公开(公告)号：US20160159036A1

公开(公告)日：2016-06-09

申请号：US14563435

申请日：2014-12-08

Applicant: THE BOEING COMPANY

Inventor： Keith Daniel Humfeld ,  Kelsi Marie Hurley

IPC: B32B7/08 ,  B32B37/18

CPC classification number: B32B7/08 ,  B29C65/02 ,  B29C65/18 ,  B29C65/564 ,  B29C66/1122 ,  B29C66/45 ,  B29C66/721 ,  B29C66/73752 ,  B29C66/73941 ,  B29C66/83431 ,  B29C70/24 ,  B29C70/543 ,  B32B3/08 ,  B32B5/06 ,  B32B5/26 ,  B32B37/18 ,  B32B2250/20 ,  B32B2250/40 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2305/076 ,  B32B2305/34 ,  B32B2311/005 ,  B32B2605/18 ,  F16B1/0014

Abstract: A layered composite assembly may include a plurality of composite fiber layers stacked onto one another. Each of the plurality of composite fiber layers may include a main body including a plurality of composite fibers. The main body may be pre-impregnated with at least one resin. Each composite fiber layer also includes a plurality of layer-securing pins secured to the main body. The layer-securing pins are configured to mechanically connect the main body to an adjacent composite fiber layer.

Abstract translation: 分层复合组件可以包括彼此堆叠的多个复合纤维层。 多个复合纤维层中的每一个可以包括包括多个复合纤维的主体。 主体可以用至少一种树脂预浸渍。 每个复合纤维层还包括固定到主体的多个层固定销。 层紧固销被构造成将主体机械地连接到相邻的复合纤维层。

公开(公告)号：US10457017B2

公开(公告)日：2019-10-29

申请号：US14563435

申请日：2014-12-08

Applicant: THE BOEING COMPANY

Inventor： Keith Daniel Humfeld ,  Kelsi Marie Hurley

IPC: B32B7/08 ,  B32B37/18 ,  F16B1/00 ,  B29C65/56 ,  B32B5/06 ,  B32B5/26 ,  B32B3/08 ,  B29C65/02 ,  B29C70/54 ,  B29C65/00 ,  B29C70/24 ,  B29C65/18

Abstract: A layered composite assembly may include a plurality of composite fiber layers stacked onto one another. Each of the plurality of composite fiber layers may include a main body including a plurality of composite fibers. The main body may be pre-impregnated with at least one resin. Each composite fiber layer also includes a plurality of layer-securing pins secured to the main body. The layer-securing pins are configured to mechanically connect the main body to an adjacent composite fiber layer.

公开(公告)号：US09821530B2

公开(公告)日：2017-11-21

申请号：US14553553

申请日：2014-11-25

Applicant: The Boeing Company

Inventor： Mark Stewart Wilenski ,  Kelsi Marie Hurley

IPC: B32B5/12 ,  B32B5/10 ,  B32B5/02 ,  B32B5/00 ,  B32B5/22 ,  B32B5/26 ,  B32B27/12 ,  B32B27/06 ,  B32B27/00 ,  B32B7/00 ,  B32B7/04 ,  B32B7/08 ,  B32B1/00 ,  B32B5/14 ,  B32B37/14 ,  B32B5/24 ,  B32B7/02 ,  B32B7/10 ,  B32B7/12 ,  B32B7/14 ,  B32B27/08 ,  B32B27/26 ,  B32B27/28 ,  B32B27/38 ,  B32B38/00

CPC classification number: B32B5/142 ,  B32B1/00 ,  B32B5/00 ,  B32B5/02 ,  B32B5/022 ,  B32B5/10 ,  B32B5/12 ,  B32B5/14 ,  B32B5/22 ,  B32B5/24 ,  B32B5/26 ,  B32B7/00 ,  B32B7/02 ,  B32B7/04 ,  B32B7/045 ,  B32B7/08 ,  B32B7/10 ,  B32B7/12 ,  B32B7/14 ,  B32B27/00 ,  B32B27/06 ,  B32B27/08 ,  B32B27/12 ,  B32B27/26 ,  B32B27/28 ,  B32B27/38 ,  B32B37/14 ,  B32B2038/0076 ,  B32B2250/00 ,  B32B2250/40 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2264/00 ,  B32B2264/02 ,  B32B2264/0221 ,  B32B2305/07 ,  B32B2305/08 ,  B32B2307/50 ,  B32B2307/552 ,  B32B2307/558 ,  B32B2307/722 ,  B32B2605/00 ,  B32B2605/18

Abstract: A composite laminate comprises first and second fiber beds, and an interlayer between the fiber beds. The interlayer includes toughened regions that extend between the fiber beds and are fused to the fiber beds.

