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公开(公告)号:US20230312088A1
公开(公告)日:2023-10-05
申请号:US18087544
申请日:2022-12-22
IPC分类号: B64C27/473 , B29C70/02 , B29C70/68 , B29D99/00
CPC分类号: B64C27/473 , B29C70/023 , B29C70/025 , B29C70/682 , B29C70/685 , B29D99/0025 , B29L2031/082
摘要: An apparatus for securing first and second skins to a core in a composite rotor blade includes an elongated member configured to be installed through a passage in the core of the composite rotor blade. The elongated member has a first end configured to be attached to an outer surface of the first skin and a second end configured to be attached to an outer surface of the second skin. The apparatus also includes a first patch configured to adhere the first end to the outer surface of the first skin, and a second patch configured to adhere the second end to the outer surface of the second skin such the elongated member extends from the outer surfaces of the first and second skins through the passage in the core.
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公开(公告)号:US20180229443A1
公开(公告)日:2018-08-16
申请号:US15434565
申请日:2017-02-16
申请人: The Boeing Company
CPC分类号: B64C3/22 , B21D47/00 , B22F3/1055 , B29C64/10 , B29C64/106 , B29C70/023 , B29C70/026 , B29C70/086 , B29C70/443 , B29D24/005 , B29D99/0014 , B29D99/0089 , B29K2063/00 , B29L2031/3082 , B29L2031/3085 , B29L2031/60 , B29L2031/608 , B32B3/12 , B33Y10/00 , B33Y80/00 , D06M15/55 , D06M2101/40
摘要: A component, including a part, comprising a honeycomb-like structure formed from at least a seamless resin-infused fiber composite material. The honeycomb-like structure includes a first plurality of honeycomb-like cells, and a second plurality of honeycomb-like cells, different than the first plurality of honeycomb-like cells.
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公开(公告)号:US20160222914A1
公开(公告)日:2016-08-04
申请号:US14610159
申请日:2015-01-30
发明人: Clifford E. Maki , Larry Dean Elie , Kevin Durand Byrd , Rick L. Williams , Wolfram Buschhaus , Matthew John Zaluzec
CPC分类号: F02F7/0095 , B29C70/023 , B29K2105/12 , B29K2105/20 , B29K2705/08 , B29L2031/749 , F02F7/0021 , F02F7/0085 , F05C2201/0412 , F05C2225/00
摘要: Systems and methods are provided for forming an engine comprising a thermoset composite engine block. One example method includes reinforcing the engine block with a plurality of metal strips, wherein a first portion of the plurality of metal strips are positioned in a substantially transverse direction of the engine block and a second portion of the plurality of metal strips are positioned in a substantially longitudinal direction of the engine block. The plurality of metal reinforcing strips may provide additional reinforcement to the engine block.
摘要翻译: 提供了用于形成包括热固性复合发动机块的发动机的系统和方法。 一个示例性方法包括用多个金属条加强发动机缸体,其中多个金属带的第一部分位于发动机缸体的基本上横向的方向上,并且多个金属带的第二部分位于 发动机缸体的大致纵向方向。 多个金属加强条可以向发动机块提供附加的加强件。
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公开(公告)号:US09376871B2
公开(公告)日:2016-06-28
申请号:US14374442
申请日:2013-04-09
IPC分类号: E21B17/10 , B29C70/06 , B29C45/14 , B29C45/16 , B29C70/02 , B29C70/68 , B32B37/12 , B32B37/16 , B29L23/00 , B29K105/08 , B29K509/02 , B29K509/04 , B29L9/00
CPC分类号: E21B17/1078 , B29C45/14786 , B29C45/1671 , B29C70/023 , B29C70/06 , B29C70/68 , B29K2105/0854 , B29K2509/02 , B29K2509/04 , B29L2009/00 , B29L2023/22 , B32B37/1284 , B32B37/16 , B32B2305/08 , B32B2597/00 , E21B17/10 , E21B17/1042 , E21B17/1085 , Y10T156/10
摘要: A positioning member (11) for a tubular (10) is formed using a prefabricated fiber-reinforced resin shell (1) positioned upon a surface of the tubular and bonded to provide a protrusion upon the surface of the tubular. In a disclosed method a fiber-reinforced resin shell (1) is secured to an external surface of a tubular (10) thereby enclosing a cavity between the shell (1) and the surface of the tubular (10); a bonding agent is introduced through inlet ports (5) in a surface of the fiber-reinforced resin shell (1) to fill a cavity between the shell (1) and the surface of the tubular (10), and the bonding agent is cured.
摘要翻译: 用于管(10)的定位构件(11)使用预定的纤维增强树脂壳(1)形成,所述预制纤维增强树脂壳(1)定位在管的表面上并结合以在管的表面上提供突起。 在公开的方法中,纤维增强树脂壳体(1)固定到管状物(10)的外表面,从而在壳体(1)和管状物(10)的表面之间封闭空腔; 通过纤维增强树脂壳体(1)的表面中的入口(5)引入粘合剂,以填充壳体(1)和管状物(10)的表面之间的空腔,并且粘结剂固化 。
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5.
