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    METHOD AND SYSTEM FOR MANUFACTURING NOODLES OF STRUCTURAL JOINTS
    2.
    发明申请
    METHOD AND SYSTEM FOR MANUFACTURING NOODLES OF STRUCTURAL JOINTS 审中-公开

    公开(公告)号：US20200276772A1

    公开(公告)日：2020-09-03

    申请号：US16878351

    申请日：2020-05-19

    申请人： The Boeing Company

    发明人： Christian Gordon

    IPC分类号： B29C70/34 ,  B29C70/54 ,  B29C65/48 ,  B32B3/28 ,  B32B37/14 ,  B29B11/16 ,  B29D99/00 ,  B29C70/52

    摘要： A method of manufacturing a noodle of a structural joint that comprises pulling a first composite sheet through a first splitting station to cut the first composite sheet into a plurality of first composite plies, pulling the plurality of first composite plies through a first alignment station to stack the plurality of first composite plies on top of each other to form a first stacked composite layup, pulling the first stacked composite layup through a first heating station to heat the first stacked composite layup to form a first heated composite layup, pulling the first heated composite layup through a first forming station to shape the first heated composite layup into a first pre-selected cross-sectional shape to form at least a first portion of a continuous noodle, and pulling at least the first portion of the continuous noodle through a cutting station to cut at least the first portion of the continuous noodle to a pre-selected length.

    Method and system for manufacturing noodles of structural joints
    4.
    发明授权
    Method and system for manufacturing noodles of structural joints 有权

    公开(公告)号：US11241845B2

    公开(公告)日：2022-02-08

    申请号：US16878351

    申请日：2020-05-19

    申请人： The Boeing Company

    发明人： Christian Gordon

    IPC分类号： B29C70/34 ,  B29C70/54 ,  B29C65/48 ,  B32B3/28 ,  B32B37/14 ,  B29B11/16 ,  B29D99/00 ,  B29C70/52 ,  B29L31/30

    摘要： A method of manufacturing a noodle of a structural joint that comprises pulling a first composite sheet through a first splitting station to cut the first composite sheet into a plurality of first composite plies, pulling the plurality of first composite plies through a first alignment station to stack the plurality of first composite plies on top of each other to form a first stacked composite layup, pulling the first stacked composite layup through a first heating station to heat the first stacked composite layup to form a first heated composite layup, pulling the first heated composite layup through a first forming station to shape the first heated composite layup into a first pre-selected cross-sectional shape to form at least a first portion of a continuous noodle, and pulling at least the first portion of the continuous noodle through a cutting station to cut at least the first portion of the continuous noodle to a pre-selected length.

    Method and system for manufacturing noodles of structural joints
    5.
    发明授权
    Method and system for manufacturing noodles of structural joints 有权

    公开(公告)号：US10703053B2

    公开(公告)日：2020-07-07

    申请号：US15642585

    申请日：2017-07-06

    申请人： The Boeing Company

    发明人： Christian Gordon

    IPC分类号： B29C70/34 ,  B29C70/54 ,  B29C65/48 ,  B32B3/28 ,  B32B37/14 ,  B29B11/16 ,  B29D99/00 ,  B29C70/52 ,  B29L31/30

    摘要： A method of manufacturing a noodle of a structural joint that comprises pulling a first composite sheet through a first splitting station to cut the first composite sheet into a plurality of first composite plies, pulling the plurality of first composite plies through a first alignment station to stack the plurality of first composite plies on top of each other to form a first stacked composite layup, pulling the first stacked composite layup through a first heating station to heat the first stacked composite layup to form a first heated composite layup, pulling the first heated composite layup through a first forming station to shape the first heated composite layup into a first pre-selected cross-sectional shape to form at least a first portion of a continuous noodle, and pulling at least the first portion of the continuous noodle through a cutting station to cut at least the first portion of the continuous noodle to a pre-selected length.

    FABRICATION OF GAP FILLERS FOR COMPOSITE PARTS THAT EXHIBIT VARYING RADII OF CURVATURE
    6.
    发明申请
    FABRICATION OF GAP FILLERS FOR COMPOSITE PARTS THAT EXHIBIT VARYING RADII OF CURVATURE 审中-公开

    公开(公告)号：US20190091945A1

    公开(公告)日：2019-03-28

    申请号：US15718704

    申请日：2017-09-28

    申请人： The Boeing Company

    发明人： Christian Gordon ,  Andrew Klimovski

    IPC分类号： B29C70/20 ,  B29C70/52 ,  B29C70/56

    摘要： Systems and methods are provided for fabricating preforms. One embodiment is a method comprising acquiring tows of fiber reinforced material, selecting a number of tows to utilize for a bundle having an aggregate shape, assembling the tows together into the bundle, curving the assembled tows by slipping the assembled tows with respect to each other, drawing the bundle through a die to bind the bundle into a preform, enforcing a longitudinally varying cross section along the preform, and locking in a curvature of the preform.