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公开(公告)号：US10076883B2
公开(公告)日：2018-09-18
申请号：US14704804
申请日：2015-05-05
Applicant: The Boeing Company
Inventor： Charles R. Prebil , James R. Fox , Randall D. Wilkerson
IPC: B29C70/38 , B29C31/08 , G01B11/02 , B29C65/18 , B29C65/78 , B29C65/82 , B29C65/00 , B29K105/08 , B29B11/04 , B29C65/14 , B29C65/22 , B29C65/30 , B29C65/32
CPC classification number: B29C70/386 , B29B11/04 , B29C31/085 , B29C65/14 , B29C65/1412 , B29C65/18 , B29C65/224 , B29C65/305 , B29C65/32 , B29C65/7802 , B29C65/8253 , B29C66/0042 , B29C66/0062 , B29C66/1142 , B29C66/341 , B29C66/345 , B29C66/435 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/73921 , B29C66/8122 , B29C66/81261 , B29C66/81469 , B29C66/8169 , B29C66/8242 , B29C66/8322 , B29C66/836 , B29C66/84121 , B29C66/863 , B29C66/91221 , B29C66/91231 , B29C66/9161 , B29C66/9241 , B29C66/92431 , B29C66/934 , B29C66/944 , B29C66/961 , B29C70/20 , B29C70/38 , B29C70/50 , B29C70/545 , B29C2793/0081 , B29K2105/0881 , G01B11/028 , B29K2905/10 , B29K2277/10 , B29K2223/00 , B29K2305/00 , B29K2309/08 , B29K2307/04 , B29K2307/02 , B29K2309/02 , B29K2027/12 , B29K2077/00 , B29K2023/06 , B29K2067/003 , B29K2067/00 , B29K2023/12 , B29K2069/00 , B29K2075/00 , B29K2071/00 , B29K2079/085
Abstract: An off-axis prepreg material manufacturing machine may include a robot configured to position a prepreg piece adjacent to an end of a prepreg layer. The machine may additionally include an alignment system configured to sense a position of the prepreg piece relative to the prepreg layer and generate a position signal representative thereof. The machine may also include a controller configured to receive the position signal and cause the robot to adjust the position of the prepreg piece such that an end edge of the prepreg piece and an end edge of the prepreg layer are in substantially abutting contact.
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公开(公告)号：US09511538B2
公开(公告)日：2016-12-06
申请号：US13673989
申请日：2012-11-09
Applicant: The Boeing Company
Inventor： Alexander M. Rubin , James R. Fox , Randall D. Wilkerson
CPC classification number: B29C65/02 , B29C70/504 , B29C2793/00 , B29K2101/12 , B29L2009/00 , B29L2031/003 , B29L2031/766 , Y10T156/1002 , Y10T156/1008 , Y10T156/101 , Y10T156/1028 , Y10T156/1031 , Y10T156/1043 , Y10T156/1044
Abstract: A fabrication method of forming thermoplastic composite laminate parts with tailored and varying thickness in a continuous process. Automated equipment or hand lay-up are used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
Abstract translation: 在连续工艺中形成具有定制且变化的厚度的热塑复合层压件的制造方法。 使用自动化设备或手动堆叠将零件或组件整理成多层堆叠。 每个堆叠包含所有层，包括堆积层，在适当的位置固定以保持定位和位置。 层压固结工具包含所有必要的部件特征，并且与定制的多层叠层协调以形成潜在地具有与多层叠层厚度不同的区域的单个集成热塑性复合层压板。
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3.发明申请公开(公告)号：US20140014274A1
公开(公告)日：2014-01-16
申请号：US13934884
申请日：2013-07-03
Applicant: The Boeing Company
Inventor： Randall D. Wilkerson , James R. Fox , Alexander M. Rubin
IPC: B29D7/01
CPC classification number: B29D7/01 , B29C43/14 , B29C43/22 , B29C43/228 , B29C70/42 , B29C70/526 , B29C70/54 , B29K2105/08 , Y10T156/101 , Y10T156/1737
Abstract: Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
Abstract translation: 热塑性层压板在连续压塑生产线中制造。 将层压板层叠放置在承载工具上的凹槽中，并且该工具通过连续的成型操作在线上移动，包括预成形和固结操作。 该工具与管线末端的完全成型部分分离，可以重新使用。 携带工具的使用减少了材料废料。
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公开(公告)号：US20170080651A1
公开(公告)日：2017-03-23
申请号：US14861197
申请日：2015-09-22
Applicant: The Boeing Company
Inventor： Mike P. Matlack , Stephen J. Morgan , Thomas K. Tsotsis , James R. Fox , Randall D. Wilkerson
CPC classification number: B29C70/56 , B29C33/22 , B29C70/46 , B29K2101/12 , B29K2105/12
Abstract: A system and method for forming an item from a material, which may include elongated fibers and/or stretched broken fibers. The material is placed on a first clamping portion, which is placed on a fixture. A second clamping portion is placed against the material and the first clamping portion and secured together, forming a clamping assembly. The clamping assembly is removed from the fixture and placed on a first die portion, having a first profile. A second die portion is also provided, having a second profile. In forming the item, at least one of the first die portion and the second die portion are moved toward each other such that a second surface of the first die portion and a first surface of the second die portion contact and form the material into the item generally replicating the first profile and the second profile.
