公开(公告)号：US09145277B2

公开(公告)日：2015-09-29

申请号：US13782180

申请日：2013-03-01

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  Levi H. Armstrong ,  Elizabeth Oberle

IPC: B65H18/00 ,  B29C53/58 ,  B29D99/00 ,  B29C53/82

CPC classification number: B65H18/00 ,  B29C53/582 ,  B29C53/828 ,  B29D99/0089 ,  Y02T50/43

Abstract: A method of manufacturing a composite core can include: wrapping a mandrel in a mandrel wrapping process by securing a mandrel with a winding jig; orienting the composite material at a wrap angle to the mandrel; and depositing the composite material around a circumference of the mandrel. The method can further include assembling the wrapped mandrels in a tool and applying a pressure to the composite material during a curing cycle.

Abstract translation: 制造复合芯的方法可以包括：通过用卷绕夹具固定心轴来将心轴缠绕在心轴缠绕过程中; 将复合材料定向成与心轴成直角; 以及围绕心轴的圆周沉积复合材料。 该方法还可以包括将包裹的心轴组装在工具中，并在固化周期期间向复合材料施加压力。

公开(公告)号：US09120255B2

公开(公告)日：2015-09-01

申请号：US13835649

申请日：2013-03-15

Applicant: Bell Helicopter Textron Inc.

Inventor： Paul K. Oldroyd ,  James D. Hethcock, Jr. ,  Mark E. Tohlen ,  Phillip A. Kendrick

IPC: B29C53/58 ,  B29C41/08 ,  B29C70/32 ,  B29C70/34 ,  B29D99/00 ,  B29C53/82 ,  B29C41/52 ,  B29C33/48 ,  B29C33/52 ,  B29L31/60 ,  B29K105/08

CPC classification number: B29C41/085 ,  B29C33/485 ,  B29C33/52 ,  B29C41/52 ,  B29C53/821 ,  B29C53/828 ,  B29C70/32 ,  B29C70/345 ,  B29C2793/0027 ,  B29D99/0089 ,  B29K2105/0872 ,  B29L2031/608

Abstract: A method of wrapping a plurality of mandrels with a composite material can include rotating each mandrel at a rotational speed; translating each mandrel at a translation speed; positioning each mandrel back to back such that an aft face of a preceding mandrel is approximate to a forward face of a trailing mandrel; and sequentially wrapping each mandrel with the composite material in a helical orientation.

Abstract translation: 用复合材料包裹多个心轴的方法可以包括以一转动速度旋转每个心轴; 以平移速度平移每个心轴; 将每个心轴背靠背定位，使得前一个心轴的后表面接近拖尾心轴的前面; 并且顺序地将每个心轴与复合材料缠绕成螺旋方向。

公开(公告)号：US20150037533A1

公开(公告)日：2015-02-05

申请号：US13955105

申请日：2013-07-31

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  David G. Carlson

IPC: B32B3/12 ,  B64C1/18 ,  B64C3/20 ,  B32B37/14

CPC classification number: B32B37/146 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/486 ,  B29C65/5042 ,  B29C65/5057 ,  B29C65/7838 ,  B29C66/0042 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/5227 ,  B29C66/54 ,  B29C66/612 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/7254 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/8122 ,  B29C66/81261 ,  B29C66/81467 ,  B29C66/8185 ,  B29C66/8284 ,  B29C66/83415 ,  B29D99/0021 ,  B29L2031/3076 ,  B29L2031/3088 ,  B29L2031/608 ,  B32B3/04 ,  B32B3/12 ,  B32B5/12 ,  B32B5/142 ,  B32B7/12 ,  B32B2038/0076 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2307/302 ,  B32B2605/00 ,  B32B2605/18 ,  B64C1/18 ,  B64C3/20 ,  Y10T156/1093 ,  Y10T428/24149 ,  Y10T428/24165 ,  B29K2827/18 ,  B29K2307/04 ,  B29K2077/00 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2071/00 ,  B29K2067/00 ,  B29K2061/00 ,  B29K2081/04 ,  B29K2063/00 ,  B29K2079/08 ,  B29K2031/00 ,  B29K2061/04

Abstract: A method of manufacturing a core stiffened structure includes orienting the plurality of core wafers in a non-uniform pattern onto a first face sheet, the non-uniform pattern producing non-uniform spacing between adjacent core wafers; assembling a second face sheet onto the plurality of wafers; and curing an adhesive to create a bond between the plurality of wafers, the first face sheet, and the second face sheet.

