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    FORMING SYSTEMS AND METHODS FOR DRAPE FORMING A COMPOSITE CHARGE
    1.
    发明申请
    FORMING SYSTEMS AND METHODS FOR DRAPE FORMING A COMPOSITE CHARGE 有权

    公开(公告)号：US20210245453A1

    公开(公告)日：2021-08-12

    申请号：US16787915

    申请日：2020-02-11

    申请人： The Boeing Company

    发明人： Richard V. Phillips ,  Jordan O. Birkland

    IPC分类号： B29C70/44 ,  B29C43/12 ,  B29C43/36

    摘要： Forming systems and methods for drape forming a composite charge are disclosed herein. The forming systems include a forming die having a forming surface configured to receive the composite charge and a collapsible support having a support surface. The forming surface has a forming surface edge that extends along a length of the forming surface, and the support surface has a die-proximate support surface edge that extends along the length of the support surface. The forming surface edge and the die-proximate support surface edge define a gap therebetween. A shape of the die-proximate support surface edge corresponds to a shape of the forming surface edge such that a gap width of the gap is at least substantially constant along a length of the gap. The collapsible support is configured to transition from an extended conformation to a collapsed conformation. The methods include methods of utilizing the systems.

    Systems and methods for assembling a skin of a composite structure
    3.
    发明授权
    Systems and methods for assembling a skin of a composite structure 有权
    组合复合结构皮肤的系统和方法

    公开(公告)号：US09511548B1

    公开(公告)日：2016-12-06

    申请号：US14055062

    申请日：2013-10-16

    申请人： The Boeing Company

    发明人： Daniel M. Rotter ,  Arvid J. Berg ,  Joseph D. Anderson ,  Kurtis Shuldberg Willden ,  Richard V. Phillips ,  Stephen Lee Metschan ,  Brad Andrew Coxon ,  Joseph J. Pruss

    IPC分类号： B29C70/44 ,  B29C65/00 ,  B32B37/10 ,  B32B38/00

    CPC分类号： B29C70/44 ,  B29C66/81455 ,  B29C66/8161 ,  B32B37/10 ,  B32B37/1018 ,  B32B38/0012

    摘要： Systems and methods for assembling a skin of a composite structure are disclosed herein. The methods include operatively attaching a charge of composite material to a flexible substrate to define an initial conformation for a composite-substrate assembly and locating the composite-substrate assembly and a layup mandrel proximal to one another. The methods further include pressing the composite-substrate assembly against an outer surface of the layup mandrel to deform the composite-substrate assembly to a final conformation. The methods also include affixing the charge of composite material to the outer surface of the layup mandrel and releasing the charge of composite material from the flexible substrate while retaining the charge of composite material on the outer surface of the layup mandrel. The systems include the flexible substrate, the layup mandrel, and an assembly deformation structure that is configured to press the composite-substrate assembly against the outer surface of the layup mandrel.

    摘要翻译： 本文公开了用于组装复合结构的皮肤的系统和方法。 所述方法包括将复合材料的电荷可操作地附接到柔性基底以限定复合 - 基底组件的初始构型并将复合 - 基底组件和叠层心轴相互靠近定位。 所述方法还包括将复合基板组件压靠在叠层心轴的外表面上以将复合衬底组件变形为最终构造。 这些方法还包括将复合材料的电荷附着到叠层心轴的外表面上，并将复合材料的电荷从柔性基底释放，同时将复合材料的电荷保持在叠层心轴的外表面上。 这些系统包括柔性基板，叠层心轴以及组合变形结构，其被构造成将复合基板组件压靠在叠层心轴的外表面上。

    Extruding nozzle, system, and method therefor
    4.
    发明授权
    Extruding nozzle, system, and method therefor 有权

    公开(公告)号：US11517866B2

    公开(公告)日：2022-12-06

    申请号：US17191952

    申请日：2021-03-04

    申请人： The Boeing Company

    发明人： Jeffrey H. Olberg ,  Stephen L. Metschan ,  Richard V. Phillips ,  Daniel J. Perron

    IPC分类号： B01J2/20

    摘要： A method for pelletizing an extruded material with an extruding nozzle includes inserting the extruded material into the extruding nozzle so that the extruded material flows through at least one material-flow channel, extending through a radiator of the extruding nozzle. Heat is transferred between the extruded material, flowing through the at least one material-flow channel, and the radiator. At least a portion of the radiator is located within a housing of the extruding nozzle.

