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77 条记录 (耗时 0.032 秒)

    Automated filling machine and associated method
    4.
    发明授权
    Automated filling machine and associated method 失效
    自动灌装机及相关方法

    公开(公告)号：US06739111B2

    公开(公告)日：2004-05-25

    申请号：US09949432

    申请日：2001-09-06

    申请人： David P. Banks ,  Darrell D. Jones

    发明人： David P. Banks ,  Darrell D. Jones

    IPC分类号： B65B116

    CPC分类号： B65B3/12 ,  B65B43/44 ,  B65B43/54

    摘要： An apparatus for filling a plurality of tubes is disclosed. The apparatus includes a positioning device that directs a tube from a hopper to a labeler where a label is applied to the tube. The positioning device further directs the tube to one of a plurality of filling stations where a continuous flow of filling material is dispensed into the tube. The tube is then directed to a capping device where a cap is applied to an end of the tube.

    摘要翻译： 公开了一种用于填充多个管的装置。 该装置包括定位装置，其将管从料斗引导到标签施加到管的标签机上。 定位装置还将管引导到多个填充站中的一个，其中将填充材料的连续流分配到管中。 然后将管导向到封盖装置，其中帽被施加到管的端部。

    Lap splice mini-riveter system
    6.
    发明授权
    Lap splice mini-riveter system 有权
    拉链拼接迷你铆钉系统

    公开(公告)号：US6073326A

    公开(公告)日：2000-06-13

    申请号：US198807

    申请日：1998-11-24

    申请人： David P. Banks ,  James N. Buttrick, Jr. ,  Charles H. Glaisyer ,  Darrell D. Jones ,  Russell C. McCrum ,  Philip M. Wright

    发明人： David P. Banks ,  James N. Buttrick, Jr. ,  Charles H. Glaisyer ,  Darrell D. Jones ,  Russell C. McCrum ,  Philip M. Wright

    IPC分类号： B21J15/10 ,  B21J15/28 ,  B23Q1/02

    CPC分类号： B21J15/142 ,  B21J15/10 ,  B21J15/28 ,  Y10T29/5118 ,  Y10T29/5191 ,  Y10T29/53978

    摘要： The present invention relates to a portable process for automated fastening of aircraft structures. The invention will employ two primary elements for locating and installing through-the-skin fasteners. Inside and outside units are attached onto an airframe and indexed to each other through coordination holes that have been pre-drilled through the structure. The aircraft structure is assembled with the pre-drilled coordination holes by aligning adjacent airframe parts and inserting alignment pins. The alignment pins will provide a degree of clamping to pull the parts together and provide indexing for inside and outside vacuum attachment track systems. The invention is equipped to traverse along the track system, accurately position itself, and drill only or countersink a hole, insert a fastener, and fasten, i.e., upset a rivet, or run down a threaded nut, then reposition itself to the next fastener location and repeat the process.

    摘要翻译： 本发明涉及一种用于飞机结构的自动紧固的便携式方法。 本发明将采用两个主要元件来定位和安装通过皮肤的紧固件。 内部和外部单元通过已经通过结构预钻孔的协调孔而附接到机身上并彼此分离。 飞机结构通过对准相邻的机身部件并插入对准销，与预钻孔的协调孔组装。 定位销将提供一定程度的夹紧，将部件拉在一起，并为内部和外部真空连接轨道系统提供分度。 本发明被配备为沿着轨道系统横向移动，精确定位自身，仅钻孔或锪孔，插入紧固件，并固定，即压住铆钉，或者沿着螺纹螺母倒下，然后将其自身重新定位到下一个紧固件 位置并重复该过程。