Abstract translation: 一种制造芯加强结构的方法包括以非均匀图案将多个芯晶片定向到第一面板上，该不均匀图案产生相邻芯片之间的不均匀间隔; 将第二面板组装到所述多个晶片上; 以及固化粘合剂以在所述多个晶片，所述第一面板和所述第二面板之间产生粘合。

公开(公告)号：US10131108B2

公开(公告)日：2018-11-20

申请号：US13782359

申请日：2013-03-01

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  Levi H. Armstrong ,  Elizabeth Oberle

IPC: B31C3/00 ,  B31D3/02 ,  B29C53/82 ,  B29D99/00 ,  B29C53/58 ,  B29C35/04 ,  B32B1/08 ,  B29L31/60

Abstract: A method of manufacturing a composite core can include: wrapping a mandrel in a mandrel wrapping process by securing a mandrel with a winding jig; orienting the composite material at a wrap angle to the mandrel; and depositing the composite material around a circumference of the mandrel. The method can further include assembling the wrapped mandrels in a tool and applying a pressure to the composite material during a curing cycle.

公开(公告)号：US20140360323A1

公开(公告)日：2014-12-11

申请号：US13914737

申请日：2013-06-11

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Levi H. Armstrong

IPC: B26D1/157

CPC classification number: B26D1/157 ,  B26D1/08 ,  B26D1/10 ,  B26D3/167 ,  B26D7/01 ,  B29C53/60 ,  B29C66/543 ,  B29C69/001 ,  B29C70/30 ,  B29C70/545 ,  B29D99/0089 ,  B32B3/12 ,  B32B37/146 ,  Y10T83/04 ,  Y10T83/0405 ,  Y10T83/0524 ,  Y10T156/1026 ,  Y10T156/1059 ,  Y10T156/1066 ,  Y10T156/1079 ,  Y10T156/13 ,  Y10T156/1357

Abstract: A method of cutting a wafer of composite core from a bulk composite core includes stabilizing the bulk composite core with a fixture, the bulk composite core having a plurality of tube members. The method also includes cutting through each of the tube members to create the wafer while the bulk composite core is stabilized by the fixture.

Abstract translation: 一种从大块复合芯片切割复合芯片的方法包括用固定装置稳定本体复合芯片，该大块复合芯片具有多个管件。 该方法还包括切割每个管构件以产生晶片，同时大体积复合芯由夹具稳定。

公开(公告)号：US09925680B2

公开(公告)日：2018-03-27

申请号：US13914737

申请日：2013-06-11

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Levi H. Armstrong

IPC: B29C70/54 ,  B32B3/12 ,  B26D1/157 ,  B26D7/01 ,  B29C69/00 ,  B29D99/00 ,  B29C53/60 ,  B26D1/10 ,  B26D3/16 ,  B26D1/08 ,  B29C65/00 ,  B32B37/14 ,  B29C70/30

CPC classification number: B26D1/157 ,  B26D1/08 ,  B26D1/10 ,  B26D3/167 ,  B26D7/01 ,  B29C53/60 ,  B29C66/543 ,  B29C69/001 ,  B29C70/30 ,  B29C70/545 ,  B29D99/0089 ,  B32B3/12 ,  B32B37/146 ,  Y10T83/04 ,  Y10T83/0405 ,  Y10T83/0524 ,  Y10T156/1026 ,  Y10T156/1059 ,  Y10T156/1066 ,  Y10T156/1079 ,  Y10T156/13 ,  Y10T156/1357

Abstract: A method of cutting a wafer of composite core from a bulk composite core includes stabilizing the bulk composite core with a fixture, the bulk composite core having a plurality of tube members. The method also includes cutting through each of the tube members to create the wafer while the bulk composite core is stabilized by the fixture.

公开(公告)号：US09550347B2

公开(公告)日：2017-01-24

申请号：US13955105

申请日：2013-07-31

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  David G. Carlson

IPC: B32B37/00 ,  B32B37/14 ,  B32B3/12 ,  B64C1/18 ,  B64C3/20 ,  B32B5/14 ,  B29D99/00 ,  B29C65/48 ,  B29C65/78 ,  B32B5/12 ,  B32B7/12 ,  B32B3/04 ,  B32B38/00 ,  B29L31/30 ,  B29L31/60 ,  B29C65/00 ,  B29C65/50

