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公开(公告)号:US10086548B2
公开(公告)日:2018-10-02
申请号:US15470304
申请日:2017-03-27
申请人: The Boeing Company
IPC分类号: B29C47/02 , B29C47/92 , B29C47/00 , B29C70/00 , B64C1/06 , B29D99/00 , B29L31/30 , B29K105/16 , B29C65/00 , B29C47/08 , B29C47/10 , B29C47/36 , B29C47/76 , B29C47/78 , B29C47/82 , B29C65/02 , B64C1/00 , B29K105/12 , B29K105/10
摘要: A thermoplastic composite structure is produced by extruding a bead of composite material to a desired cross sectional shape. An extruder extrudes the polymer bead containing reinforcing fibers, using a low compression first extruder stage where the polymer is mixed and de-gassed, and a high compression second stage where the polymer is consolidated and extruded. The cross sectional profile of the polymer bead may be altered using a variable extruder gate.
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公开(公告)号:US10780680B2
公开(公告)日:2020-09-22
申请号:US16135768
申请日:2018-09-19
申请人: THE BOEING COMPANY
IPC分类号: B32B27/30 , B32B27/38 , B32B27/28 , C08J5/04 , B64C1/06 , B29C39/00 , D04H1/00 , B29L31/30 , B29C65/00 , B29C65/02
摘要: A composite radius filler material is provided. The composite radius filler includes a resin, a first group of fibers dispersed within the resin, and a second group of fibers dispersed within the resin. The first group of fibers has a first length configured to facilitate orientation in a longitudinal direction. The second group of fibers has a second length that is shorter than the first length, with the second group of fibers configured to facilitate random orientation in a transverse direction.
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公开(公告)号:US20170029579A1
公开(公告)日:2017-02-02
申请号:US14812321
申请日:2015-07-29
申请人: THE BOEING COMPANY
CPC分类号: B32B27/30 , B29C65/02 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/43441 , B29C66/474 , B29C66/496 , B29C66/524 , B29C66/5326 , B29C66/54 , B29C66/636 , B29C66/721 , B29C66/73752 , B29L2031/3082 , B32B27/28 , B32B27/38 , B32B2250/40 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B64C1/064 , C08J5/047 , C08J2339/04 , C08J2363/00 , C08J2365/02 , C08J2379/02 , D04H1/00
摘要: A composite radius filler material is provided. The composite radius filler includes a resin, a first group of fibers dispersed within the resin, and a second group of fibers dispersed within the resin. The first group of fibers has a first length configured to facilitate orientation in a longitudinal direction. The second group of fibers has a second length that is shorter than the first length, with the second group of fibers configured to facilitate random orientation in a transverse direction.
摘要翻译: 提供复合半径填料。 复合半径填料包括树脂,分散在树脂内的第一组纤维和分散在树脂内的第二组纤维。 第一组纤维具有构造成有助于沿纵向取向的第一长度。 第二组纤维具有比第一长度短的第二长度,其中第二组纤维被配置成便于在横向上的随机取向。
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公开(公告)号:US20190152120A1
公开(公告)日:2019-05-23
申请号:US16255724
申请日:2019-01-23
申请人: The Boeing Company
发明人: Weidong Song , Daniel J. Perron , Stephen G. Moore , Jamie J. Langabeer , Jonathan D. Robbins , Jeffrey Olberg
IPC分类号: B29C48/92 , B29C48/02 , B64C1/06 , B29D99/00 , B29C48/155
摘要: A system for depositing a composite filler material into a channel of a composite structure includes an end-effector configured to extrude a bead of the filler material into the channel. The filler material can comprise a first group of relatively long fibers, a second group of relatively short fibers and a resin. A drive system is configured to move the end-effector relative to the channel, and a position sensor is configured to detect the position of the bead relative to the channel. A controller is configured to operate the drive system in response to the detected position and to operate the end-effector to heat and compress the filler material so as to orient the longer fibers in a substantially longitudinal direction relative to the channel and the shorter fibers in substantially random directions relative to the channel when the bead is extruded into the channel.
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公开(公告)号:US20190016103A1
公开(公告)日:2019-01-17
申请号:US16135768
申请日:2018-09-19
申请人: THE BOEING COMPANY
CPC分类号: B32B27/30 , B29C39/00 , B29C65/02 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/43441 , B29C66/474 , B29C66/496 , B29C66/524 , B29C66/5326 , B29C66/54 , B29C66/636 , B29C66/721 , B29C66/73752 , B29L2031/3082 , B32B27/28 , B32B27/38 , B32B2250/40 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B64C1/064 , C08J5/047 , C08J2339/04 , C08J2363/00 , C08J2365/02 , C08J2379/02 , D04H1/00
摘要: A composite radius filler material is provided. The composite radius filler includes a resin, a first group of fibers dispersed within the resin, and a second group of fibers dispersed within the resin. The first group of fibers has a first length configured to facilitate orientation in a longitudinal direction. The second group of fibers has a second length that is shorter than the first length, with the second group of fibers configured to facilitate random orientation in a transverse direction.
