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    • 2. 发明申请
    • SULFURIC ACID ELECTROLYSIS METHOD AND SULFURIC ACID ELECTROLYSIS APPARATUS
    • 硫酸电解法和硫酸电解设备
    • US20130319875A1
    • 2013-12-05
    • US14000239
    • 2012-02-23
    • MINORU UCHIDA
    • MINORU UCHIDA
    • C25B1/28C25B15/02C25B11/12
    • C25B1/285C25B9/06C25B11/12C25B15/02H01L21/31133
    • An electrolysis apparatus comprising: an electrolytic cell in which a sulfuric acid solution is fed and discharged; a conductive anode and cathode electrode of diamond composition; a feeding unit for feeding the sulfuric acid solution to the electrolytic cell; a power supply unit for applying a voltage between the anode and cathode electrodes; and a power control unit for controlling the power supply unit such that a forward voltage is applied between the anode and cathode during normal electrolysis with the polarity applied between the anode and cathode inverted under predetermined conditions during intervals between normal operation to dissolve precipitates of sulfur generated in the electrolytic cell for stabilizing the electrolysis operation.
    • 一种电解装置,包括:电解槽,其中硫酸溶液进料和排出; 金刚石组合物的导电阳极和阴极电极; 用于将硫酸溶液供给到电解槽的进料单元; 用于在阳极和阴极之间施加电压的电源单元; 以及功率控制单元,用于控制电源单元,使得在正常电解期间,在正常操作之间的间隔期间在正常操作之间的间隔期间以正反应的阳极和阴极之间的极性施加正向电压,以在阳极和阴极之间施加正向电压以溶解产生的硫的沉淀物 在用于稳定电解操作的电解池中。
    • 3. 发明授权
    • Aircraft control surface operating device
    • 飞机控制面操作装置
    • US08596582B2
    • 2013-12-03
    • US13275676
    • 2011-10-18
    • Minoru UchidaHiroshi Yamanouchi
    • Minoru UchidaHiroshi Yamanouchi
    • B64C9/00
    • B64C9/02Y02T50/32
    • An aircraft control surface operating device is provided for operating a control surface on an aircraft body portion to move between a retracted position and an extended position. The aircraft control surface operating device includes a control surface mounting assembly which movably secures the control surface to the aircraft body portion, a drive arm rotatable about a drive axis relative to the aircraft body portion, an actuator for rotating the drive, and a drive link connecting the drive arm to the control surface mounting assembly. The drive link has a control end connected to the control surface mounting assembly and a driven end connected to the drive arm via a drive bearing joint. The drive link connects the drive arm and the control surface mounting assembly such that rotation of the drive arm is causes extending or retracting movement of the control surface.
    • 飞行器控制表面操作装置被提供用于操作飞机主体部分上的控制表面以在缩回位置和延伸位置之间移动。 飞行器控制表面操作装置包括控制表面安装组件,该控制表面安装组件将控制表面可移动地固定到飞行器主体部分,相对于飞行器主体部分可围绕驱动轴线旋转的驱动臂,用于旋转驱动器的致动器和驱动连杆 将驱动臂连接到控制表面安装组件。 驱动链路具有连接到控制表面安装组件的控制端和经由驱动轴承接头连接到驱动臂的从动端。 驱动链路连接驱动臂和控制表面安装组件,使得驱动臂的旋转引起控制表面的延伸或缩回运动。
    • 4. 发明授权
    • Radio communication system
    • 无线通信系统
    • US07724695B2
    • 2010-05-25
    • US11521407
    • 2006-09-15
    • Minoru Uchida
    • Minoru Uchida
    • H04B7/00H04W36/00
    • H04W72/042H04W16/10H04W76/10
    • A radio communication system includes a line controller, a plurality of base stations connected to the line controller and a plurality of mobile stations connected to each of the plurality of base stations by radio communication line having control channel and communication channel, and each of the plurality of base stations includes a control unit for monitoring idle slot in the communication channel within a communication area of the base station. The control unit transmits the monitored information of the idle slot to the mobile station within the communication area of the base station at predetermined intervals by using the control channel and each mobile station can use an idle slot in the base station or, if there is no idle slot in the base station, in another base station based on the monitored information of the idle slot to make communication.