CPC classification number: B32B37/146 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/486 ,  B29C65/5042 ,  B29C65/5057 ,  B29C65/7838 ,  B29C66/0042 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/5227 ,  B29C66/54 ,  B29C66/612 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/7254 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/8122 ,  B29C66/81261 ,  B29C66/81467 ,  B29C66/8185 ,  B29C66/8284 ,  B29C66/83415 ,  B29D99/0021 ,  B29L2031/3076 ,  B29L2031/3088 ,  B29L2031/608 ,  B32B3/04 ,  B32B3/12 ,  B32B5/12 ,  B32B5/142 ,  B32B7/12 ,  B32B2038/0076 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2307/302 ,  B32B2605/00 ,  B32B2605/18 ,  B64C1/18 ,  B64C3/20 ,  Y10T156/1093 ,  Y10T428/24149 ,  Y10T428/24165 ,  B29K2827/18 ,  B29K2307/04 ,  B29K2077/00 ,  B29K2309/08 ,  B29K2277/10 ,  B29K2071/00 ,  B29K2067/00 ,  B29K2061/00 ,  B29K2081/04 ,  B29K2063/00 ,  B29K2079/08 ,  B29K2031/00 ,  B29K2061/04

Abstract: A method of manufacturing a core stiffened structure includes orienting the plurality of core wafers in a non-uniform pattern onto a first face sheet, the non-uniform pattern producing non-uniform spacing between adjacent core wafers; assembling a second face sheet onto the plurality of wafers; and curing an adhesive to create a bond between the plurality of wafers, the first face sheet, and the second face sheet.

Abstract translation: 一种制造芯加强结构的方法包括以非均匀图案将多个芯晶片定向到第一面板上，该不均匀图案产生相邻芯片之间的不均匀间隔; 将第二面板组装到所述多个晶片上; 以及固化粘合剂以在所述多个晶片，所述第一面板和所述第二面板之间产生粘合。

公开(公告)号：US09302869B2

公开(公告)日：2016-04-05

申请号：US13782283

申请日：2013-03-01

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  Levi H. Armstrong ,  Elizabeth Oberle ,  Kathleen Oldham

IPC: B29C53/58 ,  B65H18/00 ,  B29C53/80 ,  B29C53/82 ,  B29C53/66

CPC classification number: B65H18/00 ,  B29C53/582 ,  B29C53/66 ,  B29C53/8016 ,  B29C53/821 ,  Y02T50/43

Abstract: A method of manufacturing a composite core can include: wrapping a mandrel in a mandrel wrapping process by securing a mandrel with a winding jig; orienting the composite material at a wrap angle to the mandrel; and depositing the composite material around a circumference of the mandrel. The method can further include assembling the wrapped mandrels in a tool and applying a pressure to the composite material during a curing cycle.

公开(公告)号：US20140246143A1

公开(公告)日：2014-09-04

申请号：US13782283

申请日：2013-03-01

Applicant: BELL HELICOPTER TEXTRON INC.

Inventor： Phillip A. Kendrick ,  Paul K. Oldroyd ,  Levi H. Armstrong ,  Elizabeth Oberle

IPC: B65H18/00

CPC classification number: B65H18/00 ,  B29C53/582 ,  B29C53/66 ,  B29C53/8016 ,  B29C53/821 ,  Y02T50/43

Abstract: A method of manufacturing a composite core can include: wrapping a mandrel in a mandrel wrapping process by securing a mandrel with a winding jig; orienting the composite material at a wrap angle to the mandrel; and depositing the composite material around a circumference of the mandrel. The method can further include assembling the wrapped mandrels in a tool and applying a pressure to the composite material during a curing cycle.

公开(公告)号：US10562202B2

公开(公告)日：2020-02-18

申请号：US15897934

申请日：2018-02-15

Applicant: Bell Helicopter Textron Inc.

Inventor： Phillip A. Kendrick ,  Levi H. Armstrong

IPC: B26D1/00 ,  B29D99/00 ,  B29C53/00 ,  B29C70/00 ,  B26D7/00 ,  B29C69/00 ,  B32B3/00 ,  B32B37/00 ,  B26D1/157 ,  B29C53/60 ,  B29C70/54 ,  B26D7/01 ,  B26D1/10 ,  B26D3/16 ,  B26D1/08 ,  B29C65/00 ,  B32B3/12 ,  B32B37/14 ,  B29C70/30

Abstract: A method of cutting a wafer of composite core from a bulk composite core includes stabilizing the bulk composite core with a fixture, the bulk composite core having a plurality of tube members. The method also includes cutting through each of the tube members to create the wafer while the bulk composite core is stabilized by the fixture.