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公开(公告)号:US10099456B2
公开(公告)日:2018-10-16
申请号:US14812321
申请日:2015-07-29
申请人: THE BOEING COMPANY
摘要: A composite radius filler material is provided. The composite radius filler includes a resin, a first group of fibers dispersed within the resin, and a second group of fibers dispersed within the resin. The first group of fibers has a first length configured to facilitate orientation in a longitudinal direction. The second group of fibers has a second length that is shorter than the first length, with the second group of fibers configured to facilitate random orientation in a transverse direction.
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公开(公告)号:US11305859B2
公开(公告)日:2022-04-19
申请号:US15938175
申请日:2018-03-28
申请人: The Boeing Company
发明人: Weidong Song , Gerard J. Gallo , Gwen Marie Lanphere Gross , Jamie J. Langabeer , Jason J. McBain , Stephen L. Metschan , Jeffrey H. Olberg , Max M. Osborne , Richard V. Phillips , Paul D. Evans , Hugh A. Yap , Nicholas J. Zayas
摘要: A method for forming a composite structure includes the steps of: forming a fiber-reinforced polymer paste to a shape of a cavity of a dry fiber preform structure; heating said dry fiber preform structure having said fiber-reinforced polymer in said cavity to an infusion temperature; infusing resin into said dry fiber preform structure and around said fiber-reinforced polymer; and curing said resin-infused fiber preform structure and said fiber-reinforced polymer at a cure temperature higher than said infusion temperature.
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公开(公告)号:US20190308356A1
公开(公告)日:2019-10-10
申请号:US15948831
申请日:2018-04-09
申请人: The Boeing Company
发明人: Fei Cai , Weidong Song , Jamie J. Langabeer , Steven A. Solack , Adam DeVries , Kyler J. Kamyszek
摘要: An apparatus (100) for depositing a radius filler (102), made of a homogeneous material, into a groove (104), formed in a workpiece (106) comprises a chassis (110), first means (120) for extruding the radius filler (102) along an extrusion axis (112), second means (130) for providing the homogeneous material to the first means (120), and third means (140) for compacting the radius filler (102) in the groove (104). The apparatus (100) also comprises a first sensor (150) configured to provide first-sensor output. The apparatus (100) further comprises a controller (180), operatively coupled to the first means (120), the second means (130), and the first sensor (150). Based on the first-sensor output, the controller (180) is configured to determine the first geometric characteristics of the groove (104). In addition, based on the first geometric characteristics, the controller (180) is configured to control second geometric characteristics of the radius filler (102), extruded by the first means (120), as the tool center point (122) is moved relative to the groove (104).
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公开(公告)号:US20190300141A1
公开(公告)日:2019-10-03
申请号:US15938175
申请日:2018-03-28
申请人: The Boeing Company
发明人: Weidong Song , Gerard J. Gallo , Gwen Marie Lanphere Gross , Jamie J. Langabeer , Jason J. McBain , Stephen L. Metschan , Jeffrey H. Olberg , Max M. Osborne , Richard V. Phillips , Paul D. Evans , Hugh A. Yap , Nicholas J. Zayas
摘要: A method for forming a composite structure includes the steps of: forming a fiber-reinforced polymer paste to a shape of a cavity of a dry fiber preform structure; heating said dry fiber preform structure having said fiber-reinforced polymer in said cavity to an infusion temperature; infusing resin into said dry fiber preform structure and around said fiber-reinforced polymer; and curing said resin-infused fiber preform structure and said fiber-reinforced polymer at a cure temperature higher than said infusion temperature.
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公开(公告)号:US10195779B2
公开(公告)日:2019-02-05
申请号:US14812223
申请日:2015-07-29
申请人: The Boeing Company
发明人: Weidong Song , Daniel J. Perron , Stephen G. Moore , Jamie J. Langabeer , Jonathan D. Robbins , Jeffrey Olberg
IPC分类号: B29C47/92 , B29C47/02 , B29C47/00 , B64C1/06 , B29D99/00 , B29L31/30 , B29K105/16 , B29C47/08 , B29C47/10 , B29C47/36 , B29C47/76 , B29C47/78 , B29C47/82 , B29K105/12 , B29C65/00 , B29C65/02 , B64C1/00
摘要: A system for depositing a composite filler material into a channel of a composite structure includes an end-effector configured to extrude a bead of the filler material into the channel. The filler material can comprise a first group of relatively long fibers, a second group of relatively short fibers and a resin. A drive system is configured to move the end-effector relative to the channel, and a position sensor is configured to detect the position of the bead relative to the channel. A controller is configured to operate the drive system in response to the detected position and to operate the end-effector to heat and compress the filler material so as to orient the longer fibers in a substantially longitudinal direction relative to the channel and the shorter fibers in substantially random directions relative to the channel when the bead is extruded into the channel.
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