Mechanical excavating machines including rotary cutter and suction tube
    1.
    发明授权
    Mechanical excavating machines including rotary cutter and suction tube 失效
    机械挖掘机包括旋转切割机和吸管

    公开(公告)号:US3930324A

    公开(公告)日:1976-01-06

    申请号:US467481

    申请日:1974-05-06

    摘要: A mechanical hole digging machine comprising a rotary cutting tool and a suction tube having an inlet opening adjacent to the cutting tool, a suction device for applying suction to the tube remote from the inlet opening to cause material cut away by the cutting tool to be sucked inwards through the inlet opening, the cutting tool and part at least of the suction tube being carried on a mounting by which they are movable upwards and downwards. An electromagnetic metal detector comprising three coils is mounted near the cutter head and adapted in use to give an indication of the presence of buried metal service pipe during a hole digging operation.

    摘要翻译: 一种机械孔挖掘机,包括旋转切割工具和具有与切割工具相邻的入口的抽吸管,用于向远离入口开口的管提供吸力的抽吸装置,以引起切割工具被切割的材料被吸入 向内通过入口开口,切割工具和至少吸入管的部分被承载在它们可上下移动的安装件上。 包括三个线圈的电磁金属检测器安装在切割头附近,并适于在钻孔操作期间给出埋藏金属管道的存在的指示。

    Method of manufacturing structural parts, particularly for use in
aircraft
    2.
    发明授权
    Method of manufacturing structural parts, particularly for use in aircraft 失效
    制造结构件的方法,特别适用于飞机

    公开(公告)号:US6039239A

    公开(公告)日:2000-03-21

    申请号:US979149

    申请日:1997-11-26

    摘要: The present invention provides a method of making a frame, particularly for the aircraft industry, having a central member (34) and one or more cantilever ribs (32); such a frame can be made by forging or machining but these are time-consuming and expensive. According to the present invention such frames are made by diffusion bonding and superplastic forming techniques, whereby a pack of sheets are bonded together except in certain areas. Gas is injected into those areas to inflate the pack superplastically to form one or more closed cells (16). The top of the cells is then machined off along line 23, while the side walls of the cells are retained, to provide a frame having cantilever ribs (32).

    摘要翻译: 本发明提供一种制造具有中心构件(34)和一个或多个悬臂肋(32)的框架的方法,特别是用于飞机工业的框架。 这样的框架可以通过锻造或机械加工制造,但是这些框架是耗时且昂贵的。 根据本发明,这种框架通过扩散粘合和超塑性成形技术制成,由此除了某些区域之外,一组片材粘合在一起。 将气体注入到这些区域中以超塑性膨胀以形成一个或多个闭孔(16)。 然后,沿着线23加工细胞的顶部,同时保持细胞的侧壁,以提供具有悬臂肋(32)的框架。

    Structural parts for use in aircraft
    3.
    发明授权
    Structural parts for use in aircraft 失效
    用于飞机的结构件

    公开(公告)号:US5809737A

    公开(公告)日:1998-09-22

    申请号:US573970

    申请日:1995-12-15

    IPC分类号: B21D26/055 B21D47/00 E04C2/34

    摘要: The present invention provides a method of making a frame, particularly for the aircraft industry, having a central member (34) and one or more cantilever ribs (32); such a frame can be made by forging or machining but these are time-consuming and expensive. According to the present invention such frames are made by diffusion bonding and superplastic forming techniques, whereby a pack of sheets are bonded together except in certain areas. Gas is injected into those areas to inflate the pack superplastically to form one or more closed cells (16). The top of the cells is then machined off along line 23, while the side walls of the cells are retained, to provide a frame having cantilever ribs (32).

    摘要翻译: 本发明提供一种制造具有中心构件(34)和一个或多个悬臂肋(32)的框架的方法,特别是用于飞机工业的框架。 这样的框架可以通过锻造或机械加工制造,但是这些框架是耗时且昂贵的。 根据本发明,这种框架通过扩散粘合和超塑性成形技术制成,由此除了某些区域之外,一组片材粘合在一起。 将气体注入到这些区域中以超塑性膨胀以形成一个或多个闭孔(16)。 然后,沿着线23加工细胞的顶部,同时保持细胞的侧壁,以提供具有悬臂肋(32)的框架。