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    Object design using machine-learning model
    6.
    发明授权
    Object design using machine-learning model 有权

    公开(公告)号：US11256231B2

    公开(公告)日：2022-02-22

    申请号：US16287599

    申请日：2019-02-27

    申请人： THE BOEING COMPANY

    发明人： Phillip John Crothers ,  Carla Elizabeth Reynolds ,  Alexander Rubin ,  Samuel J. Tucker ,  Gregg Robert Bogucki ,  Joshua David Kalin

    IPC分类号： G05B19/4099 ,  B33Y50/02 ,  G06F30/15 ,  B29C70/38 ,  G05B13/02 ,  G06F119/18

    摘要： A system to aid in design for manufacturing an object includes a processor and a memory configured to store instructions. The processor is configured to receive first data representing a design of the object to be manufactured and second data representing a machine-learning model. The processor is configured to execute the instructions to generate third data using the first data and the second data. The third data indicates at least one of a modification to the design of the object or process conditions for production of the object. The processor is configured to send the design of the object, the process conditions, or both, to a manufacturing tool to enable production of the object. The machine-learning model is representative of production data and based at least partially on one or more of: object features, process parameters, environmental factors, and quality data.

    MATERIAL SYSTEMS AND METHODS OF MANUFACTURING MATERIAL SYSTEMS
    7.
    发明申请
    MATERIAL SYSTEMS AND METHODS OF MANUFACTURING MATERIAL SYSTEMS 审中-公开

    公开(公告)号：US20180162101A1

    公开(公告)日：2018-06-14

    申请号：US15378931

    申请日：2016-12-14

    申请人： The Boeing Company

    发明人： Patrick Bickford Stickler ,  Alexander Rubin

    IPC分类号： B32B15/14 ,  B32B5/02 ,  B32B15/04 ,  B32B15/20 ,  B32B5/26 ,  B29C65/02 ,  B29C43/56 ,  B29C65/00

    摘要： A material system may include: an aluminum layer; a glass composite layer adjacent to the first aluminum layer; and a carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that may include thermoplastic prepreg plies, and carbon composite layer so that the aluminum layer is adjacent to the glass composite layer, and the glass composite layer is adjacent to the carbon composite layer; and consolidating the thermoplastic prepreg plies to soften the aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that comprises thermoplastic resin, and carbon composite layer so that the glass composite layer is between the aluminum and carbon composite layers; and adjusting temperature and pressure to consolidate the stack.

    Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
    10.
    发明授权
    Laminate structures comprising fiber-reinforced thermoplastic prepreg plies 有权

    公开(公告)号：US11014337B2

    公开(公告)日：2021-05-25

    申请号：US15378982

    申请日：2016-12-14

    申请人： The Boeing Company

    发明人： Patrick Bickford Stickler ,  Alexander Rubin

    IPC分类号： B32B15/14 ,  B32B5/02 ,  B32B5/26 ,  B32B15/20 ,  B32B7/12 ,  B29C70/88

    摘要： A laminate structure may include: an aluminum layer; a glass composite layer adjacent to the aluminum layer; and/or a carbon composite layer adjacent to the glass composite layer, opposite to the aluminum layer. The glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies. A laminate structure may include: a first aluminum layer; a first glass composite layer adjacent to the first aluminum layer; a first carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer; and/or a second glass composite layer adjacent to the first carbon composite layer, and opposite to the first glass composite layer. The first glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The first carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies.