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    Method and device for adhesively joining large-surface components in vehicle construction
    7.
    发明授权
    Method and device for adhesively joining large-surface components in vehicle construction 有权
    在车辆结构中粘接大面积部件的方法和装置

    公开(公告)号：US08968500B2

    公开(公告)日：2015-03-03

    申请号：US13221279

    申请日：2011-08-30

    Applicant: Dirk Niermann ,  Holger Frauen

    Inventor： Dirk Niermann ,  Holger Frauen

    IPC: B32B41/00 ,  B64F5/00 ,  B05C11/10 ,  B64C1/06 ,  B05C5/02 ,  B05C13/02 ,  B62D27/02 ,  B62D65/02

    CPC classification number: B64F5/0009 ,  B05C5/0216 ,  B05C11/1021 ,  B05C13/02 ,  B62D27/026 ,  B62D65/028 ,  B64C1/068 ,  B64F5/10

    Abstract: A method for joining, by adhesive bonding, at least two large joining partners in vehicle construction, in particular in aircraft construction, comprises the following steps: detecting the geometric data of the joining partners in an automated manner, detecting the joint gap dimensions of the joining partners from the geometric data, applying adhesive to one or both joint faces of the two joining partners to be joined as a function of the joint gap dimensions, joining the joining partners in the joining position, and sequentially applying joining pressure to the joint faces along the joint gap to bring the joining partners into the final joining position.

    Abstract translation: 一种用于通过粘合剂粘合在车辆结构中，特别是飞机结构中的至少两个大的接合伙伴的方法包括以下步骤：以自动方式检测接合伙伴的几何数据，检测接合伙伴的接合间隙尺寸 从所述几何数据接合伙伴，根据所述接合间隙尺寸将所述两个接合伙伴的一个或两个接合面施加粘合剂，将所述接合部件接合在所述接合位置，以及将接合压力依次施加到所述接合面 沿着联合差距，使加盟伙伴进入最终加盟的位置。

    METHOD FOR MOUNTING A PYLON TO AN AIRCRAFT
    8.
    发明申请
    METHOD FOR MOUNTING A PYLON TO AN AIRCRAFT 有权
    将PYLON安装到飞机上的方法

    公开(公告)号：US20150013142A1

    公开(公告)日：2015-01-15

    申请号：US13939526

    申请日：2013-07-11

    Applicant: Spirit AeroSystems, Inc.

    Inventor： Randall Ray West

    IPC: B64F5/00 ,  B64D27/26

    CPC classification number: B64F5/0009 ,  B64D27/18 ,  B64D27/26 ,  B64D2027/262 ,  B64D2027/264 ,  Y10T29/49826 ,  Y10T29/49893 ,  Y10T29/49947 ,  Y10T29/49948 ,  Y10T29/49959 ,  Y10T29/49963

    Abstract: An assembly and method for attaching an engine pylon to an aircraft wing. The method may include attaching a first forward wing-mounted fitting to the pylon at a first side of the pylon between upper and lower spars of the pylon and attaching a second forward wing-mounted fitting to the pylon at a second side of the pylon between the upper and lower spars of the pylon. The second side of the pylon is located opposite of the first side of the pylon. Mechanical attachment devices may be inserted through holes on the sides of the pylon aligned with holes formed through the forward wing-mounted fittings. The mechanical attachment devices may be made of steel and the forward wing-mounted fittings may be made of composite or aluminum material.

    Abstract translation: 用于将发动机吊架连接到飞机机翼的组件和方法。 该方法可以包括在塔架的上部和下部翼梁之间的第二侧安装在塔架的第一侧上的第一前翼安装的配件到塔架上，并且在塔架的第二侧将第二前翼架安装件连接到塔架 塔架的上下翼梁。 塔架的第二面位于塔架第一侧的对面。 机械附接装置可以插入通过与通过前翼安装的配件形成的孔对准的塔的侧面上的孔。 机械附接装置可以由钢制成，并且前翼安装的配件可以由复合材料或铝材料制成。

    DUAL FUNCTION MOVEMENT COMPONENT FOR AUTOMATED ASSEMBLY SYSTEMS
    9.
    发明申请
    DUAL FUNCTION MOVEMENT COMPONENT FOR AUTOMATED ASSEMBLY SYSTEMS 有权
    自动组装系统的双功能运动部件

    公开(公告)号：US20140115894A1

    公开(公告)日：2014-05-01

    申请号：US13663805

    申请日：2012-10-30

    Applicant: The Boeing Company

    Inventor： James Darryl Gamboa

    IPC: B21D53/92 ,  B25B11/00

    CPC classification number: B23Q9/0007 ,  B25B11/00 ,  B60V1/043 ,  B62D57/024 ,  B64F5/0009 ,  Y10T29/49 ,  Y10T29/49622

    Abstract: A pneumatic device may be configured and used to provide multiple movement related functions, such as in an automated assembly system. The pneumatic device may comprise a chamber; a sealing element configurable to contact a surface, to enable creating a seal around the chamber by application of pneumatic suction into the chamber; a biasing element configurable to push the sealing element away from the surface; and a pneumatic cushion configurable to expand by application of pneumatic inflow, thus urging the pneumatic device away from the surface.

    Abstract translation: 气动装置可以被配置和用于提供多个与运动相关的功能，例如在自动装配系统中。 气动装置可包括腔室; 可配置为接触表面的密封元件，以便通过将空气吸力施加到所述腔室中而能够在所述腔周围产生密封; 偏置元件，其可配置成将所述密封元件推离所述表面; 气动垫可配置为通过施加气动流入而膨胀，从而将气动装置推离表面。

    ACTUATING SYSTEM OF SECTORS OF A DEVICE FOR PRODUCING AN AIRPLANE FUSELAGE
    10.
    发明申请
    ACTUATING SYSTEM OF SECTORS OF A DEVICE FOR PRODUCING AN AIRPLANE FUSELAGE 有权
    用于生产机场配件的装置的动作执行系统

    公开(公告)号：US20130298365A1

    公开(公告)日：2013-11-14

    申请号：US13852021

    申请日：2013-03-28

    Applicant: Alenia Aermacchi S.p.A.

    Inventor： Guido SIBONA ,  Ettore Mostarde ,  Giuseppe Iovine

    IPC: B64F5/00

    CPC classification number: B64F5/0009 ,  B29C33/485 ,  B29C53/824 ,  B64F5/10 ,  F16H25/2021 ,  F16H2025/249 ,  Y02T50/43 ,  Y10T29/53961

    Abstract: An actuating system of sectors of a device for producing an airplane fuselage in which a lamination mandrel comprises a plurality of sectors angularly spaced about the axis and mobile along guides between: an expanded lamination position and a contracted disassembling position. Each sector is provided with an actuating system of the screw—nut screw type in which a threaded element is rotated about a rotation axis by a motor. The threaded element comprises an internal shaft made of a first material and extending along the rotation axis and an external tubular portion made of a second material, mounted axially on a portion of the shaft and provided externally with a thread.

    Abstract translation: 一种用于生产飞机机身的装置的扇区的致动系统，其中层压心轴包括围绕所述轴线成角度地间隔开的多个扇区，并且可沿着引导件移动：扩展的层压位置和收缩的拆卸位置。 每个扇区设置有螺杆螺母型的致动系统，螺纹元件通过电动机围绕旋转轴线旋转。 螺纹元件包括由第一材料制成并沿着旋转轴线延伸的内轴和由第二材料制成的外部管状部分，其轴向安装在轴的一部分上并且在外部设置有螺纹。

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