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    • 4. 发明授权
    • Radio base station and cell-identifier specifying method
    • 无线基站和小区标识符指定方法
    • US08085747B2
    • 2011-12-27
    • US12960595
    • 2010-12-06
    • Koji Ogawa
    • Koji Ogawa
    • H04Q7/24
    • H04W8/26H04W64/003
    • A radio base station includes a first obtaining device to obtain position information for locating a position of a local station; a second obtaining device to obtain a matrix that includes blocks, each block representing an area with which a uniquely identifiable cell identifier is associated, and that covers a cell coverage of the local station and a cell coverage in which use of the same cell identifiers as those of the local station is to be avoided; and a specifying device to specify the cell identifiers associated with the blocks included in the cell coverage of the local station, on a basis of the local station position located by the position information and the matrix.
    • 无线基站包括获取用于定位本地站位置的位置信息的第一获取装置; 用于获得包括块的矩阵的第二获取装置,每个块表示与唯一可识别的小区标识符相关联的区域,并且覆盖本地站的小区覆盖和小区覆盖,其中使用相同小区标识符作为 要避免当地的电台; 以及指定装置,其基于由位置信息和矩阵定位的本地站位置来指定与包括在本地站的小区覆盖中的块相关联的小区标识符。
    • 6. 发明申请
    • LOAD APPARATUS
    • 装载装置
    • US20080242970A1
    • 2008-10-02
    • US12059246
    • 2008-03-31
    • Eiichi MinagawaRyoichi SakaiKoji Ogawa
    • Eiichi MinagawaRyoichi SakaiKoji Ogawa
    • A61B5/05A61B5/103
    • A61B5/4504A61B8/0875A61B8/485G01N3/32G01N2203/0016
    • An oscillation arm moves in a seesaw fashion about an oscillation axis which is supported by a support rod and which serves as a fulcrum. A rotation arm and a pressurizer are provided on one end of the oscillation arm. One end of the rotation arm is rotatably attached to the oscillation arm, and a load weight is placed on the other end of the rotation arm. By rotating the rotation arm, the magnitude of a force to be applied by the load weight to the pressurizer is adjusted. More specifically, by displacing the load weight to a predetermined position by rotation and then causing the load weight to stop at this position, a static load corresponding to the rotation angle can be applied to the pressurizer. Further, by causing the load weight to perform rotational motion, the magnitude of the force to be applied to the pressurizer is periodically varied, so that a load which varies periodically can be applied to hard tissue.
    • 振荡臂围绕由支撑杆支撑并作为支点的摆动轴线以跷跷板方式移动。 旋转臂和加压器设置在摆动臂的一端。 旋转臂的一端可旋转地安装在摆动臂上,并且负载重量被放置在旋转臂的另一端上。 通过旋转旋转臂,调整由负载重量施加到加压器的力的大小。 更具体地,通过旋转将负载重量移动到预定位置,然后使负载重量在该位置停止,可以对加压器施加与旋转角度相对应的静态负载。 此外,通过使负载重量进行旋转运动,施加到加压器的力的大小周期性地变化,使得周期性变化的负载可以施加到硬组织。
    • 7. 发明授权
    • Immersion-type temperature measuring apparatus using thermocouple
    • 使用热电偶的浸入式温度测量装置
    • US5360269A
    • 1994-11-01
    • US151532
    • 1993-11-12
    • Koji OgawaHiroshi Suzuki
    • Koji OgawaHiroshi Suzuki
    • G01K1/10G01K1/12
    • G01K1/105
    • An immersion-type temperature measuring apparatus using a thermocouple for measuring temperature of a melt, which comprises: a replaceable cartridge-type temperature sensor (11) for detecting a thermoelectromotive force corresponding to a temperature of a melt, the temperature sensor (11) comprising a thermocouple (13), a protecting tube (12) for protecting the thermocouple (13) from the melt, and a connector (16); a holder for releasably supporting the temperature sensor (11); a measuring instrument (28) for processing the thermoelectromotive force to determine the temperature of the melt; and an extension lead wire (25) for connecting the temperature sensor (11) with the measuring instrument (28). At least part of the above-mentioned protecting tube (12) is formed of a molybdenum-zirconia refractory consisting essentially of from 20 to 95 wt. % molybdenum and from 5 to 80 wt. % zirconia.
    • 一种使用用于测量熔体温度的热电偶的浸入型温度测量装置,包括:用于检测与熔体温度相对应的热电动势的可替换的盒式温度传感器,所述温度传感器包括: 热电偶(13),用于保护热电偶(13)免受熔体的保护管(12)和连接器(16); 用于可释放地支撑温度传感器(11)的保持器; 用于处理热电动势以测定熔体温度的测量仪器(28); 以及用于将温度传感器(11)与测量仪器(28)连接的延长引线(25)。 上述保护管(12)的至少一部分由基本上由20〜95重量%组成的钼 - 氧化锆耐火材料形成。 %钼和5〜80wt。 %氧化锆。
    • 8. 发明授权
    • Active control mechanism for a helicopter
    • 直升机的主动控制机制
    • US4958786A
    • 1990-09-25
    • US423695
    • 1989-10-18
    • Koji OgawaHikoichi Machida
    • Koji OgawaHikoichi Machida
    • B64C27/72G05D1/08
    • G05D1/0858B64C27/72Y02T50/34
    • The rotor damping and control power value can be made arbitrary by controlling a cyclic pitch control mechanism with a signal proportional to the angular acceleration of the attitude angle .theta., a signal proportional to the angular velocity of the attitude angle .theta., and a correction signal based upon the difference between the attitude angle .theta. and assumed attitude angle .theta..sub.0, plus the cyclic pitch control input .PSI. applied to a cyclic pitch lever of a pilot. Thus, the rotor damping and control power are brought to their optimum values in response to the actual flight conditions of a helicopter for ideal operability, resulting in both high stability and operability, and, for example, fully automatically controlled hovering can be accomplished without producing any vibration in the attitude angle control response.
    • 可以通过控制具有与姿态角θ的角加速度成比例的信号(与姿态角θ的角速度成比例的信号)和基于校正信号的校正信号来控制循环俯仰控制机构来使转子阻尼和控制功率值任意 在姿态角度θ和假设姿态角度θ0之间的差异加上施加到飞行员的循环俯仰杆上的循环俯仰控制输入PSI。 因此,为了理想的可操作性,转子阻尼和控制功率响应于直升机的实际飞行条件而达到其最佳值,导致高稳定性和可操作性,并且例如可以完全自动控制悬停,而不产生 任何振动的姿态角控制响应。