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Shock-attenuating seamless surface system for use on vertical takeoff and landing zones

机译:减震无缝表面系统,用于垂直起降区

摘要

Shock-attenuating seamless surface systems, for use on vertical takeoff and landing zones, can be installed on a base or installed in a recess in the base such that an integrated installation is obtained. PPAll systems have a surface layer with a bottom and outer edges; ribs extending from the bottom of the surface layer for defining an array of air-filled cells affixed to the bottom of the surface layer; and a first layer of sealer and aggregate spread over the surface layer, the outer edges, and the base immediate to surface system.P PMore complex systems may include one or more of the following: a plurality of median ribs extending a shorter distance from the bottom of the surface layer than the defining ribs in order to give added support against a strong blow striking the surface layer and the array of air- filled cells affixed thereto; a void area left in place of at least one median rib in order to facilitate cutting through the surface layer; a second layer of sealer spread under the array of air- filled cells and above the base in order to prevent the escape of air therefrom upon impact thereto and also for holding the array of air- filled cells in a substantially vertical orientation with respect to the base; a sloping outer edge surrounding all sides to help prevent tripping and facilitate access by handicapped person; and a beveled outer edge surrounding all sides for facilitating attachment to the base.
机译:可以在垂直起飞和着陆区使用的减震无缝表面系统可以安装在基座上,也可以安装在基座的凹槽中,从而获得集成安装。

所有系统都具有表面层具有底部和外部边缘;从表面层的底部延伸的肋,用于限定固定在表面层的底部的空气填充单元的阵列;较复杂的系统可能包括以下一个或多个:多个中间肋延伸距表面层底部的距离比限定肋的距离短,以便为打击表面层和固定在其上的充气单元阵列的强力打击提供额外的支撑;留有至少一个中间肋骨的空隙区域,以便于切穿表面层;第二层密封剂分布在充气单元阵列的下方和基座上方,以防止空气从其撞击时逸出,并且还用于将充气单元阵列相对于容器保持在基本垂直的方向上。基础;围绕所有侧面的倾斜外边缘,有助于防止绊倒并方便残障人士进入;以及围绕所有侧面的倾斜外边缘,以便于固定到基座。

著录项

  • 公开/公告号US5013029A

    专利类型

  • 公开/公告日1991-05-07

    原文格式PDF

  • 申请/专利权人 VAUX;THOMAS M.;

    申请/专利号US19890377415

  • 发明设计人 THOMAS M. VAUX;

    申请日1989-07-10

  • 分类号A63G71/02;

  • 国家 US

  • 入库时间 2022-08-22 05:46:33

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