    AUTOMATED FIBER PLACEMENT ROLLER
    5.
    发明申请
    AUTOMATED FIBER PLACEMENT ROLLER 有权

    公开(公告)号：US20220126531A1

    公开(公告)日：2022-04-28

    申请号：US17399876

    申请日：2021-08-11

    申请人： THE BOEING COMPANY

    发明人： Julie Frances Murphy ,  Adam La Gorce ,  Kevin F. Malik ,  Alexandra K. Dillon ,  Richard V. Phillips

    IPC分类号： B29C70/38

    摘要： A roller for automated fiber placement includes a flexible rim member arranged about a central axis. The flexible rim member has an inner side and an outer side, and the central axis is closer to the inner side than to the outer side. The roller also includes a hub member arranged substantially concentric with the flexible rim member about the central axis. The hub member defines an opening to receive a shaft of an automated fiber placement machine. The roller further includes a plurality of curved interconnect members extending between the hub member and the flexible rim member. Each of the plurality of curved interconnect members is elastically deformable to accommodate deformation of the flexible rim member. The roller also includes one or more roller skin layers coupled to the outer side of the flexible rim member.

    SYSTEMS, METHODS, AND VACUUM CHUCKS FOR TRANSFERRING FLEXIBLE ELONGATE BODIES
    8.
    发明申请
    SYSTEMS, METHODS, AND VACUUM CHUCKS FOR TRANSFERRING FLEXIBLE ELONGATE BODIES 有权
    系统，方法和真空夹头用于传输柔性的双轴体

    公开(公告)号：US20160251091A1

    公开(公告)日：2016-09-01

    申请号：US14633979

    申请日：2015-02-27

    申请人： The Boeing Company

    发明人： Daniel M. Rotter ,  Kieran Patrick Davis ,  Stephen Lee Metschan ,  Richard V. Phillips ,  Joseph J. Pruss

    IPC分类号： B64F5/00 ,  B23Q3/08

    CPC分类号： B64F5/40 ,  B23Q3/088 ,  B25B11/005 ,  B64F5/50 ,  B66C1/0243 ,  B66C1/0256 ,  B66C1/0281

    摘要： Systems, methods, and vacuum chucks for transferring flexible elongate bodies are disclosed herein. The vacuum chucks include an elongate rigid support, a vertically oriented vacuum surface, a vacuum manifold, and a skirt seal. The systems include an elongate horizontal support structure, a transfer structure, a plurality of vertical linkages, which are operatively attached to the elongate horizontal support structure, and a plurality of vacuum chucks. Each of the plurality of vacuum chucks is operatively attached to a respective one of the plurality of vertical linkages. The methods include suspending an elongate horizontal support structure with a transfer structure, aligning each of a plurality of vacuum chucks with a respective portion of a vertical surface of a flexible elongate body, selectively actuating each of the plurality of vacuum chucks to retain the respective portion of the vertical surface of the flexible elongate body, and lifting the flexible elongate body.

    摘要翻译： 本文公开了用于传送柔性细长体的系统，方法和真空吸盘。 真空吸盘包括细长的刚性支撑件，垂直取向的真空表面，真空歧管和裙部密封件。 这些系统包括细长的水平支撑结构，转移结构，可操作地连接到细长的水平支撑结构的多个垂直连杆以及多个真空吸盘。 多个真空吸盘中的每一个可操作地连接到多个垂直连杆中的相应一个。 所述方法包括用传递结构悬挂细长的水平支撑结构，将多个真空卡盘中的每一个与柔性细长主体的垂直表面的相应部分对准，选择性地致动多个真空卡盘中的每一个以保持相应部分 的柔性细长体的垂直表面，以及提升柔性细长体。

    Systems of forming a skin for a composite structure
    10.
    发明授权
    Systems of forming a skin for a composite structure 有权

    公开(公告)号：US10226915B1

    公开(公告)日：2019-03-12

    申请号：US14926298

    申请日：2015-10-29

    申请人： The Boeing Company

    发明人： Stephen Lee Metschan ,  Richard V. Phillips ,  Kurtis S. Willden

    IPC分类号： B29C70/30 ,  B32B37/14 ,  B32B37/10 ,  B32B37/06 ,  B29C70/54

    摘要： Systems and methods of forming a skin for a composite structure and composite structures including the same. The systems and methods include operatively attaching a charge of composite material to a flexible substrate to define a composite-substrate assembly. The systems and methods further include deforming the composite-substrate assembly by conforming the composite-substrate assembly to a non-planar pre-forming surface of a pre-forming mandrel to define a non-planar skin surface contour on the charge of composite material. The systems and methods further include maintaining the charge of composite material in tension in a direction that is parallel to an interface between the charge of composite material and the flexible substrate during the deforming.