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11.发明授权Hybrid three-dimensional woven/laminated struts for composite structural applications 有权用于复合结构应用的混合三维编织/层压支柱公开(公告)号：US07655581B2
公开(公告)日：2010-02-02
申请号：US11281063
申请日：2005-11-17
申请人： Jonathan Goering
发明人： Jonathan Goering
CPC分类号： B29B11/16 , B29C70/222 , B29C70/24 , D03D11/00 , D03D11/02 , D03D25/005 , D10B2505/02 , Y10T428/24008 , Y10T428/24132 , Y10T428/24479 , Y10T428/24488 , Y10T428/24785 , Y10T442/3179 , Y10T442/3195 , Y10T442/3472 , Y10T442/3569 , Y10T442/3594
摘要： A woven preform used to reinforce a composite structure which includes a central portion having a plurality of interwoven layers. The preform also includes first and second end portions having a plurality of independent woven layers that are integrally woven with the plurality of interwoven layers in the central portion and which extend along the entire length the preform. Interspersed between the plurality of independent woven layers in the first and second end portions are bias plies.
摘要翻译： 用于加强复合结构的编织预制件，其包括具有多个交织层的中心部分。 预型件还包括第一和第二端部，其具有多个独立的编织层，其与中心部分中的多个交织层整体编织并且沿整个长度延伸预成型件。 散布在第一和第二端部中的多个独立编织层之间是偏置层。
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公开(公告)号：US11959511B2
公开(公告)日：2024-04-16
申请号：US17225353
申请日：2021-04-08
发明人： Ralph Funck , Martin Welsch , Alexander Wieland
CPC分类号： F16B7/042
摘要： The present invention concerns a rod end that has a locking mechanism where the locking mechanism has an insert, a fork end, a female torque locking element, and a male torque locking element. Upon activation of the locking mechanism, the female torque locking element engages with the male torque locking element in a form-fitting connection. The locking mechanism of the present invention can easily be activated and is capable of withstanding a torque.
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公开(公告)号：US20230183891A1
公开(公告)日：2023-06-15
申请号：US18107180
申请日：2023-02-08
发明人： Stephen Biddle
CPC分类号： D03D3/08 , D03D1/00 , D03D25/005 , D03D49/20 , D03J1/22 , D10B2505/02
摘要： Disclosed is an apparatus and method for forming three-dimensional woven preforms that can be curved and have continuous fibers in the direction of curvature. Also disclosed are woven preforms formed thereby.
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公开(公告)号：US11192312B2
公开(公告)日：2021-12-07
申请号：US16154961
申请日：2018-10-09
发明人： Jonathan Goering
摘要： Disclosed is a method of forming a 3D woven omega-shaped stiffener by flat weaving a plurality of layers of interwoven warp and weft fibers to form a flat woven fabric having a cap portion, a first and a second web portion, a first and second foot portion, and an inner wrap portion. The 3D woven fabric is woven so that least some of the weft fibers are continuous across a juncture between the web portion and the foot portions. The flat woven fabric is then formed into the omega shape.
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15.发明申请公开(公告)号：US20210370619A1
公开(公告)日：2021-12-02
申请号：US17328351
申请日：2021-05-24
发明人： Ralph Funck , Jens Jung , Martin Welsch
摘要： Disclosed are reinforced structures. The structures are comprised of reinforced elements that have continuous fibers embedded in a matrix material. The reinforced elements are combined in a matrix material to form a desired shape of reinforced structure.
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公开(公告)号：US10150229B2
公开(公告)日：2018-12-11
申请号：US15799959
申请日：2017-10-31
发明人： Jonathan Goering
IPC分类号： D03D3/00 , B32B5/16 , D05B23/00 , B32B17/02 , B32B1/04 , B32B18/00 , B29B11/16 , F01D25/24 , F01D21/04
摘要： Woven preforms, for example those used for jet aircraft engine fancases, may need additional stiffeners to improve the strength and/or dynamic performance of the preform assembly, as well as to serve as attachment points. The present invention describes several improved woven preforms that include circumferential or axial stiffeners, as well as methods of manufacturing the same. One embodiment includes circumferential stiffeners added to a woven preform. Another embodiment includes sub-preforms with integral flanges that combine to make integral stiffeners. A further embodiment includes an intermediate stiffener wrapped onto a base sub-preform wrap, wherein the intermediate stiffener wrap incorporates intermediate stiffeners. Another embodiment incorporates bifurcations in one or more layers of an outermost wrap of a multi-layer fabric composite that forms a preform, wherein the bifurcated outer wrap is folded to form stiffeners that may be oriented circumferentially or axially.
