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    Display apparatus
    275.
    发明授权
    Display apparatus 有权
    显示装置

    公开(公告)号：US09414514B2

    公开(公告)日：2016-08-09

    申请号：US14347615

    申请日：2011-09-30

    Applicant: Kenji Yoshida

    Inventor： Kenji Yoshida

    IPC: H05K7/14 ,  G02F1/1333 ,  G02F1/1362

    CPC classification number: H05K7/14 ,  G02F1/133308 ,  G02F2001/13332 ,  G02F2001/136254 ,  G02F2201/58 ,  G09G2360/141 ,  G09G2360/145

    Abstract: A display apparatus includes: a display panel which has a display surface; an apparatus base to which the display panel is attached; a detecting unit which has a detecting surface disposed so as to face a region to be inspected being a part of the display surface, the detecting unit detecting by means of the detecting surface, light emitted from the region to be inspected, and outputting a detection result; and a case which supports the detecting unit, and is attached to a peripheral area of the region to be inspected.

    Abstract translation: 一种显示装置，包括：具有显示面的显示面板; 安装显示面板的装置基座; 检测单元，其具有被设置为面对被检查区域的检测表面是显示表面的一部分，检测单元通过检测表面检测从被检查区域发射的光，并输出检测 结果; 以及支撑检测单元并且附接到待检查区域的周边区域的壳体。

    Method for designing a natural laminar flow wing of a supersonic aircraft
    277.
    发明授权
    Method for designing a natural laminar flow wing of a supersonic aircraft 有权
    设计超音速飞机天然层流翼的方法

    公开(公告)号：US09031817B2

    公开(公告)日：2015-05-12

    申请号：US13325742

    申请日：2011-12-14

    Applicant: Kenji Yoshida ,  Kisa Matsushima ,  Yoshine Ueda ,  Hiroaki Ishikawa

    Inventor： Kenji Yoshida ,  Kisa Matsushima ,  Yoshine Ueda ,  Hiroaki Ishikawa

    IPC: G06F17/50 ,  B64C3/14 ,  B64F5/00 ,  B64C30/00

    CPC classification number: B64C3/14 ,  B64C30/00 ,  B64C2003/149 ,  B64F5/00 ,  G06F17/5095 ,  Y02T50/12

    Abstract: In designing supersonic aircrafts, a method of designing a natural laminar flow wing is provided which reduces friction drag by delaying boundary layer transition under flight conditions of actual aircrafts. A target Cp distribution on wing upper surface, suited to natural laminarization in which boundary layer transition is delayed rearward in desired Reynolds number states, is defined by a functional type having as coefficients parameters depending on each spanwise station, a sensitivity analysis employing a transition analysis method is applied to the parameters, and a search is performed for the optimum combination of parameters to delay transition rearward.

    Abstract translation: 在设计超音速飞机时，提供了一种设计自然层流翼的方法，通过延迟实际飞机飞行条件下的边界层过渡来减少摩擦阻力。 翼型上表面上的目标Cp分布适用于边界层转变在所需雷诺数状态下向后延伸的自然层流，由具有取决于每个翼展方向站的系数参数的函数类型定义，使用转换分析的灵敏度分析 方法应用于参数，并且对于参数的最佳组合执行搜索以向后延迟转换。

    Stream dot pattern, method of forming stream dot pattern, information input/output method using stream dot pattern, and dot pattern
    278.
    发明授权
    Stream dot pattern, method of forming stream dot pattern, information input/output method using stream dot pattern, and dot pattern 有权
    流点图案，形成流点图案的方法，使用流点图案的信息输入/输出方法和点图案

    公开(公告)号：US09010640B2

    公开(公告)日：2015-04-21

    申请号：US13384134

    申请日：2010-07-13

    Applicant: Kenji Yoshida

    Inventor： Kenji Yoshida

    IPC: G06K19/00 ,  G06K19/06 ,  H04N1/405 ,  G06K1/12 ,  G06F3/03

    CPC classification number: G06F3/0317 ,  G06F3/0321 ,  G06K1/121 ,  G06K7/143 ,  G06K19/06037 ,  H04N1/4051

    Abstract: A stream dot technique forming a dot pattern at an arbitrary position on a curved surface body or a medium surface by including the step of linearly and consecutively arranging a plurality of reference dots according to a predetermined rule, providing a first virtual reference line which connects the plurality of reference dots, providing a second virtual reference line which is defined at a predetermined position from the reference dot and/or the first virtual reference line, providing a plurality of virtual reference points at predetermined positions on the second virtual reference line, and placing an information dot whose information is defined by a distance and a direction from the virtual reference point at an end point expressed by a vector with the virtual reference point being a start point.

    Abstract translation: 通过包括根据预定规则线性连续地排列多个参考点的步骤，在曲面体或介质表面上的任意位置形成点图形的流点技术，提供将第 提供多个参考点，提供从参考点和/或第一虚拟参考线在预定位置定义的第二虚拟参考线，在第二虚拟参考线上的预定位置处提供多个虚拟参考点，以及放置 一个信息点，其信息由距虚拟参考点和虚拟参考点为起始点的向量表示的终点处的方向定义。

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