专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US09156239B2 Method of manufacturing net edge core and a method of bonding net edge core to a substructure 有权
标题翻译：网边缘芯线的制造方法以及将网边缘芯焊接到子结构的方法
公开(公告)号：US09156239B2
公开(公告)日：2015-10-13
申请号：US14136622
申请日：2013-12-20
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Jonathan A. Freeman , Paul K. Oldroyd , Robert G. Pierce , Daniel Burns
IPC分类号： B32B3/12 , B32B37/10 , B32B37/14 , B29D99/00
CPC分类号： B32B37/10 , B29D99/0089 , B32B3/12 , B32B37/146 , B32B2037/1081 , B32B2305/024 , B32B2398/00 , Y10T428/24149 , Y10T428/24165
摘要： A method of assembling a core stiffened structure that includes bonding a composite core to a substructure by utilizing magnetic force to create pressure between a flat surface of the composite core the substructure, and bonding a face sheet onto a surface network of the composite core.
摘要翻译：一种组装芯加强结构的方法，其包括通过利用磁力将复合芯结合到子结构上，以在复合芯的平面与子结构之间产生压力，以及将表面片粘合到复合芯的表面网络上。

2. 发明授权

US09211618B2 Method of securing composite core during a manufacturing process 有权
标题翻译：在制造过程中固定复合材料芯的方法
公开(公告)号：US09211618B2
公开(公告)日：2015-12-15
申请号：US14136579
申请日：2013-12-20
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Jonathan A. Freeman
IPC分类号： B29C65/78 , B32B37/10 , B25B11/00 , B23Q3/154 , B29D99/00 , B32B3/12 , B32B37/16 , B32B5/02 , B32B15/14 , B29L31/30 , B29C65/48 , B29C65/50 , B29C65/00 , B29C53/60 , B29L31/60 , B29L31/08
CPC分类号： B23Q3/1546 , B25B11/002 , B29C53/60 , B29C65/48 , B29C65/5057 , B29C65/785 , B29C66/1122 , B29C66/1248 , B29C66/1312 , B29C66/43 , B29C66/438 , B29C66/5227 , B29C66/63 , B29C66/7254 , B29D99/0089 , B29L2031/082 , B29L2031/3088 , B29L2031/608 , B32B3/12 , B32B5/022 , B32B5/024 , B32B15/14 , B32B37/10 , B32B37/16 , B32B2037/1081 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2305/024 , B32B2313/04 , B32B2603/00 , Y10T29/49995 , Y10T29/49998 , Y10T156/10
摘要： A method of carving a contour surface on a composite core can include positioning a first edge of the composite core against a first tooled member; locating a first magnet within an outer cell member along the first edge of the composite core so that the first edge of the composite core is magnetically drawn to the first tooled member; locating a second magnet along a second edge of the composite core such that the second edge of the composite core is magnetically drawn to a second tooled member; and carving a first contour of the composite core.
摘要翻译：在复合芯上雕刻轮廓表面的方法可以包括将复合芯的第一边缘抵靠第一加工构件定位; 沿着复合芯的第一边缘将第一磁体定位在外电池构件内，使得复合磁芯的第一边缘被磁力拉伸到第一工具构件; 沿着所述复合芯的第二边缘定位第二磁体，使得所述复合芯的第二边缘被磁力地拉伸到第二工具构件; 并雕刻复合芯的第一轮廓。