    • 无线电通信系统包括线路控制器,连接到线路控制器的多个基站和通过具有控制信道和通信信道的无线电通信线路连接到多个基站中的每一个的多个移动台,并且多个 的基站包括用于监视基站的通信区域内的通信信道中的空闲时隙的控制单元。 控制单元通过使用控制信道以预定的间隔将所监视的空闲时隙的信息发送到基站的通信区域内的移动站,并且每个移动站可以使用基站中的空闲时隙,或者如果没有 基站中的空闲时隙,在另一基站中基于所监视的空闲时隙信息进行通信。
    • 5. 发明申请
    • Radio communication system
    • 无线通信系统
    • US20070087750A1
    • 2007-04-19
    • US11521407
    • 2006-09-15
    • Minoru Uchida
    • Minoru Uchida
    • H04Q7/20
    • H04W72/042H04W16/10H04W76/10
    • A radio communication system includes a line controller, a plurality of base stations connected to the line controller and a plurality of mobile stations connected to each of the plurality of base stations by radio communication line having control channel and communication channel, and each of the plurality of base stations includes a control unit for monitoring idle slot in the communication channel within a communication area of the base station. The control unit transmits the monitored information of the idle slot to the mobile station within the communication area of the base station at predetermined intervals by using the control channel and each mobile station can use an idle slot in the base station or, if there is no idle slot in the base station, in another base station based on the monitored information of the idle slot to make communication.
    • 无线电通信系统包括线路控制器,连接到线路控制器的多个基站和通过具有控制信道和通信信道的无线电通信线路连接到多个基站中的每一个的多个移动台,并且多个 的基站包括用于监视基站的通信区域内的通信信道中的空闲时隙的控制单元。 控制单元通过使用控制信道以预定的间隔将所监视的空闲时隙的信息发送到基站的通信区域内的移动站,并且每个移动站可以使用基站中的空闲时隙,或者如果没有 基站中的空闲时隙,在另一基站中基于所监视的空闲时隙信息进行通信。
    • 7. 发明授权
    • Flap operating device
    • 翻转操作装置
    • US06464176B2
    • 2002-10-15
    • US09911372
    • 2001-07-25
    • Minoru UchidaHiroshi YamanouchiWataru YadaHidetaka Nagano
    • Minoru UchidaHiroshi YamanouchiWataru YadaHidetaka Nagano
    • B64C911
    • B64C13/30B64C3/50B64C9/16B64C9/20Y02T50/44
    • A flap mounted on a tapered main wing of an aircraft, is supported by at least two link units. The link units are formed into analogous shapes with an analogous size ratio equal to the ratio between corresponding chord lengths of the main wing. As a result, the amounts of protrusion of the flap are varied in the span direction in accordance with the analogous size ratio, and the flap performs a three-dimensional motion such that it is moved in the span direction while being retracted and lowered. Thus, the flap can be moved to protrude to an optimal position and through an optimal angle according to the chord lengths of the main wing. When the flap is a slotted flap, an appropriate slot width can be ensured at each of the portions in the span direction, whereby the aerodynamic characteristic of the flap mounted on the tapered main wing can be uniform in the span direction.
    • 安装在飞机的锥形主翼上的翼片由至少两个连杆单元支撑。 链节单元形成类似的形状,类似的尺寸比等于主翼翼的相应弦长之比。 结果,翼片的突出量根据类似的尺寸比在跨度方向上变化,并且翼片执行三维运动,使得其在缩回和降低的同时在跨度方向上移动。 因此,翼片可以根据主翼翼的弦长而移动到突出到最佳位置并且通过最佳角度。 当翼片是开槽翼片时,可以在跨越方向的每个部分处确保适当的槽宽度,由此安装在锥形主翼上的翼片的空气动力学特性在跨度方向上可以是均匀的。