公开(公告)号：US20160339647A1

公开(公告)日：2016-11-24

申请号：US14718893

申请日：2015-05-21

Applicant: The Boeing Company

Inventor： Marc R. Matsen ,  Mark A. Negley ,  Jeffery L. Marcoe ,  Stephen G. Moore ,  Brice A. Johnson ,  Alexandra K. Dillon ,  Megan M. Petersen

IPC: B29C70/38 ,  B29C65/00 ,  B29C65/32 ,  B29C65/16

CPC classification number: B29C70/382 ,  B29C65/02 ,  B29C65/08 ,  B29C65/1416 ,  B29C65/1419 ,  B29C65/1432 ,  B29C65/1616 ,  B29C65/1619 ,  B29C65/1622 ,  B29C65/1632 ,  B29C65/18 ,  B29C65/22 ,  B29C65/30 ,  B29C65/32 ,  B29C66/1122 ,  B29C66/45 ,  B29C66/723 ,  B29C66/7392 ,  B29C66/8322 ,  B29C66/8362 ,  B29C70/38 ,  B29K2101/12

Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.

Abstract translation: 一种光纤放置系统，包括在第一位置处的光纤放置台，所述光纤放置台包括工具和配置成在所述工具上构造加强层的光纤放置组件，所述第一光纤放置组件包括压缩辊， 至少部分地限定压区的压实辊，延伸穿过压区的热塑性复合层，以及定位成加热邻近压区的热塑性复合层的加热单元，以及固结位置处的固结位置， 所述第一位置，所述合并工位包括固结工具和被配置为整合包括所述加固层的加强层叠组件的合并系统。

公开(公告)号：US20160316522A1

公开(公告)日：2016-10-27

申请号：US14697418

申请日：2015-04-27

Applicant: The Boeing Company

Inventor： Marc R. Matsen ,  Mark A. Negley

IPC: H05B6/10 ,  C21D9/42 ,  B21D21/00 ,  C21D1/18 ,  C21D1/42 ,  H05B6/08 ,  C21D6/00

CPC classification number: H05B6/101 ,  B21D21/00 ,  B22F3/03 ,  B22F3/087 ,  B22F3/105 ,  B22F3/14 ,  B22F3/16 ,  B22F2003/1053 ,  B22F2202/05 ,  B22F2202/07 ,  B22F2203/00 ,  C21D1/18 ,  C21D1/42 ,  C21D6/00 ,  C21D9/42 ,  H05B6/06 ,  H05B6/08 ,  H05B6/105 ,  H05B2206/023 ,  Y02P10/253

Abstract: Described herein is a method of forming a heat-treated material includes positioning the heat-treated material between first and second susceptors. Each of the first and second susceptors includes a tool face shaped according to a desired shape of the heat-treated material. The method also includes applying a low-strength magnetic field to the first and second susceptors to heat the first and second susceptors. Further, the method includes compressing the heat-treated material between the first and second susceptors to form the heat-treated material into the desired shape. The method additionally includes applying a high-strength magnetic field to the heat-treated material before compressing the heat-treated material between the first and second susceptors.

Abstract translation: 这里描述的是形成热处理材料的方法，包括将热处理材料定位在第一和第二基座之间。 第一和第二基座中的每一个包括根据热处理材料的期望形状成形的工具面。 该方法还包括将低强度磁场施加到第一和第二感受器以加热第一和第二感受体。 此外，该方法包括在第一和第二基座之间压缩经热处理的材料，以将热处理的材料形成为期望的形状。 该方法还包括在将第一和第二感受器之间的热处理材料压缩之前，向热处理材料施加高强度磁场。

公开(公告)号：US20140099477A1

公开(公告)日：2014-04-10

申请号：US13644628

申请日：2012-10-04

Applicant: THE BOEING COMPANY

Inventor： Marc R. Matsen ,  Mark A. Negley

IPC: B32B3/26 ,  B32B37/00

CPC classification number: B29C70/34 ,  B29C70/543 ,  Y02T50/43 ,  Y10T156/10 ,  Y10T428/24562

Abstract: A composite structure may include a laminate and a stabilizing element. The laminate may have a plurality of composite plies. The composite structure may include a geometric discontinuity that may be associated with the laminate. The stabilizing element may be included with the composite plies and may be located proximate the geometric discontinuity.

Abstract translation: 复合结构可以包括层压板和稳定元件。 层压板可以具有多个复合层。 复合结构可以包括可以与层压板相关联的几何不连续性。 稳定元件可以包括在复合层中，并且可以位于几何不连续处附近。