Worthy Hollander , Eric Gregory , Ashish A. Choudhari , Jesica E. Ferro , Gregory E. James , Maxwell Shimshak , Benjamin D. Voiles
摘要： A method and system for automated fabrication of composite preforms. In one implementation, a fabrication apparatus includes a stitching assembly, needle apparatus, motion stage, preform cartridge, CAD/CAM Software, and embedded machine software. The stitching assembly includes an upper portion that supports a stitching mechanism. The stitching mechanism includes at least one needle assembly. The needle assembly may be configured with at least one needle apparatus configured to pass filaments through composite preforms. In one implementation, the stitching assembly is used to stitch layers of the composite preforms using a variety of stitching patterns. The fabrication apparatus may be configured to fold fabric layers of the composite preform before or after stitching two or more layers of the composite preform.
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公开(公告)号：US20170197399A1
公开(公告)日：2017-07-13
申请号：US15400638
申请日：2017-01-06
摘要： A process to create composite preforms and parts by stacking layers of two-dimensional fiber material (e.g., fiber cloth, fiber reinforced fabric, etc.) having pin-receiving holes and/or gaps disposed between the fibers of the fiber material is described. The stack is pinned together using a subset of pins, such as fiber reinforcing pins, inserted into a subset of the pin receiving holes and/or gaps, leaving at least some of the pin receiving holes and/or gaps available for pinning other layers, as layers of fiber material are added to the stack. As additional layers are added to the stack, different subsets of pins connect the additional layers to the stack, thereby building up the stack. Each layer of fiber material may have a different shape than the other layers and any arbitrary topology, potentially including non-convex and/or disjoint shapes. Furthermore, implementations may produce composite preforms having an arbitrary number of interconnected layers.
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10.发明授权公开(公告)号：US10773469B2
公开(公告)日：2020-09-15
申请号：US15900566
申请日：2018-02-20
申请人： Seriforge, Inc.
摘要： Various embodiments provide an apparatus, method, and/or system by which fiber, e.g., in the form of tow or tow, is used to create a shaped ply by facilitating drawing fiber from a supply along a fiber axis between two sets of pins; moving the pins across the fiber axis to form a fiber web in the desired ply shape; fixing the fiber web to form the shaped ply; and releasing the shaped ply. By enabling formation of shaped plies (including plies with doubly curved surfaces and simultaneous sequences of strategically shaped plies) directly from a single piece of fiber tow, various embodiments discussed herein enable substantial reductions in labor and materials costs that are conventionally associated with construction of composite preforms and accompanying composite products.
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