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    SYSTEMS AND METHODS FOR DEFINING A SURFACE CONTOUR OF A LAYERED CHARGE OF MATERIAL
    1.
    发明申请
    SYSTEMS AND METHODS FOR DEFINING A SURFACE CONTOUR OF A LAYERED CHARGE OF MATERIAL 有权
    用于定义材料层状电荷的表面轮廓的系统和方法

    公开(公告)号：US20150352795A1

    公开(公告)日：2015-12-10

    申请号：US14295884

    申请日：2014-06-04

    Applicant: The Boeing Company

    Inventor： Brad Andrew Coxon ,  Kurtis Shuldberg Willden ,  Kieran P. Davis

    IPC: B29C70/34 ,  B29C70/78

    CPC classification number: B29C70/342 ,  B29C33/48 ,  B29C70/78 ,  B29C2043/3649 ,  B29K2105/0872 ,  Y02T50/43

    Abstract: Systems and methods for defining a surface contour of a layered charge of material are disclosed herein. The systems include a forming die, which includes a forming surface shaped to define a desired surface contour of the layered charge, and a fluidly actuated support, which includes a support surface that is adjacent to the forming surface and located to support the layered charge. The systems further include a vacuum bag that at least partially defines an enclosed volume and a vacuum source configured to selectively apply a vacuum to the enclosed volume. The methods include locating the layered charge on the forming surface and on the support surface, covering the layered charge with the vacuum bag to define the enclosed volume, applying the vacuum to the enclosed volume, compressing the fluidly actuated support, translating the support surface, and deforming the layered charge to define the desired surface contour.

    Abstract translation: 本文公开了用于限定层状电荷材料的表面轮廓的系统和方法。 该系统包括成形模，其包括成形为形成分层电荷的期望表面轮廓的成形表面，以及流体致动的支撑件，其包括邻近成形表面并被定位成支撑层状电荷的支撑表面。 系统还包括至少部分地限定封闭容积的真空袋和构造成选择性地将真空施加到封闭容积的真空源。 所述方法包括将成层表面和支撑表面上的分层电荷定位，用真空袋覆盖层状电荷以限定封闭体积，将真空施加到封闭容积，压缩流体致动支撑件，平移支撑表面， 并使分层电荷变形以限定所需的表面轮廓。

    VENTILATION SYSTEMS FOR USE WITH A PLASMA TREATMENT SYSTEM
    3.
    发明申请
    VENTILATION SYSTEMS FOR USE WITH A PLASMA TREATMENT SYSTEM 有权
    使用等离子体处理系统的通风系统

    公开(公告)号：US20160379808A1

    公开(公告)日：2016-12-29

    申请号：US14748466

    申请日：2015-06-24

    Applicant: THE BOEING COMPANY

    Inventor： Benjamin Jeffrey Stephenson ,  Richard Allen Miller, II ,  Kieran P. Davis ,  Marcus Anthony Belcher

    IPC: H01J37/32 ,  B08B15/02

    CPC classification number: H01J37/32834 ,  B08B15/04 ,  H01J37/32844 ,  Y02C20/30

    Abstract: A gas containment apparatus for use with an end effector including at least one plasma head includes at least one enclosing structure coupled to the end effector. The enclosing structure is configured to capture a gas produced by the at least one plasma head. The gas containment apparatus also includes a duct coupled to the at least one enclosing structure and configured to channel the gas from within the enclosing structure.

    Abstract translation: 一种用于包括至少一个等离子体头部的末端执行器的气体封存装置包括耦合到端部执行器的至少一个封闭结构。 封闭结构构造成捕获由至少一个等离子体头产生的气体。 气体收容装置还包括连接到至少一个封闭结构并被构造成从封闭结构内引导气体的管道。

    Systems and methods for compacting a charge of composite material
    7.
    发明授权
    Systems and methods for compacting a charge of composite material 有权
    用于压实复合材料的电荷的系统和方法