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公开(公告)号：US20180104857A1
公开(公告)日：2018-04-19
申请号：US15799991
申请日：2017-10-31
发明人： Jonathan Goering
CPC分类号： B29B11/16 , F01D21/045 , F01D25/24 , F05D2300/6012 , F05D2300/603 , Y02T50/672 , Y10T29/49826 , Y10T428/13 , Y10T428/1314 , Y10T428/1362
摘要： Woven preforms, for example those used for jet aircraft engine fancases, may need additional stiffeners to improve the strength and/or dynamic performance of the preform assembly, as well as to serve as attachment points. The present invention describes several improved woven preforms that include circumferential or axial stiffeners, as well as methods of manufacturing the same. One embodiment includes circumferential stiffeners added to a woven preform. Another embodiment includes sub-preforms with integral flanges that combine to make integral stiffeners. A further embodiment includes an intermediate stiffener wrapped onto a base sub-preform wrap, wherein the intermediate stiffener wrap incorporates intermediate stiffeners. Another embodiment incorporates bifurcations in one or more layers of an outermost wrap of a multi-layer fabric composite that forms a preform, wherein the bifurcated outer wrap is folded to form stiffeners that may be oriented circumferentially or axially.
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公开(公告)号：US09725832B1
公开(公告)日：2017-08-08
申请号：US15019137
申请日：2016-02-09
CPC分类号： D03C9/02 , D03D41/004
摘要： An apparatus for weaving a multilayer product that has one or more warp columns for placing warp fibers and one or more heddle columns for heddles for lacing the warp fibers. The weaving apparatus has a numerical ratio of warp columns and heddle columns that is a fractional number. And a portion of the warp fibers are laceable through heddles on one or more heddle columns based on the fractional number. A method for weaving a multilayer product where adjacent warp fibers are segmented and laced through heddles on the heddle columns based on the fractional number.
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19.发明授权公开(公告)号：US09186850B2
公开(公告)日：2015-11-17
申请号：US12607715
申请日：2009-10-28
申请人： Jonathan Goering
发明人： Jonathan Goering
CPC分类号： B29C70/222 , B29B11/16 , D03D3/00 , D03D3/08 , Y10T428/1362 , Y10T428/24074
摘要： A woven fiber preform, a fiber reinforced composite incorporating the preform, and methods of making thereof are disclosed. The woven preform includes a plurality of warp and weft yarns or fibers interwoven to form a continuous spiral fabric. The spiral fabric may take the shape of an Archimedes spiral. The weft yarns in the preform may have a uniform or variable pick spacing, or a uniform or variable angular separation. The spiral fabric of the Archimedes spiral may be assembled or wrapped to form a conical shell structure, which could be a portion of a spinner or an exit cone. The spiral fabric may be woven on a loom equipped with a differential take-up mechanism.
摘要翻译： 公开了一种编织纤维预成型体，包含该预型体的纤维增强复合材料及其制造方法。 编织预制件包括多个经纱和纬纱或纤维交织以形成连续的螺旋织物。 螺旋织物可以采取阿基米德螺旋形的形状。 预制件中的纬纱可以具有均匀或可变的拾取间距，或均匀或可变的角分离。 阿基米德螺旋的螺旋织物可以组装或包裹以形成锥形壳结构，其可以是旋转器或出口锥体的一部分。 螺旋织物可以在配有差速牵引机构的织机上编织。
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公开(公告)号：US20150132487A1
公开(公告)日：2015-05-14
申请号：US14602861
申请日：2015-01-22
发明人： Jonathan Goering , Craig Rowles
CPC分类号： D03D25/005 , B29B11/16 , B29C70/222 , B29C70/462 , B29C70/48 , B29K2707/04 , B29L2031/005 , D03D3/08 , D03D15/12 , D03D49/04 , D03D49/20 , D06C15/00 , Y02T50/43 , Y10T442/2984 , Y10T442/30 , Y10T442/3008 , Y10T442/3187 , Y10T442/3195 , Y10T442/3236 , Y10T442/3301
摘要： A three dimensional woven preform, a fiber reinforced composite incorporating the preform, and methods of making thereof are disclosed. The woven preform includes one or more layers of a warp steered fabric. A portion of the warp steered fabric is compressed into a mold to form an upstanding leg. The preform includes the upstanding leg and a joggle in a body portion. The body portion and upstanding leg are integrally woven so there is continuous fiber across the preform. A portion of the warp steered fabric includes stretch broken carbon fibers in the warp direction, and another portion includes conventional carbon fibers. The warp steered fabric can be woven on a loom equipped with a differential take-up mechanism. The warp steered fabric can be a single or multilayer fabric. The preform or the composite can be a portion of an aircraft window frame.
摘要翻译： 公开了一种三维编织预制件，包含该预制件的纤维增强复合材料及其制造方法。 编织预制件包括一层或多层经向转向织物。 经向转向织物的一部分被压缩成模具以形成直立的腿部。 预成型件包括直立的腿部和身体部分中的弯曲部。 主体部分和直立的腿部是整体编织的，因此在预成型件上有连续纤维。 经向转向织物的一部分在经向上包括拉伸断裂的碳纤维，另一部分包括常规的碳纤维。 经向转向织物可以在配有差速牵引机构的织机上编织。 经向转向织物可以是单层或多层织物。 预制件或复合材料可以是飞机窗框的一部分。
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