3. 发明申请

US20140023431A1 Apparatus for Joining Members and Assembly Thereof 有权
标题翻译：连接会员及其装配的装置
公开(公告)号：US20140023431A1
公开(公告)日：2014-01-23
申请号：US14035031
申请日：2013-09-24
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Rodney H. Jones , Carl A. May
IPC分类号： F16B11/00
CPC分类号： F16B11/006 , F16B5/0266 , Y10T403/32991 , Y10T403/45 , Y10T403/47
摘要： An apparatus for joining a first member and a second member includes means for joining the first member and the second member, means for transferring shear loads between the first member and the second member separate from the means for joining the first member and the second member, and means for providing a compression preload to the means for transferring shear loads between the first member and the second member. An assembly includes a first member, a second member, and means for joining the first member and the second member. The assembly further includes means for transferring shear loads between the first member and the second member separate from the means for joining the first member and the second member and means for providing a compression preload to the means for transferring shear loads between the first member and the second member.
摘要翻译：一种用于接合第一构件和第二构件的装置包括用于接合第一构件和第二构件的装置，用于在第一构件和第二构件之间传递剪切载荷的装置与用于接合第一构件和第二构件的装置分离，以及用于向所述用于在所述第一构件和所述第二构件之间传递剪切载荷的装置提供压缩预载荷的装置。组件包括第一构件，第二构件和用于接合第一构件和第二构件的装置。组件还包括用于在第一构件和第二构件之间传递剪切载荷的装置，其与用于接合第一构件和第二构件的装置分开，以及用于向第一构件和第二构件之间传递剪切载荷的装置提供压缩预载荷的装置第二名成员

4. 发明申请

US20170320289A1 Composite Core and Method of Making Same 审中-公开
公开(公告)号：US20170320289A1
公开(公告)日：2017-11-09
申请号：US15659427
申请日：2017-07-25
申请人： BELL HELICOPTER TEXTRON INC.
发明人： James D. Hethcock , Kenneth E. Nunn , Paul Oldroyd
IPC分类号： B32B5/26 , B32B3/12 , B32B3/20 , B32B5/28 , B32B27/12 , B32B7/04 , B32B7/12 , B32B27/04 , D04C3/48 , B32B5/12
CPC分类号： B32B5/26 , B32B3/12 , B32B3/20 , B32B5/12 , B32B5/28 , B32B7/04 , B32B7/12 , B32B27/04 , B32B27/12 , B32B2250/40 , B32B2255/02 , B32B2255/26 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/106 , B32B2307/50 , D04C3/48 , Y10T428/24074 , Y10T428/31504
摘要： A composite core includes a plurality of tubes, each the plurality of tubes comprising a plurality of fibers disposed in a polymeric matrix. Adjacent tubes of the plurality of tubes are adhesively bonded to one another along sides of the adjacent tubes. A method of making a composite core includes the steps of providing a plurality of tubes, each of the plurality of tubes including a plurality of fibers disposed in a polymeric matrix, and adhesively bonding adjacent tubes of the plurality of tubes along sides of the adjacent tubes. A method of making a composite core such that a removable band is included in the core, the removable band being configured to be removable through a procedure subsequent to the cure of the composite core, thereby producing gaps in the core.

5. 发明授权

US09347473B2 Apparatus for joining members and assembly thereof 有权
标题翻译：用于连接构件和组件的装置
公开(公告)号：US09347473B2
公开(公告)日：2016-05-24
申请号：US14035031
申请日：2013-09-24
申请人： BELL HELICOPTER TEXTRON INC.
发明人： James D. Hethcock , Rodney H. Jones , Carl A. May
IPC分类号： F16B11/00 , F16B5/02
CPC分类号： F16B11/006 , F16B5/0266 , Y10T403/32991 , Y10T403/45 , Y10T403/47
摘要： An apparatus for joining a first member and a second member includes fasteners for joining the first member and the second member, a shear transfer layer for transferring shear loads between the first member and the second member separate from the fasteners for joining the first member and the second member. An assembly includes a first member, a second member, and fasteners for joining the first member and the second member. The assembly further includes a shear transfer layer for transferring shear loads between the first member and the second member separate from the fasteners for joining the first member and the second.
摘要翻译：用于接合第一构件和第二构件的装置包括用于接合第一构件和第二构件的紧固件，用于在第一构件和第二构件之间传递剪切载荷的剪切传递层，与用于接合第一构件和第二构件的紧固件分离，第二名成员组件包括第一构件，第二构件和用于接合第一构件和第二构件的紧固件。组件还包括用于在第一构件和第二构件之间传递剪切载荷的剪切传递层，其与用于接合第一构件和第二构件的紧固件分开。

