公开(公告)号：US20140076479A1

公开(公告)日：2014-03-20

申请号：US13621991

申请日：2012-09-18

Applicant: The Boeing Company

Inventor： Aaron W. Bartel ,  John B. Moser

IPC: B29C53/08 ,  B32B37/00

CPC classification number: B29C53/04 ,  B29C53/385 ,  B29C53/42 ,  B29C53/84 ,  B29C65/08 ,  B29C65/36 ,  B29C65/48 ,  B29C65/5071 ,  B29C65/5085 ,  B29C65/56 ,  B29C66/1142 ,  B29C66/1222 ,  B29C66/1224 ,  B29C66/1226 ,  B29C66/4322 ,  B29C66/49 ,  B29C66/53243 ,  B29C66/547 ,  B29C66/71 ,  B29C66/721 ,  B29C66/723 ,  B29C66/72523 ,  B29C66/72525 ,  B29C66/727 ,  B29C66/73921 ,  B29C66/81455 ,  B29C2791/006 ,  B29K2079/085 ,  B29K2101/12 ,  B29L2009/00 ,  B29L2023/22 ,  B29L2031/3076 ,  Y10T156/1038

Abstract: A method of forming a structural tube may include urging a substantially flat thermoplastic sandwich sheet against a mandrel and heating the thermoplastic sandwich sheet to a temperature below a glass transition temperature. The method may further include allowing the thermoplastic sandwich sheet to cool and removing the mandrel, thereby forming a tube portion.

Abstract translation: 形成结构管的方法可以包括将基本上平坦的热塑性夹层板推向心轴并将热塑性夹层板加热到低于玻璃化转变温度的温度。 该方法还可以包括允许热塑性夹层板冷却并移除芯棒，从而形成管部分。

公开(公告)号：US10744722B2

公开(公告)日：2020-08-18

申请号：US15797314

申请日：2017-10-30

Applicant: The Boeing Company

Inventor： Angelo Rossi ,  Jeffery L. Marcoe ,  Marc R. Matsen ,  Aaron W. Bartel ,  Waeil M. Ashmawi ,  Sahrudine Apdalhaliem ,  Adriana Willempje Blom-Schieber ,  David Reusch

IPC: B29C65/72 ,  B29C70/50 ,  B29C70/24 ,  B29C65/62 ,  D04C1/06 ,  B29C33/44 ,  B29D99/00 ,  B29B11/16

Abstract: A radius filler includes a plurality of fibers encapsulated in resin and braided into a braided radius filler. The braided radius filler has a substantially triangular shape with concave radius filler side surfaces and a substantially planar radius filler base surface.

公开(公告)号：US10183735B2

公开(公告)日：2019-01-22

申请号：US15012325

申请日：2016-02-01

Applicant: The Boeing Company

Inventor： David E. Gideon ,  Ian E. Schroeder ,  Kristin L. Hall ,  Kin M. Ng ,  Megan C. Kinney ,  Greg M. Reyneke ,  Randall D. Wilkerson ,  Richard R. Rosman ,  Aaron W. Bartel

IPC: B64C1/14

Abstract: A window frame assembly for an aircraft, includes a window frame of composite material, adapted for attachment in a window opening of an aircraft, having an outer flange with an exterior surface and an interior surface, a metal erosion shield attached to the exterior surface of the outer flange, and a polymer adapter ring, attached to the interior surface of the outer flange. The window frame has a substantially constant thickness, and the erosion shield has a substantially constant cross-sectional shape. The adapter ring has a sloped engagement surface configured for supporting a window pane assembly.

公开(公告)号：US20180065314A1

公开(公告)日：2018-03-08

申请号：US15797314

申请日：2017-10-30

Applicant: The Boeing Company

Inventor： Angelo Rossi ,  Jeffery L. Marcoe ,  Marc R. Matsen ,  Aaron W. Bartel ,  Waeil M. Ashmawi ,  Sahrudine Apdalhaliem ,  Adriana Willempje Blom-Schieber ,  David Reusch

IPC: B29C65/72 ,  B29D99/00 ,  B29C33/44 ,  B29C65/62 ,  B29C70/24 ,  B29C70/50 ,  D04C1/06

Abstract: A radius filler includes a plurality of fibers encapsulated in resin and braided into a braided radius filler. The braided radius filler has a substantially triangular shape with concave radius filler side surfaces and a substantially planar radius filler base surface.

公开(公告)号：US09498915B2

公开(公告)日：2016-11-22

申请号：US13732624

申请日：2013-01-02

Applicant: The Boeing Company

Inventor： Aaron W. Bartel ,  David E. Gideon ,  Michael H. Larson

IPC: B29C70/46 ,  B29C51/02 ,  B29C70/50 ,  B29D99/00

CPC classification number: B29C51/02 ,  B29C70/50 ,  B29D99/0003

Abstract: A method of fabricating a reinforced thermoplastic composite part comprises moving a laminate of reinforcing fibers embedded in a thermoplastic matrix for sequential operations through a heating station and then a forming station. The heating station is used to soften the thermoplastic matrix in a portion of the laminate while the forming station is used to impart a geometry to a portion of the laminate whose thermoplastic matrix had just been softened. The softening and the forming are performed simultaneously on different portions of the laminate.

Abstract translation: 制造增强热塑性复合材料部件的方法包括将嵌入热塑性基质中的增强纤维的层压体移动通过加热站然后成形站进行顺序操作。 加热站用于软化层压体的一部分中的热塑性基质，同时使用成形工位将几何形状赋予热塑性基体刚刚软化的层压体的一部分。 在层压体的不同部分上同时进行软化和成形。

公开(公告)号：US09452840B2

公开(公告)日：2016-09-27

申请号：US14252816

申请日：2014-04-15

Applicant: The Boeing Company

Inventor： Brett I. Lyons ,  Aaron W. Bartel ,  Trevor E. Tucker

IPC: F16L9/21 ,  B32B1/08 ,  B32B3/24 ,  B32B3/26 ,  B29C67/00 ,  B64D13/00 ,  B29L31/30 ,  B33Y10/00 ,  F16L9/00 ,  B33Y80/00

CPC classification number: B29C64/135 ,  B22F3/1055 ,  B29C64/118 ,  B29C64/124 ,  B29C64/129 ,  B29C64/153 ,  B29C67/0062 ,  B29C67/0066 ,  B29C67/0077 ,  B29K2995/0016 ,  B29K2995/0091 ,  B29L2031/3076 ,  B32B1/08 ,  B32B3/263 ,  B32B3/266 ,  B32B3/30 ,  B32B2605/18 ,  B33Y10/00 ,  B33Y80/00 ,  F16L9/006 ,  F16L9/21

Abstract: One example of the present disclosure relates to a monolithic part including an exterior wall and a first cavity. The first cavity includes a first aperture in communication with the exterior wall and a first inner surface defining a first shape. The first shape prevents extraction from the first cavity, via the first aperture, of a first virtual object having the first shape.

Abstract translation: 本公开的一个实例涉及包括外壁和第一腔的整体部件。 第一腔包括与外壁连通的第一孔和限定第一形状的第一内表面。 第一形状防止具有第一形状的第一虚拟物体从第一孔经由第一孔提取。