公开(公告)号：EP1995044A3

公开(公告)日：2017-07-05

申请号：EP08156751.3

申请日：2008-05-22

申请人： The Boeing Company

发明人： Brennan, Joseph D. ,  Hempstead, George D. ,  Jones, Darrell D. ,  Lum, Matthew K. ,  McCowin, Peter D. ,  Rowe, Terrence J. ,  Schlosstein, Hugh R.

IPC分类号： B29C70/30 ,  B29C70/32 ,  B29C70/54 ,  B29C70/38 ,  B29L31/30

CPC分类号： B29C70/30 ,  B29C70/32 ,  B29C70/386 ,  B29C70/541 ,  B29L2031/3076 ,  Y10T29/49622 ,  Y10T29/53

摘要： Method and apparatus for layup placement on a layup structure is provided. The method includes iteratively loading a layup for the layup structure on a support frame of a saddle module; aligning the saddle module with a pre-selected registration position corresponding to a predetermined application path on the layup structure; and impressing the layup into forced contact with the layup structure along the predetermined application path using a predetermined application force. The apparatus includes a plurality of saddle modules configured to operate in unison, wherein the plurality of saddle modules is configured to receive a pre-selected composite material layup.

摘要翻译： 提供了用于叠层放置在叠层结构上的方法和装置。 该方法包括在鞍座模块的支撑框架上迭代地加载用于叠层结构的叠层; 将所述鞍座模块与对应于所述叠层结构上的预定应用路径的预先选择的配准位置对准; 并且使用预定的施加力将叠层施加为沿着预定的施加路径与叠层结构强制接触。 该设备包括被配置为一致地操作的多个鞍座模块，其中多个鞍座模块被配置为接收预先选择的复合材料叠层。

公开(公告)号：EP1995045A2

公开(公告)日：2008-11-26

申请号：EP08156756.2

申请日：2008-05-22

申请人： The Boeing Company

发明人： Brennan, Joseph D. ,  Hempstead, George D. ,  Jones, Darrell D. ,  Lum, Matthew K. ,  McCowin, Peter D. ,  Rowe, Terrence J. ,  Schlosstein, Hugh R.

IPC分类号： B29C70/30

CPC分类号： B29C70/30 ,  B29C70/545 ,  B29L2031/3082 ,  Y02T50/43 ,  Y10T29/49622 ,  Y10T29/53004 ,  Y10T156/10 ,  Y10T156/1002

摘要： A pre-patterned layup kit with layup patterned to accommodate an airframe topological feature, trimmed to fit a preselected target region of a layup structure, and conformed to the target region contour. The kit can be fabricated in advance of airframe manufacture and stored until use. The kit includes a flexible carrier upon which the layup is laid, and a release layer between the layup and the carrier. The layup has multiple laminae oriented to an carrier indexing element, and indexed to the target region thereby. A kit manufacturing method includes preparing the laminae constituent of the layup, preparing the carrier, and laying down the laminae on the carrier to make the kit. The kit can be compacted, inspected, and prepared for storage. The layup can be fabricated of a pre-patterned lamina or multiple laminae that are shaped and trimmed to accommodate an airframe topological feature.

摘要翻译： 具有图案化以适应机体拓扑特征的叠层的预先图案化的铺设套件，其被修剪以适合上层结构的预选的目标区域，并且符合目标区域轮廓。 该套件可以在机身制造之前制造并存储直到使用。 该套件包括铺设铺层的柔性载体，以及铺层和载体之间的释放层。 叠层具有定向到载体分度元件的多个层，并由此指定到目标区域。 试剂盒制备方法包括制备铺层的薄片成分，制备载体，以及将载片上的薄片铺设成载体。 试剂盒可以压实，检查和准备储存。 叠层可以由预先图案化的薄片或多个薄片制成，其被成形和修剪以适应机身拓扑特征。

公开(公告)号：EP1995044A2

公开(公告)日：2008-11-26

申请号：EP08156751.3

申请日：2008-05-22

申请人： THE BOEING COMPANY

发明人： Brennan, Joseph D. ,  Hempstead, George D. ,  Jones, Darrell D. ,  Lum, Matthew K. ,  McCowin, Peter D. ,  Rowe, Terrence J. ,  Schlosstein, Hugh R.

IPC分类号： B29C70/30

CPC分类号： B29C70/30 ,  B29C70/32 ,  B29C70/386 ,  B29C70/541 ,  B29L2031/3076 ,  Y10T29/49622 ,  Y10T29/53

摘要： Method and apparatus for layup placement on a layup structure is provided. The method includes iteratively loading a layup for the layup structure on a support frame of a saddle module; aligning the saddle module with a pre-selected registration position corresponding to a predetermined application path on the layup structure; and impressing the layup into forced contact with the layup structure along the predetermined application path using a predetermined application force. The apparatus includes a plurality of saddle modules configured to operate in unison, wherein the plurality of saddle modules is configured to receive a pre-selected composite material layup.

摘要翻译： 提供了用于上铺布置在上铺结构上的方法和装置。 该方法包括在鞍座模块的支撑框架上迭代地加载叠层结构的叠层; 将鞍座模块与对应于铺设结构上的预定应用路径的预先选择的对位位置对准; 并且使用预定的施加力沿着预定的施加路径将叠层压印成与上铺结构的强制接触。 该装置包括配置成一致操作的多个鞍座模块，其中多个鞍座模块被配置为接收预选的复合材料叠层。

公开(公告)号：EP1995045A3

公开(公告)日：2017-11-22

申请号：EP08156756.2

申请日：2008-05-22

申请人： The Boeing Company

发明人： Brennan, Joseph D. ,  Hempstead, George D. ,  Jones, Darrell D. ,  Lum, Matthew K. ,  McCowin, Peter D. ,  Rowe, Terrence J. ,  Schlosstein, Hugh R. ,  Kordel, Jan A.

IPC分类号： B29C70/30 ,  B29C70/54 ,  B29L31/30

CPC分类号： B29C70/30 ,  B29C70/545 ,  B29L2031/3082 ,  Y02T50/43 ,  Y10T29/49622 ,  Y10T29/53004 ,  Y10T156/10 ,  Y10T156/1002

摘要： A pre-patterned layup kit with layup patterned to accommodate an airframe topological feature, trimmed to fit a preselected target region of a layup structure, and conformed to the target region contour. The kit can be fabricated in advance of airframe manufacture and stored until use. The kit includes a flexible carrier upon which the layup is laid, and a release layer between the layup and the carrier. The layup has multiple laminae oriented to an carrier indexing element, and indexed to the target region thereby. A kit manufacturing method includes preparing the laminae constituent of the layup, preparing the carrier, and laying down the laminae on the carrier to make the kit. The kit can be compacted, inspected, and prepared for storage. The layup can be fabricated of a pre-patterned lamina or multiple laminae that are shaped and trimmed to accommodate an airframe topological feature.

摘要翻译： 一种预先图案化的叠层套件，其叠层被图案化以适应机身拓扑特征，被修剪以适应叠层结构的预选目标区域，并符合目标区域轮廓。 该套件可以在机身制造之前制造并储存直至使用。 该套件包括敷设敷层的柔性载体以及敷层和载体之间的释放层。 叠层具有多个定向于载体索引元件的薄片，并由此索引到目标区域。 试剂盒制造方法包括制备叠层的薄片组分，制备载体，并将薄层放在载体上以制备试剂盒。 该试剂盒可以被压实，检查并准备好储存。 叠层可以由预先图案化的薄片或多个薄片制成，其被成形和修剪以适应机身拓扑特征。