    公开(公告)号：US09314976B2

    公开(公告)日：2016-04-19

    申请号：US13769022

    申请日：2013-02-15

    Applicant: The Boeing Company

    Inventor： Brian Gregory Robins ,  Daniel M. Rotter ,  Kieran P. Davis ,  Mark E. King

    IPC: B29C65/00 ,  B32B37/00 ,  B29C70/44 ,  B29C43/36 ,  B29C43/10

    CPC classification number: B29C70/44 ,  B29C43/10 ,  B29C43/36 ,  B29C2043/3605

    Abstract: Systems and methods for compacting a charge of composite material. These systems and methods may utilize a vacuum compaction device to compact the charge of composite material on a supporting surface. The vacuum compaction device may be reusable and may be configured to define an enclosed volume when positioned on the supporting surface and may include a barrier structure and a sealing structure that is configured to form a fluid seal when compressed between the supporting surface and the barrier structure. The vacuum compaction device also may include a vacuum distribution manifold that is in fluid communication with and configured to selectively apply a vacuum to the enclosed volume. Application of the vacuum to the enclosed volume may decrease a pressure within the enclosed volume and transition the vacuum compaction device from an undeformed configuration to a deformed configuration, thereby compacting the charge of composite material on the supporting surface.

    Abstract translation: 用于压实复合材料的电荷的系统和方法。 这些系统和方法可以利用真空压实装置来压缩支撑表面上的复合材料的电荷。 真空压实装置可以是可重复使用的，并且可以被配置为当定位在支撑表面上时限定封闭容积，并且可以包括阻挡结构和密封结构，所述阻挡结构和密封结构被构造成当在支撑表面和阻挡结构之间被压缩时形成流体密封 。 真空压实装置还可以包括真空分配歧管，该真空分配歧管与封闭容积选择性地施加真空。 将真空施加到封闭容积中可以减小封闭体积内的压力并将真空压实装置从未变形的构型转变为变形构型，从而压实支撑表面上的复合材料的电荷。

    SYSTEMS AND METHODS FOR COMPACTING A CHARGE OF COMPOSITE MATERIAL
    8.
    发明申请
    SYSTEMS AND METHODS FOR COMPACTING A CHARGE OF COMPOSITE MATERIAL 有权
    用于计算复合材料电荷的系统和方法

    公开(公告)号：US20140367039A1

    公开(公告)日：2014-12-18

    申请号：US13769022

    申请日：2013-02-15

    Applicant: The Boeing Company

    Inventor： BRIAN GREGORY ROBINS ,  Daniel M. Rotter ,  Kieran P. Davis ,  Mark E. King

    IPC: B32B37/10

    CPC classification number: B29C70/44 ,  B29C43/10 ,  B29C43/36 ,  B29C2043/3605

    Abstract: Systems and methods for compacting a charge of composite material. These systems and methods may utilize a vacuum compaction device to compact the charge of composite material on a supporting surface. The vacuum compaction device may be reusable and may be configured to define an enclosed volume when positioned on the supporting surface and may include a barrier structure and a sealing structure that is configured to form a fluid seal when compressed between the supporting surface and the barrier structure. The vacuum compaction device also may include a vacuum distribution manifold that is in fluid communication with and configured to selectively apply a vacuum to the enclosed volume. Application of the vacuum to the enclosed volume may decrease a pressure within the enclosed volume and transition the vacuum compaction device from an undeformed configuration to a deformed configuration, thereby compacting the charge of composite material on the supporting surface.

    Abstract translation: 用于压实复合材料的电荷的系统和方法。 这些系统和方法可以利用真空压实装置来压缩支撑表面上的复合材料的电荷。 真空压实装置可以是可重复使用的，并且可以被配置为当定位在支撑表面上时限定封闭容积，并且可以包括阻挡结构和密封结构，该阻挡结构和密封结构被构造成当在支撑表面和阻挡结构之间被压缩时形成流体密封 。 真空压实装置还可以包括真空分配歧管，该真空分配歧管与封闭容积选择性地施加真空。 将真空施加到封闭容积中可以减小封闭体积内的压力并将真空压实装置从未变形的构型转变为变形构型，从而压实支撑表面上的复合材料的电荷。

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