-
1.发明申请
公开(公告)号：WO2010101744A3
公开(公告)日：2010-12-16
申请号：PCT/US2010025176
申请日：2010-02-24
Applicant: BOEING CO , PREBIL CHARLES R , FOX JAMES R , RUBIN ALEXANDER M , WILKERSON RANDALL D
Inventor： PREBIL CHARLES R , FOX JAMES R , RUBIN ALEXANDER M , WILKERSON RANDALL D
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 (22) used to compression mold a part. The device includes a sleeve (24) placed between the die and a charge to be molded. The sleeve (24) has an inner face (65) generally conforming to a face of the die, and an outer face (67) for molding a part.
Abstract translation: 装置改变用于压缩模制零件的模具（22）的形状。 该装置包括放置在模具和要模制的电荷之间的套筒（24）。 套筒（24）具有通常与模具的表面相一致的内表面（65）和用于模制零件的外表面（67）。
-
2.发明申请
公开(公告)号：WO2008073164A3
公开(公告)日：2008-06-19
申请号：PCT/US2007/018611
申请日：2007-08-22
Applicant: THE BOEING COMPANY , RUBIN, Alexander M. , FOX, James R. , WILKERSON, Randall D.
Inventor： RUBIN, Alexander M. , FOX, James R. , WILKERSON, Randall D.
Abstract: A fabrication method of forming curved thermoplastic composite laminate parts with tailored and varying thickness in a continuous process and a curved thermoplastic laminate part obtained thereby. Automated equipment or hand lay-up are used to collate parts or components into, a multi-layer stack (226). Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Ply consolidation tooling (275, 284) 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.
-
公开(公告)号：WO2007092371A2
公开(公告)日：2007-08-16
申请号：PCT/US2007/003021
申请日：2007-02-02
Applicant: THE BOEING COMPANY , RUBIN, Alexander, M. , FOX, James, R. , WILKERSON, Randall, D.
Inventor： RUBIN, Alexander, M. , FOX, James, R. , WILKERSON, Randall, D.
IPC: B29D99/00
CPC classification number: B29D99/0007 , B29C70/525 , B29C70/545 , B29K2101/12 , Y02T50/43 , Y10T156/10 , Y10T156/1002 , Y10T156/1007 , Y10T156/1008 , Y10T156/101 , Y10T156/1011 , Y10T156/1028 , Y10T156/1034 , Y10T156/1043 , Y10T156/1044 , Y10T156/1046 , Y10T156/1049 , Y10T156/1051 , Y10T156/1075 , Y10T156/1077 , Y10T156/1079
Abstract: A fabrication method of forming a thermoplastic composite laminate material with tailored and varying thickness in a continuous process. This process utilizes automated equipment or hand lay-up 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. The 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 10 differing thickness from these multiple ply stacks.
Abstract translation: 一种在连续工艺中形成具有定制且变化的厚度的热塑性复合层压材料的制造方法。 该过程利用自动化设备或手工铺层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。 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单个集成的热塑复合层压材料，潜在地具有与这些多层堆叠不同厚度的区域。
-
公开(公告)号：WO2011106117A1
公开(公告)日：2011-09-01
申请号：PCT/US2011/022003
申请日：2011-01-21
Applicant: THE BOEING COMPANY , RUBIN, Alexander, M. , FOX, James, R. , WILKERSON, Randall, D.
Inventor： RUBIN, Alexander, M. , FOX, James, R. , WILKERSON, Randall, D.
CPC classification number: B29C53/04 , B29L2031/003 , Y10T156/1007 , Y10T156/1013 , Y10T428/24 , Y10T428/24744
Abstract: An elongate thermoplastic composite member (20) is fabricated by a continuous molding process. A pre - consolidated thermoplastic laminate is softened by heating it to a temperature below its melting layup, and is fed substantially continuously through multiple sets of tool dies. The tool dies incrementally mold portions of softened laminate over a mandrel to form the laminate into a shape having a closed cross section.
Abstract translation: 通过连续成型工艺制造细长的热塑性复合材料（20）。 通过将预固化的热塑性层压体加热到低于其熔融铺层的温度来软化，并且通过多组工具模具基本连续地进料。 该软件在心轴上逐渐模制软化层压板的模制部分，以将层压体形成为具有封闭横截面的形状。
-
Patent Agency Ranking5.发明申请THERMOPLASTIC COMPOSITE PARTS HAVING INTEGRATED METAL FITTINGS AND METHOD OF MAKING THE SAME 审中-公开具有集成金属配件的热塑性复合材料及其制造方法
公开(公告)号：WO2008094227A1
公开(公告)日：2008-08-07
申请号：PCT/US2007/022234
申请日：2007-10-17
Applicant: THE BOEING COMPANY , RUBIN, Alexander, M. , WILKERSON, Randall, D. , FOX, James, R.
Inventor： RUBIN, Alexander, M. , WILKERSON, Randall, D. , FOX, James, R.
