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公开(公告)号:US20240123696A1
公开(公告)日:2024-04-18
申请号:US18392746
申请日:2023-12-21
申请人: Zephyros, Inc.
发明人: Henry E. Richardson
CPC分类号: B29C70/52 , B29C44/00 , B29C44/04 , B29C44/186 , B29C65/48 , B62D29/002 , B29C70/72
摘要: A structural member (10) comprising: (i) a pultruded secondary member (14) including a first surface and an opposing second surface: and (ii) a molded carrier (12) overmolded onto at least one of the first and second surface of the pultruded secondary member, the molded carrier including a plurality of ribs (16); wherein the secondary member and the carrier are dissimilar materials.
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公开(公告)号:US11938655B2
公开(公告)日:2024-03-26
申请号:US16772502
申请日:2018-12-13
发明人: Eita Konno , Taito Ueda , Mayuka Yamada
IPC分类号: C08J5/24 , B29B11/16 , B29B15/12 , B29C70/20 , B29C70/52 , B32B5/26 , B32B5/28 , B29K77/00 , B29K101/12 , B29K105/08 , B29K307/04
CPC分类号: B29B15/122 , B29B11/16 , B29C70/20 , B29C70/52 , B29C70/521 , B29C70/528 , B32B5/26 , C08J5/243 , B29B15/12 , B29K2077/00 , B29K2101/12 , B29K2105/0872 , B29K2105/0881 , B29K2307/04 , B32B2307/538 , C08J2377/00 , Y10T428/24994 , Y10T428/249942 , Y10T428/249944 , Y10T428/249945 , Y10T428/31
摘要: The invention aims to provide a tape-shaped prepreg including unidirectionally oriented reinforcing fibers and a thermoplastic resin composition and being high in handleability during molding and high in adhesiveness to other members. The tape-shaped prepreg includes unidirectionally oriented reinforcing fibers and a thermoplastic resin composition and has an arithmetic average roughness (Ra) of 0.1 to 10 μm in a direction perpendicular to the orientation direction of the reinforcing fibers, as measured according to JIS B 0601: 2013, and a warpage rate of 5% or less as determined by the procedure specified in (i) to (iii) below: (i) place a test piece of the above tape-shaped prepreg having a length of 100 mm in the fiber orientation direction on a plane in such manner that the end portions curl upward, (ii) measure the vertical distance from the highest position at the right end of the curled tape to the plane, which is denoted by a, and the vertical distance from the highest position at the left end to the plane, which is denoted by b, and calculate the arithmetic average of a and b, which is defined as the warpage distance, and (iii) calculate the warpage rate by the following equation: warpage rate (%)=warpage distance (mm)/100 (mm)×100.
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公开(公告)号:US11738493B2
公开(公告)日:2023-08-29
申请号:US17242014
申请日:2021-04-27
IPC分类号: B23P19/10 , B32B27/02 , B33Y10/00 , B29C48/05 , B29C63/00 , B64C11/16 , B64C3/00 , B29C70/52 , B29C64/118 , B29C33/38 , B64F5/10 , B29C65/78 , B29C65/00 , B25B11/02 , B29C70/54 , B29K105/10 , B29K105/14 , B29L31/00 , B29L31/08 , B29L31/30
CPC分类号: B29C48/05 , B25B11/02 , B29C33/3842 , B29C63/0069 , B29C64/118 , B29C65/78 , B29C65/7802 , B29C66/721 , B29C66/7311 , B29C66/73111 , B29C66/73112 , B29C70/52 , B29C70/541 , B29C70/543 , B32B27/02 , B64C3/00 , B64C11/16 , B64F5/10 , B23P2700/01 , B29K2105/106 , B29K2105/14 , B29K2995/0044 , B29L2031/08 , B29L2031/082 , B29L2031/3076 , B29L2031/3079 , B29L2031/3082 , B29L2031/3085 , B29L2031/3088 , B29L2031/757 , B32B2262/0215
摘要: In one embodiment, a method includes fastening a plurality of components of a composite structure in an assembly fixture, wherein the assembly fixture comprises a plurality of strands of a fiber-reinforced thermoplastic material, wherein the fiber-reinforced thermoplastic material comprises a thermoplastic embedded with a plurality of reinforcement fibers, wherein the plurality of reinforcement fibers is aligned within each strand of the plurality of strands, and wherein the assembly fixture further comprises an anisotropic thermal expansion property based on an orientation of the plurality of reinforcement fibers within the assembly fixture; and heating the assembly fixture in an autoclave to bond the plurality of components of the composite structure.