6. 发明申请

US20150174819A1 METHOD OF SPLICING COMPOSITE CORE 有权
标题翻译：分离复合核的方法
公开(公告)号：US20150174819A1
公开(公告)日：2015-06-25
申请号：US14136523
申请日：2013-12-20
申请人： BELL HELICOPTER TEXTRON INC.
发明人： James D. Hethcock , Jonathan A. Freeman
IPC分类号： B29C65/00
CPC分类号： B29C66/8126 , B29C53/60 , B29C65/00 , B29C65/48 , B29C65/5057 , B29C65/74 , B29C65/785 , B29C66/0042 , B29C66/1122 , B29C66/1142 , B29C66/1248 , B29C66/1312 , B29C66/43 , B29C66/438 , B29C66/5227 , B29C66/63 , B29C66/71 , B29C66/7254 , B29C66/8122 , B29C66/81261 , B29C66/8185 , B29D99/0089 , B29L2031/082 , B29L2031/3088 , B29L2031/608 , B32B3/12 , B32B5/022 , B32B5/024 , B32B5/26 , B32B7/12 , B32B27/12 , B32B27/20 , B32B27/281 , B32B27/286 , B32B27/34 , B32B27/36 , B32B27/38 , B32B27/42 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/208 , B32B2307/516 , Y10T156/1089 , Y10T156/1093 , Y10T156/1744 , B29K2827/18 , B29K2905/00 , B29K2905/02 , B29K2031/00 , B29K2061/04 , B29K2063/00 , B29K2067/00 , B29K2071/00 , B29K2077/00 , B29K2079/08 , B29K2079/085 , B29K2081/04
摘要： A method of splicing together a first composite core and a second composite core can include: positioning a first flange of the first composite core adjacent to a second flange of the second composite core, applying an adhesive, and locating a first magnet and a second magnet to provide a pressure on the adhesive.
摘要翻译：将第一复合芯和第二复合芯拼接在一起的方法可以包括：将第一复合芯的第一凸缘邻近第二复合芯的第二凸缘定位，施加粘合剂，以及将第一磁体和第二磁体以提供粘合剂上的压力。

7. 发明授权

US09090026B2 Method of splicing composite core 有权
标题翻译：拼接复合芯的方法
公开(公告)号：US09090026B2
公开(公告)日：2015-07-28
申请号：US14136523
申请日：2013-12-20
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Jonathan A. Freeman
IPC分类号： B31F5/00 , B29C65/00 , B29C65/74
CPC分类号： B29C66/8126 , B29C53/60 , B29C65/00 , B29C65/48 , B29C65/5057 , B29C65/74 , B29C65/785 , B29C66/0042 , B29C66/1122 , B29C66/1142 , B29C66/1248 , B29C66/1312 , B29C66/43 , B29C66/438 , B29C66/5227 , B29C66/63 , B29C66/71 , B29C66/7254 , B29C66/8122 , B29C66/81261 , B29C66/8185 , B29D99/0089 , B29L2031/082 , B29L2031/3088 , B29L2031/608 , B32B3/12 , B32B5/022 , B32B5/024 , B32B5/26 , B32B7/12 , B32B27/12 , B32B27/20 , B32B27/281 , B32B27/286 , B32B27/34 , B32B27/36 , B32B27/38 , B32B27/42 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/208 , B32B2307/516 , Y10T156/1089 , Y10T156/1093 , Y10T156/1744 , B29K2827/18 , B29K2905/00 , B29K2905/02 , B29K2031/00 , B29K2061/04 , B29K2063/00 , B29K2067/00 , B29K2071/00 , B29K2077/00 , B29K2079/08 , B29K2079/085 , B29K2081/04
摘要： A method of splicing together a first composite core and a second composite core can include: positioning a first flange of the first composite core adjacent to a second flange of the second composite core, applying an adhesive, and locating a first magnet and a second magnet to provide a pressure on the adhesive.
摘要翻译：将第一复合芯和第二复合芯拼接在一起的方法可以包括：将第一复合芯的第一凸缘邻近第二复合芯的第二凸缘定位，施加粘合剂，以及将第一磁体和第二磁体以提供粘合剂上的压力。