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公开(公告)号：US09545778B2
公开(公告)日：2017-01-17
申请号：US14451065
申请日：2014-08-04
Applicant: The Boeing Company
Inventor： Ryan Joseph Merriman , James R. Fox , Charles Richard Prebil , Steven J. Burpo
IPC: B32B37/00 , B32B37/10 , B32B37/14 , B29C70/44 , B29C65/00 , B29D99/00 , B64F5/00 , B29L31/30 , F16B11/00 , B29C65/48 , B29C65/50 , B29C65/02
CPC classification number: B32B37/0046 , B29C65/02 , B29C65/48 , B29C65/4815 , B29C65/5057 , B29C66/112 , B29C66/131 , B29C66/524 , B29C66/532 , B29C66/61 , B29C66/721 , B29C66/73752 , B29C66/742 , B29C66/8161 , B29C66/8322 , B29C66/8432 , B29C70/44 , B29D99/0014 , B29L2031/3082 , B32B37/10 , B32B37/14 , B32B2309/12 , B32B2605/18 , B64F5/10 , F16B11/006
Abstract: A mechanical pressure application system for applying a tailored pressure distribution to a plurality of structural components is provided. Each structural component has a first surface, and each first surface is configured to interface with the first surface of another of the structural components at a contact area. A base and at least one tooling block are configured to removably couple to the structural components. Each at least one tooling block includes a first surface configured to be positioned proximate at least one of the plurality of structural components. A second surface of each tooling block is configured to receive at least one forcing member. At least one biasing mechanism is configured to apply a predetermined load to the at least one forcing member, such that a force is transmitted from the at least one forcing member through the tooling block to a corresponding portion of the contact area.
Abstract translation: 提供了一种用于向多个结构部件施加定制的压力分布的机械压力施加系统。 每个结构部件具有第一表面，并且每个第一表面构造成在接触区域与另一个结构部件的第一表面相接合。 基座和至少一个工具块构造成可移除地联接到结构部件。 每个至少一个工具块包括构造成邻近多个结构部件中的至少一个定位的第一表面。 每个加工块的第二表面被配置成接收至少一个强制构件。 至少一个偏压机构构造成将预定负载施加到至少一个迫使构件，使得力从至少一个强制构件通过工具块传递到接触区域的相应部分。
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Patent Agency Ranking
公开(公告)号：US20160325509A1
公开(公告)日：2016-11-10
申请号：US14704804
申请日：2015-05-05
Applicant: The Boeing Company
Inventor： Charles R. Prebil , James R. Fox , Randall D. Wilkerson
IPC: B29C70/38
CPC classification number: B29C70/386 , B29B11/04 , B29C31/085 , B29C65/14 , B29C65/1412 , B29C65/18 , B29C65/224 , B29C65/305 , B29C65/32 , B29C65/7802 , B29C65/8253 , B29C66/0042 , B29C66/0062 , B29C66/1142 , B29C66/341 , B29C66/345 , B29C66/435 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/73921 , B29C66/8122 , B29C66/81261 , B29C66/81469 , B29C66/8169 , B29C66/8242 , B29C66/8322 , B29C66/836 , B29C66/84121 , B29C66/863 , B29C66/91221 , B29C66/91231 , B29C66/9161 , B29C66/9241 , B29C66/92431 , B29C66/934 , B29C66/944 , B29C66/961 , B29C70/38 , B29C2793/0081 , B29K2105/0881 , G01B11/028 , B29K2905/10 , B29K2277/10 , B29K2223/00 , B29K2305/00 , B29K2309/08 , B29K2307/04 , B29K2307/02 , B29K2309/02 , B29K2027/12 , B29K2077/00 , B29K2023/06 , B29K2067/003 , B29K2067/00 , B29K2023/12 , B29K2069/00 , B29K2075/00 , B29K2071/00 , B29K2079/085
Abstract: An off-axis prepreg material manufacturing machine may include a robot configured to position a prepreg piece adjacent to an end of a prepreg layer. The machine may additionally include an alignment system configured to sense a position of the prepreg piece relative to the prepreg layer and generate a position signal representative thereof. The machine may also include a controller configured to receive the position signal and cause the robot to adjust the position of the prepreg piece such that an end edge of the prepreg piece and an end edge of the prepreg layer are in substantially abutting contact.