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公开(公告)号:US20230191725A1
公开(公告)日:2023-06-22
申请号:US17925345
申请日:2021-05-17
申请人: Moba Group B.V.
CPC分类号: B29C70/52 , A01K43/00 , B29C45/14598 , B29C45/14631 , B29C70/086
摘要: The present invention relates to a device, for example a machine part, comprising:—a body with a cylinder shape of substantially carbon fibers with the fibers in the longitudinal direction of the cylinder shape, the body functioning as carrier body with a carrier surface, and—at least a single circumferential body of a plastic provided through injection molding on the body, the circumferential body being provided on at least a part of the carrier surface. Further, the present invention concerns a method for manufacturing the device, comprising:—manufacturing with pultrusion the cylinder shape of substantially carbon reinforced fiber material with carbon fibers substantially in the longitudinal direction of the cylinder shape, and—injection molding of a plastic on the cylinder shape for obtaining the circumferential body on at least a part of the carrier surface.
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公开(公告)号:US20230182405A1
公开(公告)日:2023-06-15
申请号:US17926464
申请日:2021-06-04
申请人: LM WIND POWER A/S
发明人: Thomas MERZHAEUSER
CPC分类号: B29C70/08 , B29C70/52 , F03D1/0675 , B29K2307/04
摘要: A pultruded fibre-reinforced strip (50) configured to be stacked with one or more similar strips (50) to form a spar cap of a wind turbine blade (10), comprising—a core (51) comprising a plurality of first fibres embedded in a resin matrix, the plurality of first fibres being carbon fibres and/or glass fibres, and—a surface layer (52) enclosing and covering the core (51) and comprising a plurality of second fibres imbedded in the resin matrix, the majority of the plurality of second fibres having an elastic modulus less than 10 GPa.
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公开(公告)号:US20190009477A1
公开(公告)日:2019-01-10
申请号:US15642585
申请日:2017-07-06
申请人: The Boeing Company
发明人: Christian Gordon
CPC分类号: B29C70/34 , B29B11/16 , B29C65/4815 , B29C70/52 , B29C70/545 , B29C2793/0036 , B29C2793/0063 , B29D99/0003 , B29L2031/3082 , B32B3/28 , B32B37/142
摘要: A method of manufacturing a noodle of a structural joint that comprises pulling a first composite sheet through a first splitting station to cut the first composite sheet into a plurality of first composite plies, pulling the plurality of first composite plies through a first alignment station to stack the plurality of first composite plies on top of each other to form a first stacked composite layup, pulling the first stacked composite layup through a first heating station to heat the first stacked composite layup to form a first heated composite layup, pulling the first heated composite layup through a first forming station to shape the first heated composite layup into a first pre-selected cross-sectional shape to form at least a first portion of a continuous noodle, and pulling at least the first portion of the continuous noodle through a cutting station to cut at least the first portion of the continuous noodle to a pre-selected length.
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公开(公告)号:US20180252202A1
公开(公告)日:2018-09-06
申请号:US15447248
申请日:2017-03-02
CPC分类号: B29C70/342 , B29C70/52 , B29L2031/085 , F03D1/0675 , F05B2230/31 , F05B2240/221 , F05B2280/6013 , F05B2280/6015 , Y02E10/721 , Y02P70/523
摘要: The present disclosure is directed to a method of manufacturing a rotor blade component of a wind turbine is disclosed. The method includes placing at least one first pultruded member into a curved rotor blade component mold. More specifically, the first pultruded member includes at least one design characteristic configured to allow the first pultruded member to sit substantially flush against an inner surface of the curved rotor blade component mold. The method also includes placing at least one second pultruded member atop the at least one first pultruded member and infusing the first and second pultruded members together to form the rotor blade component.