8. 发明申请

US20150174876A1 METHOD OF MANUFACTURING NET EDGE CORE AND A METHOD OF BONDING NET EDGE CORE TO A SUBSTRUCTURE 有权
标题翻译：制造网边核心的方法和将网边核心连接到子结构的方法
公开(公告)号：US20150174876A1
公开(公告)日：2015-06-25
申请号：US14136622
申请日：2013-12-20
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Jonathan A. Freeman , Paul K. Oldroyd , Robert G. Pierce , Daniel Burns
IPC分类号： B32B37/10
CPC分类号： B32B37/10 , B29D99/0089 , B32B3/12 , B32B37/146 , B32B2037/1081 , B32B2305/024 , B32B2398/00 , Y10T428/24149 , Y10T428/24165
摘要： A method of assembling a core stiffened structure that includes bonding a composite core to a substructure by utilizing magnetic force to create pressure between a flat surface of the composite core the substructure, and bonding a face sheet onto a surface network of the composite core.
摘要翻译：一种组装芯加强结构的方法，其包括通过利用磁力将复合芯结合到子结构上，以在复合芯的平面与子结构之间产生压力，以及将表面片粘合到复合芯的表面网络上。

9. 发明申请

US20150174717A1 METHOD OF SECURING COMPOSITE CORE DURING A MANUFACTURING PROCESS 有权
标题翻译：在制造过程中保护复合芯的方法
公开(公告)号：US20150174717A1
公开(公告)日：2015-06-25
申请号：US14136579
申请日：2013-12-20
申请人： Bell Helicopter Textron Inc.
发明人： James D. Hethcock , Jonathan A. Freeman
IPC分类号： B23Q3/154 , B32B37/16 , B32B37/10
CPC分类号： B23Q3/1546 , B25B11/002 , B29C53/60 , B29C65/48 , B29C65/5057 , B29C65/785 , B29C66/1122 , B29C66/1248 , B29C66/1312 , B29C66/43 , B29C66/438 , B29C66/5227 , B29C66/63 , B29C66/7254 , B29D99/0089 , B29L2031/082 , B29L2031/3088 , B29L2031/608 , B32B3/12 , B32B5/022 , B32B5/024 , B32B15/14 , B32B37/10 , B32B37/16 , B32B2037/1081 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2305/024 , B32B2313/04 , B32B2603/00 , Y10T29/49995 , Y10T29/49998 , Y10T156/10
摘要： A method of carving a contour surface on a composite core can include positioning a first edge of the composite core against a first tooled member; locating a first magnet within an outer cell member along the first edge of the composite core so that the first edge of the composite core is magnetically drawn to the first tooled member; locating a second magnet along a second edge of the composite core such that the second edge of the composite core is magnetically drawn to a second tooled member; and carving a first contour of the composite core.
摘要翻译：在复合芯上雕刻轮廓表面的方法可以包括将复合芯的第一边缘抵靠第一加工构件定位; 沿着复合芯的第一边缘将第一磁体定位在外电池构件内，使得复合磁芯的第一边缘被磁力拉伸到第一工具构件; 沿着所述复合芯的第二边缘定位第二磁体，使得所述复合芯的第二边缘被磁力地拉伸到第二工具构件; 并雕刻复合芯的第一轮廓。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式