Method of conveying articles hanging on hangers and devices for use in
the method
    1.
    发明授权
    Method of conveying articles hanging on hangers and devices for use in the method 失效
    输送挂在衣架上的物品的方法,用于该方法

    公开(公告)号:US5971131A

    公开(公告)日:1999-10-26

    申请号:US722454

    申请日:1996-09-27

    摘要: A method and apparatus for conveying material hanging on hangers. The material is transported from a loading region to a conveyance region, and then to a delivery region. Grip units of various lengths are formed by combining individual materials into groups. A theoretical maximum length for a grip unit is established. Clock pulses are produced in the conveyance region and are counted. Grip units stowed in the loading region are individualized to form well-defined spaces between the materials. Individualized grip units fed to the conveyance region are switched into the conveyance region when a gap sufficiently large to accommodate the grip unit is present in the conveyance region, determined by the maximum length established and counting of the clock pulses. The distance to be moved by the grip unit in the conveyance region to reach its destination is established, and progress of the grip unit is tracked. The grip unit is switched out to the delivery region, the switch-out mechanism remaining in effect to accommodate the length of the grip unit.

    摘要翻译: 一种用于输送挂在衣架上的材料的方法和装置。 材料从装载区域运送到输送区域,然后运送到输送区域。 通过将各种材料组合成组合形成各种长度的夹持单元。 建立了握持单元的理论最大长度。 在输送区域产生时钟脉冲,并进行计数。 存放在装载区域中的夹持单元被个体化以在材料之间形成明确定义的空间。 当由建立的最大长度和时钟脉冲的计数确定的输送区域中存在供给到输送区域的个体化夹持单元,当在足够大的位置以容纳夹持单元的间隙存在输送区域时。 建立由把手单元在输送区域中移动以到达其目的地的距离,并且跟踪握持单元的进度。 把手单元被切换到输送区域,切换机构保持有效地适应把手单元的长度。

    Apparatus for adjusting aircraft wing flaps
    2.
    发明授权
    Apparatus for adjusting aircraft wing flaps 失效
    用于调整飞机机翼的装置

    公开(公告)号:US5566910A

    公开(公告)日:1996-10-22

    申请号:US322055

    申请日:1994-10-12

    IPC分类号: B64C9/16 B64C13/28

    CPC分类号: B64C9/16 B64C13/28

    摘要: A wing gap closure flap is positioned in an aircraft wing so that a gap between the wing structure and the leading edge of a landing flap can be closed during normal cruising positions of the landing flap and opened when the landing flap is in a starting position or in a landing position. The gap is formed on the underside of the aircraft wing and the gap closure flap is operated by a positioning shaft which itself is driven through a drive lever linkage by the drive shaft for the landing flap. The wing gap closure flap is connected through a lever mechanism to the positioning shaft which is preferably divided into shaft sections where a plurality of wing gap closure flaps are used. Each shaft section is driven by the landing flap drive shaft. A defined motion of the wing gap closure flap or flaps is achieved in that the positioning of the wing gap closure flaps is synchronized in a limited angular range with the positioning of the landing flap by the cooperation of the respective drive mechanisms.

    摘要翻译: 机翼间隙关闭翼片定位在飞机机翼中,使得在着陆翼的正常巡航位置期间,机翼结构和着陆翼的前缘之间的间隙可以关闭,并且当着陆翼处于起始位置时打开, 在着陆位置。 间隙形成在飞行器机翼的下侧,并且间隙闭合翼片由定位轴操作,定位轴本身通过用于着陆挡板的驱动轴通过驱动杆连杆驱动。 机翼间隙闭合翼片通过杠杆机构连接到定位轴,定位轴优选地分成轴部分,其中使用多个机翼间隙闭合翼片。 每个轴段由着陆挡板驱动轴驱动。 实现翼间隙闭合翼片或翼片的限定运动的目的在于,通过各个驱动机构的配合,机翼间隙闭合翼片的定位在有限角度范围内与着陆翼片的定位同步。