Abstract translation: 离轴预浸料材料制造机器可以包括机器人，其被配置为将预浸料片与预浸料层的端部相邻定位。 该机器可以另外包括对准系统，该对准系统构造成感测预浸料坯件相对于预浸料层的位置，并产生代表其的位置信号。 机器还可以包括控制器，其被配置为接收位置信号并使机器人调节预浸料坯件的位置，使得预浸料坯件的端边缘和预浸料层的端边缘基本上邻接接触。
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公开(公告)号：US20160031199A1
公开(公告)日：2016-02-04
申请号：US14451065
申请日：2014-08-04
Applicant: The Boeing Company
Inventor： Ryan Joseph Merriman , James R. Fox , Charles Richard Prebil , Steven J. Burpo
CPC classification number: B32B37/0046 , B29C65/02 , B29C65/48 , B29C65/4815 , B29C65/5057 , B29C66/112 , B29C66/131 , B29C66/524 , B29C66/532 , B29C66/61 , B29C66/721 , B29C66/73752 , B29C66/742 , B29C66/8161 , B29C66/8322 , B29C66/8432 , B29C70/44 , B29D99/0014 , B29L2031/3082 , B32B37/10 , B32B37/14 , B32B2309/12 , B32B2605/18 , B64F5/10 , F16B11/006
Abstract: A mechanical pressure application system for applying a tailored pressure distribution to a plurality of structural components is provided. Each structural component has a first surface, and each first surface is configured to interface with the first surface of another of the structural components at a contact area. A base and at least one tooling block are configured to removably couple to the structural components. Each at least one tooling block includes a first surface configured to be positioned proximate at least one of the plurality of structural components. A second surface of each tooling block is configured to receive at least one forcing member. At least one biasing mechanism is configured to apply a predetermined load to the at least one forcing member, such that a force is transmitted from the at least one forcing member through the tooling block to a corresponding portion of the contact area.
Abstract translation: 提供了一种用于向多个结构部件施加定制的压力分布的机械压力施加系统。 每个结构部件具有第一表面，并且每个第一表面构造成在接触区域与另一个结构部件的第一表面相接合。 基座和至少一个工具块构造成可移除地联接到结构部件。 每个至少一个工具块包括构造成邻近多个结构部件中的至少一个定位的第一表面。 每个加工块的第二表面被配置成接收至少一个强制构件。 至少一个偏压机构构造成将预定负载施加到至少一个迫使构件，使得力从至少一个强制构件通过工具块传递到接触区域的相应部分。
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公开(公告)号：US11524471B2
公开(公告)日：2022-12-13
申请号：US16660398
申请日：2019-10-22
Applicant: The Boeing Company
Inventor： Charles R. Prebil , James R. Fox
IPC: B29C70/50 , B29C70/34 , B29C53/22 , B29C53/08 , B29K101/00 , B29L31/00 , B29L9/00 , B29K101/12 , B64C1/00 , B64C1/06
Abstract: A system and method for forming a composite part. The apparatus comprises a sleeve that molds a composite material. The sleeve has a first face and a second face. The second face has features to mold the composite material. The first face comprises a first inclined surface having an angle less than about 90 degrees and greater than about 0 degrees.
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公开(公告)号：US20180154596A1
公开(公告)日：2018-06-07
申请号：US15831388
申请日：2017-12-04
Applicant: The Boeing Company
Inventor： Randall D. Wilkerson , James R. Fox , Alexander M. Rubin
IPC: B29D7/01 , B29C43/22 , B29C70/52 , B29C70/54 , B29K105/08
CPC classification number: B29D7/01 , B29C43/14 , B29C43/22 , B29C43/228 , B29C70/42 , B29C70/526 , B29C70/54 , B29K2105/08 , Y10T156/101 , Y10T156/1737
Abstract: Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.
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公开(公告)号：US09545761B2
公开(公告)日：2017-01-17
申请号：US14182215
申请日：2014-02-17
Applicant: The Boeing Company
Inventor： Charles R. Prebil , James R. Fox , Alexander M. Rubin , Randall D. Wilkerson
CPC classification number: B29C70/526 , B29C33/306 , B29C43/222 , B29C43/36 , B29C43/44 , B29C2043/3665 , B29D99/0003
Abstract: A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.
Abstract translation: 装置改变用于压缩模制零件的模具的形状。 该装置包括放置在模具和待模制的电荷之间的套筒。 套筒具有大致与模具的表面相一致的内表面和用于模制零件的外表面。
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