Modular stanchion system
    3.
    发明授权
    Modular stanchion system 有权
    模块化支柱系统

    公开(公告)号:US09272793B2

    公开(公告)日:2016-03-01

    申请号:US14265946

    申请日:2014-04-30

    Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

    Abstract translation: 一种用于在翼组件支撑高度处支撑翼组件的装置。 提供基部,每个具有相对于彼此具有不同的预定高度。 可移动平台承载多个基部部分,并且多个翼组件支撑部分搁置在基部上并且包括翼组件连接器,其可在第一平面中移动,第二平面相对于第一平面大致垂直。 在翼组件支撑高度和平台的组合高度和翼组件连接器的高度之间相对于翼组件支撑部分的底部限定差速高度。 基座部分中的至少一个具有接近差速高度的预定高度并且在平台上承载。 翼组件支撑部分在该基部上承载。

    Metrology System for Positioning Assemblies
    5.
    发明申请
    Metrology System for Positioning Assemblies 有权
    定位组件计量系统

    公开(公告)号:US20150314891A1

    公开(公告)日:2015-11-05

    申请号:US14559034

    申请日:2014-12-03

    Abstract: A method and apparatus for maintaining a selected configuration for a structure during a manufacturing process for forming a product using the structure. Metrology data for a support system is received. The support system holds the structure during the manufacturing process. A determination is made as to whether a current configuration of the structure is within selected tolerances of the selected configuration for the structure based on the metrology data. The support system is reconfigured to move the structure into the selected configuration in response to a determination that the current configuration of the structure is not within the selected tolerances of the selected configuration for the structure.

    Abstract translation: 一种用于在用于使用该结构形成产品的制造过程期间保持用于结构的所选构造的方法和装置。 收到支持系统的计量数据。 支撑系统在制造过程中保持结构。 确定结构的当前配置是否在基于测量数据的结构的所选配置的选定公差内。 响应于确定结构的当前配置不在所选择的结构的配置的公差内,支持系统被重新配置为将结构移动到所选择的配置中。

    Flexible Manufacturing System for Aircraft Structures
    6.
    发明申请
    Flexible Manufacturing System for Aircraft Structures 审中-公开
    飞机结构柔性制造系统

    公开(公告)号:US20150314889A1

    公开(公告)日:2015-11-05

    申请号:US14558867

    申请日:2014-12-03

    Abstract: A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.

    Abstract translation: 一种用于制造飞行器结构的方法和装置。 可驱动支撑件可以从第一位置驱动到第二位置,以将可驱动支撑件与至少一个其它可驱动支撑件一起形成可驱动的支撑系统。 可以使用可驱动的支撑系统将结构保持在期望的位置。

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