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公开(公告)号:US20170368768A1
公开(公告)日:2017-12-28
申请号:US15699101
申请日:2017-09-08
IPC分类号: B29C70/52 , B29C51/14 , B29C51/20 , B29C51/26 , B29C51/42 , B29C51/46 , E04B1/32 , G05B19/4099 , B29C43/22 , B29C59/04 , B29C47/88 , B29C43/48 , B29K101/12 , B29L31/08 , B29L31/30 , B29C53/04 , B29C33/02
CPC分类号: B29C70/526 , B29C33/026 , B29C43/228 , B29C43/48 , B29C47/885 , B29C51/14 , B29C51/20 , B29C51/261 , B29C51/264 , B29C51/421 , B29C51/46 , B29C53/043 , B29C59/043 , B29C70/52 , B29C70/521 , B29C70/522 , B29C70/523 , B29C70/525 , B29C70/527 , B29C70/528 , B29C2043/483 , B29K2101/12 , B29L2031/08 , B29L2031/3076 , E04B1/32 , E04B2001/3223 , G05B19/4099 , G05B2219/49007
摘要: A 3D thermoplastic pultrusion system and method based upon a 3D variable die system and including one or more sets of 3D thermoplastic forming machines to continuously produce thermoplastic composite pultrusions with at least one of varying cross-section geometry and constant surface contours, varying cross-section geometry and varying surface contours, and constant cross-section geometry and varying surface contours. The 3D thermoplastic pultrusion system and method including at least one of one or more pairs of shapeable and flexible dual-temperature bands and a rotating assembly that rotates the one or more sets of 3D thermoplastic forming machines to impart a twist to the thermoplastic composite.
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公开(公告)号:US20170297251A1
公开(公告)日:2017-10-19
申请号:US15285165
申请日:2016-10-04
申请人: CC3D LLC
发明人: Kenneth Lyle Tyler
IPC分类号: B29C47/12 , B29C35/02 , B29C35/08 , B29B15/12 , B29C47/00 , B29C47/24 , B29L23/00 , B29K105/08
CPC分类号: B29C47/128 , B05B3/001 , B05B3/1007 , B05B5/032 , B05B5/04 , B05B7/1481 , B05B13/0636 , B05D3/061 , B29B15/122 , B29C35/0261 , B29C35/0805 , B29C47/0023 , B29C47/0038 , B29C47/0042 , B29C47/0066 , B29C47/022 , B29C47/065 , B29C47/0867 , B29C47/1045 , B29C47/20 , B29C47/22 , B29C47/24 , B29C64/106 , B29C64/209 , B29C64/264 , B29C70/388 , B29C70/50 , B29C70/52 , B29C70/521 , B29C70/523 , B29C70/526 , B29C2035/0827 , B29D23/00 , B29K2105/08 , B29L2023/00 , B29L2023/22 , B33Y30/00
摘要: A head is disclosed for use with a manufacturing system. The head may have a housing configured to discharge a tubular structure reinforced with at least one continuous fiber and having a three-dimensional trajectory, and a cure enhancer operatively connected to the housing and configured to cure a liquid matrix in the tubular structure during discharge. The head may also have a nozzle configured to discharge a fill material into the tubular structure, and a wand extending from the housing to the nozzle.
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公开(公告)号:US20170252988A1
公开(公告)日:2017-09-07
申请号:US15503857
申请日:2015-08-17
CPC分类号: B29C70/521 , B29B11/06 , B29B11/16 , B29B15/122 , B29C70/52 , B29K2023/12 , B29K2307/04
摘要: Provided are a process and an apparatus for producing a fiber-reinforced thermoplastic resin tape, the process and the apparatus being capable of preventing fiber cut from occurring at the start of production of the fiber-reinforced thermoplastic resin tape. The provided process includes a resin impregnation step of opening a fiber bundle and impregnating the fiber bundle with molten thermoplastic resin and a through-nozzle passing step of passing the fiber bundle having undergone the resin impregnation step through a slit formed in a nozzle. The through-nozzle passing step includes setting, at the start of production, a gap dimension of the slit to a dimension larger than a normal dimension and changing the gap dimension of the slit to the normal dimension when a predetermined condition is satisfied, after the production start.
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