利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

9 条记录 (耗时 0.045 秒)

    Nested automatically separable flying disk assembly
    8.
    发明授权
    Nested automatically separable flying disk assembly 失效
    嵌套自动可分离飞盘组件

    公开(公告)号：US5480334A

    公开(公告)日：1996-01-02

    申请号：US231165

    申请日：1994-04-22

    申请人： James M. Wilson ,  Dean M. Wilson

    发明人： James M. Wilson ,  Dean M. Wilson

    IPC分类号： A63H33/18 ,  A63H27/00

    CPC分类号： A63H33/18

    摘要： The nested automatically separable flying disk assembly includes an outer or cover disk assembly enclosing a nested or inner disk assembly. The outer or cover disk assembly is of a generally cylinderical disk shape having an air space between itself and the nested or inner disk assembly provided by a central nub projection cooperating with flange nub projections. The nested or inner disk assembly is provided with an outer peripheral flange section extended downwardly and below a similar peripheral rim section on the outer or cover disk assembly for allowing air to flow therebetween to cause the desired separation between the nested disk assemblies. An adjustable central nub projection is provided to adjustably change separation between the outer or cover disk assembly and the nested or inner disk assembly. The nested or inner disk assembly is provided with a plurality of inclined concentric aerodynamic ridges to alter air flow and resultant turbulence of air flow between the nested disk assemblies to vary the aerodynamic flight characteristics thereof. Second and third embodiments provide different angular relationships, either inwardly or outwardly, of the outer adjacent peripheral rim section of the outer or cover disk assembly and the peripheral flange section of the nested or inner disk assembly to achieve an increase or decrease in the time of separation of the outer or cover disk assembly from the nested or inner disk assembly.

    摘要翻译： 嵌套的可自动分离的飞盘组件包括封闭嵌套或内部盘组件的外部或盖板组件。 外盘或盖盘组件具有大致圆柱形盘形，在其与由与凸缘凸起突起配合的中心凸起突起提供的嵌套或内盘组件之间具有空气空间。 嵌套或内盘组件设置有外周凸缘部分，该外周边凸缘部分在外盘盖组件或盖盘组件上向下延伸并位于类似的周边边缘部分下面，以允许空气在其间流动，从而在嵌套盘组件之间产生期望的间隔。 提供可调节的中央凸起凸起以可调节地改变外部或盖盘组件与嵌套或内部盘组件之间的间隔。 嵌套或内盘组件设置有多个倾斜的同心空气动力学脊，以改变空中流动，并导致嵌套圆盘组件之间的空气流动的湍流，以改变其空气动力学飞行特性。 第二和第三实施例提供外部或覆盖盘组件的外部相邻外围边缘部分的内向或向外的不同的角度关系，以及嵌套或内部盘组件的周边凸缘部分以实现时间的增加或减少 外部或盖盘组件与嵌套或内部盘组件的分离。