公开(公告)号:US20150151390A1
公开(公告)日:2015-06-04
申请号:US14619877
申请日:2015-02-11
申请人: NEPTCO, INC.
发明人: Daniel E. Upton , Joel D. Gruhn
CPC分类号: B23P15/04 , B29B11/16 , B29C70/023 , B29C70/083 , B29C70/54 , B29C2793/0081 , B29D99/0028 , B29L2031/085 , F03D1/0675 , F03D80/00 , Y02E10/721 , Y02E10/74 , Y02P70/523 , Y10T29/49336 , Y10T29/53961 , Y10T156/10
摘要: Apparatus for storing, tapering, cutting and dispensing preform layers of material includes a device for storing coiled lengths of the preform layers of material and a mechanism for receiving coiled lengths of the preform layers of material. The mechanism includes a grinding mechanism to grind portions of the preform layers of material and a cutter to cut the grinded portions of material. A programmable controller is configured to control the operations of at least one of the device and mechanism.
摘要翻译: 用于存储,渐缩,切割和分配预成型材料层的装置包括用于存储螺旋长度的预成型材料层的装置和用于接收螺旋长度的预成型体材料层的装置。 该机构包括研磨机构,用于研磨材料的预制件层的一部分和切割机以切割材料的磨削部分。 可编程控制器被配置为控制装置和机构中的至少一个的操作。
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公开(公告)号:US20150122484A1
公开(公告)日:2015-05-07
申请号:US14592464
申请日:2015-01-08
CPC分类号: E21B17/1078 , B29C45/14786 , B29C45/1671 , B29C70/023 , B29C70/06 , B29C70/68 , B29K2105/0854 , B29K2509/02 , B29K2509/04 , B29L2009/00 , B29L2023/22 , B32B37/1284 , B32B37/16 , B32B2305/08 , B32B2597/00 , E21B17/10 , E21B17/1042 , E21B17/1085 , Y10T156/10
摘要: A positioning member for a tubular is formed using a prefabricated fibre-reinforced resin shell positioned upon a surface of the tubular and bonded to provide a protrusion upon the surface of the tubular. In a disclosed method a fibre-reinforced resin shell is secured to an external surface of a tubular thereby enclosing a cavity between the shell and the surface of the tubular; a bonding agent is introduced through inlet ports in a surface of the fibre-reinforced resin shell to fill a cavity between the shell and the surface of the tubular (10), and the bonding agent is cured.
摘要翻译: 用于管状的定位构件使用预定的纤维增强树脂壳形成,所述预制纤维增强树脂壳定位在管的表面上并结合以在管的表面上提供突起。 在公开的方法中,纤维增强树脂壳固定到管的外表面,从而在壳与管的表面之间封闭空腔; 通过纤维增强树脂壳体的表面中的入口引入粘合剂以填充壳体和管状物(10)的表面之间的空腔,并且粘合剂固化。
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公开(公告)号:US20110243750A1
公开(公告)日:2011-10-06
申请号:US13007111
申请日:2011-01-14
IPC分类号: F03D11/02
CPC分类号: F03D1/0675 , B29B11/16 , B29C70/023 , B29C70/083 , B29D99/0028 , B29L2031/085 , F03D9/25 , F03D80/00 , F05B2220/30 , F05B2230/20 , F05B2240/2211 , F05B2280/6003 , Y02E10/721 , Y02E10/722 , Y02E10/725 , Y02E10/74 , Y02P70/523 , Y10T156/10
摘要: Structural preform layers of multiple rigid unidirectional strength elements or rods are constructed and arranged for use in fabricating load-bearing support structures and reinforcements of wind turbine blades. Individual preform layers include multiple elongate unidirectional strength elements or rods arranged in a single layer along a longitudinal axis of the preform layer. Each preform layer includes one or more fibrous carrier layers to which the multiple strength elements or rods are joined and arranged in the single layer. Each strength element or rod is longitudinally oriented and adjacent to other elements or rods. Individual strength elements or rods include a mass of substantially straight unidirectional structural fibers embedded within a matrix resin such that the elements or rods have a substantially uniform distribution of fibers and high degree of fiber collimation. The relative straightness of the fibers and fiber collimation provide strength elements or rods and the preform layers with high rigidity and significant compression strength.
摘要翻译: 多个刚性单向强度元件或杆的结构预制件层被构造和布置用于制造风力涡轮机叶片的承载支撑结构和增强件。 单独的预成型层包括沿预成型体层的纵向轴线布置在单层中的多个细长单向强度元件或棒。 每个预成型件层包括一个或多个纤维载体层,多个强度元件或杆连接并布置在单层中。 每个强度元件或杆纵向定向并且与其它元件或杆相邻。 单独的强度元件或棒包括嵌入基体树脂内的基本上直的单向结构纤维的质量,使得元件或棒具有基本均匀的纤维分布和高度的纤维准直。 纤维和纤维准直的相对直线性提供强度元素或棒和具有高刚性和显着压缩强度的预制件层。
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8.