CPC classification number: B29C70/34 , B29C70/50 , B29C70/525 , B29C70/545 , B29C70/86 , B29C70/885 , B29D99/0007 , B29K2101/12 , B32B3/085 , B32B15/08 , B32B27/08 , B32B27/285 , B32B27/286 , B32B27/288 , B32B2262/101 , B32B2262/106 , B32B2605/003 , B32B2605/18 , Y10T156/1002
Abstract: Thermoplastic composite parts having integrated metal fittings (342, 343, 350) are manufactured using a continuous compression molding process. Automated equipment or hand lay-up are used to collate composite material plies and metal fittings 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. Multiple lay-ups may be cut from each stack. The lay-ups (345) are placed in tooling containing part features and are continuously fed through a performing station where the lay-ups are preformed into the approximate shape of the finished part. Following pre-forming, the tooling is moved incrementally through a consolidation station where a compression press (354, 356) presses successive sections of the tooling to form a single integrated thermoplastic composite laminate part having integrated metal fittings, which may include areas of differing thickness.
Abstract translation: 具有集成金属配件（342,343,350）的热塑性复合材料部件使用连续压缩成型工艺制造。 自动化设备或手工铺层用于将复合材料层和金属配件整理成多层堆叠。 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。 可以从每个堆叠中切割多个叠层。 叠层（345）被放置在包含零件特征的模具中，并且连续地通过执行站进给，其中叠层被预成形为成品的近似形状。 在预成形之后，模具通过压实压机（354,356）压缩模具的连续部分以形成具有集成金属配件的单个集成热塑复合材料层压件部件的固结工位逐渐移动，该组合材料可以包括不同厚度的区域 。
-
6.发明申请
公开(公告)号：WO2010101744A2
公开(公告)日：2010-09-10
申请号：PCT/US2010/025176
申请日：2010-02-24
Applicant: THE BOEING COMPANY , PREBIL, Charles R. , FOX, James R. , RUBIN, Alexander M. , WILKERSON, Randall D.
Inventor： PREBIL, Charles R. , FOX, James R. , RUBIN, Alexander M. , WILKERSON, Randall D.
IPC: B29C43/36
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。
-
7.发明申请
公开(公告)号：WO2008097847A1
公开(公告)日：2008-08-14
申请号：PCT/US2008/052806
申请日：2008-02-01
Applicant: THE BOEING COMPANY , WILKERSON, Randall, D. , FOX, James, R. , RUBIN, Alexander, M.
Inventor： WILKERSON, Randall, D. , FOX, James, R. , RUBIN, Alexander, M.
CPC classification number: B29D7/01 , B29C43/22 , B29C43/228 , 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。
-
公开(公告)号：WO2008073164A2
公开(公告)日：2008-06-19
申请号：PCT/US2007018611
申请日：2007-08-22
Applicant: BOEING CO , RUBIN ALEXANDER M , FOX JAMES R , WILKERSON RANDALL D
Inventor： RUBIN ALEXANDER M , FOX JAMES R , WILKERSON RANDALL D
IPC: B29D99/00
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 curved 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弯曲热塑复合层压件部件的制造方法。 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。
-
9.发明申请FABRICATION PROCESS FOR THERMOPLASTIC COMPOSITE PARTS AND PRODUCTS OBTAINED THEREBY 审中-公开热塑性复合材料的制造工艺及其获得的产品
公开(公告)号：WO2007092371A3
公开(公告)日：2007-12-06
申请号：PCT/US2007003021
申请日：2007-02-02
Applicant: BOEING CO , RUBIN ALEXANDER M , FOX JAMES R , WILKERSON RANDALL D
Inventor： RUBIN ALEXANDER M , FOX JAMES R , WILKERSON RANDALL D
CPC classification number: B29D99/0007 , B29C70/525 , B29C70/545 , B29K2101/12 , Y02T50/433 , Y10T156/10 , Y10T156/1002 , Y10T156/1007 , Y10T156/1008 , Y10T156/101 , Y10T156/1011 , Y10T156/1028 , Y10T156/1034 , Y10T156/1043 , Y10T156/1044 , Y10T156/1046 , Y10T156/1049 , Y10T156/1051 , Y10T156/1075 , Y10T156/1077 , Y10T156/1079
Abstract: A fabrication method of forming a thermoplastic composite laminate material (20) with tailored and varying thickness (tl, t2) in a continuous process. This process utilizes automated equipment or hand lay-up to collate parts or components into a multi-layer stack (74, 76). Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. The 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 10 differing thickness from these multiple ply stacks.
Abstract translation: 一种在连续工艺中形成具有定制且变化的厚度（t1，t2）的热塑复合层压材料（20）的制造方法。 该过程利用自动化设备或手工铺层将部件或组件整理成多层堆叠（74,76）。 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。 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单个集成的热塑复合层压材料，潜在地具有与这些多层堆叠不同厚度的区域。
-
-
-
-
-
-
-
-
Search Results
9
records
(took 0.009 seconds)