公开(公告)号：US10688766B2

公开(公告)日：2020-06-23

申请号：US14553568

申请日：2014-11-25

Applicant: The Boeing Company

Inventor： Mark Stewart Wilenski ,  Kelsi Marie Hurley

IPC: B32B37/14 ,  B32B5/02 ,  B32B27/12 ,  B32B27/26 ,  B32B7/02 ,  B32B7/08 ,  B32B27/28 ,  B32B5/22 ,  B32B7/00 ,  B32B7/12 ,  B32B5/00 ,  B32B27/38 ,  B32B5/24 ,  B32B27/00 ,  B32B7/10 ,  B32B5/14 ,  B32B5/26 ,  B32B7/14 ,  B32B5/10 ,  B32B7/04 ,  B32B27/08 ,  B32B5/12 ,  B32B27/06 ,  B32B38/10

Abstract: A method of fabricating a composite laminate comprises forming a stack including first and second fiber beds and an interlayer between the fiber beds. The fiber beds are impregnated with matrix resin. The interlayer includes a soluble thermoplastic component on an insoluble component. The method further comprises dissolving the soluble thermoplastic component into the matrix resin to reduce thickness of the interlayer.

公开(公告)号：US20160257104A1

公开(公告)日：2016-09-08

申请号：US14553568

申请日：2014-11-25

Applicant: The Boeing Company

Inventor： Mark Stewart Wilenski ,  Kelsi Marie Hurley

IPC: B32B37/14 ,  B32B27/12 ,  B32B38/10 ,  B32B5/02

Abstract: A method of fabricating a composite laminate comprises forming a stack including first and second fiber beds and an interlayer between the fiber beds. The fiber beds are impregnated with matrix resin. The interlayer includes a soluble thermoplastic component on an insoluble component. The method further comprises dissolving the soluble thermoplastic component into the matrix resin to reduce thickness of the interlayer.

Abstract translation: 制造复合层压体的方法包括形成包括第一和第二纤维床和纤维床之间的中间层的堆叠。 纤维床用基质树脂浸渍。 中间层包括在不溶性组分上的可溶性热塑性组分。 该方法还包括将可溶性热塑性组分溶解到基质树脂中以减小中间层的厚度。

公开(公告)号：US20160144595A1

公开(公告)日：2016-05-26

申请号：US14553553

申请日：2014-11-25

Applicant: The Boeing Company

Inventor： Mark Stewart Wilenski ,  Kelsi Marie Hurley

IPC: B32B5/14 ,  B32B7/04 ,  B32B37/14

CPC classification number: B32B5/142 ,  B32B1/00 ,  B32B5/00 ,  B32B5/02 ,  B32B5/022 ,  B32B5/10 ,  B32B5/12 ,  B32B5/14 ,  B32B5/22 ,  B32B5/24 ,  B32B5/26 ,  B32B7/00 ,  B32B7/02 ,  B32B7/04 ,  B32B7/045 ,  B32B7/08 ,  B32B7/10 ,  B32B7/12 ,  B32B7/14 ,  B32B27/00 ,  B32B27/06 ,  B32B27/08 ,  B32B27/12 ,  B32B27/26 ,  B32B27/28 ,  B32B27/38 ,  B32B37/14 ,  B32B2038/0076 ,  B32B2250/00 ,  B32B2250/40 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2264/00 ,  B32B2264/02 ,  B32B2264/0221 ,  B32B2305/07 ,  B32B2305/08 ,  B32B2307/50 ,  B32B2307/552 ,  B32B2307/558 ,  B32B2307/722 ,  B32B2605/00 ,  B32B2605/18

Abstract: A composite laminate comprises first and second fiber beds, and an interlayer between the fiber beds. The interlayer includes toughened regions that extend between the fiber beds and are fused to the fiber beds.

Abstract translation: 复合层压板包括第一和第二纤维床以及纤维床之间的中间层。 夹层包括在纤维床之间延伸并与纤维床融合的韧化区域。