公开(公告)号:US5733404A
公开(公告)日:1998-03-31
申请号:US545392
申请日:1995-10-19
申请人: Glen Freitas , Joseph S. Boyce , Constance Magee
发明人: Glen Freitas , Joseph S. Boyce , Constance Magee
CPC分类号: B29C70/24 , B29C70/023 , B29C70/82 , B29C70/887 , B32B7/08 , Y10T428/24058 , Y10T428/24074 , Y10T428/24116 , Y10T428/24124 , Y10T428/24174 , Y10T428/249953 , Y10T428/249958 , Y10T428/31
摘要: A translaminar reinforcement system for Z-direction reinforcement of a fiber matrix structure in which a plurality of reinforcing elements are disposed in a body of compactible material to extend in at least one direction and orientated at at least one acute angle and driven into a fiber matrix structure when the body is compacted by a compressive force.
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公开(公告)号:US5665441A
公开(公告)日:1997-09-09
申请号:US312929
申请日:1994-09-30
申请人: Hiroyasu Suzue , Yuichi Aizawa
发明人: Hiroyasu Suzue , Yuichi Aizawa
IPC分类号: A01K87/00 , A63B53/10 , A63C11/22 , B29C70/02 , B32B1/08 , B32B15/08 , B62K19/16 , F16C3/02 , F16C13/00 , A63B53/12
CPC分类号: F16C3/026 , A01K87/00 , A63B53/10 , A63C11/22 , B29C70/023 , B32B1/08 , B32B15/08 , B62K19/16 , F16C13/00 , B29K2105/206 , Y10T428/1314 , Y10T428/1321 , Y10T428/1355 , Y10T428/1359 , Y10T428/1362 , Y10T428/1369 , Y10T428/249942 , Y10T428/24995 , Y10T442/3407 , Y10T442/3431 , Y10T442/3447 , Y10T442/3659 , Y10T442/3683 , Y10T442/3691
摘要: A main body of a hollow cylindrical member is formed of a wound preimpregnation sheet made of reinforcing fibers impregnated with synthetic resins. A synthetic resins layer with a metallic member is provided onto an outer periphery of the main body for reinforcing and/or decorative property. The metallic member is in the form of a thin film bonded to an outer periphery of the synthetic resins layer or a net-like metallic member embedded in the layer.
摘要翻译: 中空圆柱形构件的主体由浸渍有合成树脂的增强纤维制成的卷绕预浸层形成。 具有金属构件的合成树脂层设置在主体的外周上,用于加强和/或装饰性能。 金属构件为与合成树脂层的外周接合的薄膜或嵌入该层的网状金属构件。
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公开(公告)号:US5362345A
公开(公告)日:1994-11-08
申请号:US11397
申请日:1993-01-28
申请人: Andreas Stettler , Kurt Anderegg
发明人: Andreas Stettler , Kurt Anderegg
CPC分类号: B62D29/046 , B29C53/583 , B29C70/023 , B61D17/005
摘要: A method for the manufacture of integral coach bodies includes the steps of winding an inner covering layer on a body-shaped winding core and attaching a plurality of U-shaped channel segments to outer surfaces of ceiling and floor walls and attaching a plurality of insulation segments in corner regions of the body. A stiffening framework is attached to the outer surfaces of side walls of the body, insulation plates are attached in some rectangular openings in the stiffening framework and blank covers are positioned in other ones of the openings for subsequently installing windows and doors. The attached elements form a step-tree surface upon which is wound an outer covering layer. The coach body thus manufactured is removed from the winding core, the blank covers are cut out for the door and window openings, apertures are formed in the inner covering layer for the feed and removal of air and openings are formed for mounting illumination devices in the ceiling wall. One or both of the covering layers can be formed with a sandwich type construction having a first winding layer, an insulation mat attached to an outer surface of the first winding layer, and a second winding layer wound over the insulation mat.
摘要翻译: 制造整体式教练体的方法包括以下步骤:将内覆盖层卷绕在体形卷绕芯上,并将多个U形通道段连接到天花板和地板壁的外表面,并将多个绝缘段 在身体的角落区域。 加强框架附接到主体的侧壁的外表面,绝缘板附接在加强框架中的一些矩形开口中,并且空白盖定位在其他开口中,用于随后安装窗户和门。 附着元件形成阶梯树表面,在其上缠绕外覆盖层。 将如此制造的车身主体从卷绕芯上移除,为了打开和关闭门窗,切割出坯料盖,在内层中形成孔,用于进料和除去空气,形成开口以将照明装置安装在 天花板墙。 覆盖层中的一个或两个可以形成为具有第一绕组层,附着到第一绕组层的外表面的绝缘垫和缠绕在绝缘垫上的第二绕组层的夹层结构。
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