Fixing apparatus
    11.
    发明授权
    Fixing apparatus 失效
    固定装置

    公开(公告)号:US4192229A

    公开(公告)日:1980-03-11

    申请号:US946756

    申请日:1978-09-28

    IPC分类号: G03G15/20 B30B3/04

    CPC分类号: G03G15/2092 G03G2215/2064

    摘要: Apparatus for fixing toner image on a toner image supporting member in electrophotographic copying machine is disclosed. The fixing apparatus includes three rotary rollers which are in contact with each other under the action of pressing means. One of the three rollers has a smaller diameter than the other two rollers. Two rollers with which the toner image supporting member comes into contact are disposed in such a manner that the axes of the two rollers intersect each other and the portion at which the two rollers contact each other or are closest to each other forms a straight line relative to the direction of roller axis. According to one embodiment of the invention, the remaining one roller with which the supporting member does not contact, is formed as a crown roller, that is, a roller which has its largest diameter at the middle portion of the roller.

    摘要翻译: 公开了一种用于将调色剂图像定影在电子照相复印机中的调色剂图像支持部件上的装置。 定影装置包括在压制装置的作用下彼此接触的三个旋转辊。 三个辊中的一个具有比其他两个辊更小的直径。 调色剂图像支撑部件接触的两个辊以这样的方式设置,使得两个辊的轴彼此相交,并且两个辊彼此接触或彼此最接近的部分形成直线相对 到辊轴方向。 根据本发明的一个实施例,支撑构件不与其接触的剩余的一个辊形成为冠辊,即在辊的中间部分具有最大直径的辊。

    Information processing device and disk drive device
    12.
    发明授权
    Information processing device and disk drive device 失效
    信息处理装置和磁盘驱动装置

    公开(公告)号:US08000097B2

    公开(公告)日:2011-08-16

    申请号:US12082174

    申请日:2008-04-09

    IPC分类号: G06F1/16

    摘要: An information processing device is provided. The device includes an upper enclosure; a lower enclosure which supports the upper enclosure with a varied attitude and on which the upper enclosure may be superposed; a disk drive device stored in the upper or lower enclosure and having a disk mounting part on which a disk-shaped recording medium is detachably mounted; and an enclosure moving mechanism setting a disk storage region to have a first thickness with the upper enclosure allowed to have a distance from the lower enclosure when the disk drive device is used and setting the disk storage region to have a second thickness smaller than the first thickness with the upper enclosure allowed to come close to the lower enclosure to reduce the disk storage region when the disk drive device is not used.

    摘要翻译: 提供信息处理装置。 该装置包括上部外壳; 下部外壳,其以不同的姿态支撑上部外壳,并且上部外壳可以叠置在该外壳上; 存储在上壳体或下壳体中并且具有盘安装部分的盘驱动装置,盘形记录介质可拆卸地安装在盘安装部分上; 以及机壳移动机构,当使用所述磁盘驱动装置时,将所述磁盘存储区域设置为具有第一厚度,使所述上壳体允许与所述下壳体距离一定距离,并且将所述磁盘存储区域设置为具有小于所述第一厚度的第二厚度 当不使用磁盘驱动器装置时,上壳体的厚度允许靠近下壳体以减小磁盘存储区域。

    INPUT APPARATUS, CONTROL APPARATUS, CONTROL SYSTEM, CONTROL METHOD, AND HANDHELD APPARATUS
    13.
    发明申请
    INPUT APPARATUS, CONTROL APPARATUS, CONTROL SYSTEM, CONTROL METHOD, AND HANDHELD APPARATUS 失效
    输入装置,控制装置,控制系统,控制方法和手持装置

    公开(公告)号:US20100103096A1

    公开(公告)日:2010-04-29

    申请号:US12522137

    申请日:2008-07-04

    IPC分类号: G06F3/033

    CPC分类号: G06F3/0383 G06F3/0346

    摘要: An input apparatus, a control apparatus, a control system, and a control method therefor, that are capable of solving a problem on gravity that affects an acceleration sensor of an input apparatus when tilted from its original position, and reducing a calculation amount are provided. An MPU of an input apparatus corrects angular velocity values by rotational coordinate conversion corresponding to a calculated roll angle to obtain correction angular velocity values (second and first correction angular velocity values) as correction values. Accordingly, even when a user moves the input apparatus in a state where the input apparatus is tilted with respect to an axis in a gravity direction (vertical axis) about a Z axis, effects of gravity acceleration components in X′- and Y′-axis directions that are generated by the tilt can be removed.

    摘要翻译: 一种输入装置,控制装置,控制系统及其控制方法,其能够解决当从原始位置倾斜时影响输入装置的加速度传感器的重力问题,并且减少计算量 。 输入装置的MPU通过对应于计算出的滚动角度的旋转坐标转换来校正角速度值,以获得校正角速度值(第二和第一校正角速度值)作为校正值。 因此,即使用户在输入装置相对于Z轴的重力方向(纵轴)上的轴线倾斜的状态下移动输入装置,也能够将X'和Y'- 可以去除由倾斜产生的轴方向。

    Connection controller, IP telephone communication system, connection control method and program
    14.
    发明申请
    Connection controller, IP telephone communication system, connection control method and program 审中-公开
    连接控制器,IP电话通信系统,连接控制方法和程序

    公开(公告)号:US20070286177A1

    公开(公告)日:2007-12-13

    申请号:US11727737

    申请日:2007-03-28

    IPC分类号: H04L12/66

    CPC分类号: H04W28/16 H04W76/25 H04W80/04

    摘要: In an IP telephone communication system at least including a plurality of Access Points and stations under control of the Access Points, each of the Access Points determines presence or absence of a station in a silent state not conducting IP telephone communication among stations having established communication lines for IP telephone communication and conducts, when presence of the station in a silent state is determined, pseudo IP telephone communication corresponding to a state in which the station in a silent state conducts IP telephone communication. According to the system, even if there exists a station in the silent state not conducting IP telephone communication, it is possible to determine connectibility of IP telephone communication with high reliability.

    摘要翻译: 在至少包括接入点控制下的多个接入点和站的IP电话通信系统中,每个接入点确定无声状态的站的存在或不存在,在没有建立通信线路的站之间进行IP电话通信 对于IP电话通信,并且当确定处于静音状态的站的存在时,执行与静默状态的站进行IP电话通信的状态相对应的伪IP电话通信。 根据该系统,即使存在不进行IP电话通信的无声状态的站,也可以确定IP电话通信的可靠性高可靠性。

    Apparatus for determining attitude of artificial satellite
    15.
    发明授权
    Apparatus for determining attitude of artificial satellite 失效
    用于确定人造卫星姿态的装置

    公开(公告)号:US06523786B2

    公开(公告)日:2003-02-25

    申请号:US09879918

    申请日:2001-06-14

    IPC分类号: B64G136

    CPC分类号: B64G1/361 B64G2001/245

    摘要: An apparatus for determining the attitude of an artificial satellite by narrowing attitude candidates to a correct one in a short time. The apparatus has star sensors, a star catalog data base, star identification sections in each of which star images output from the star sensors are collated with a star catalog with respect to each star sensor to output a group of corresponding candidates, attitude computation sections for computing a value of an attitude candidate of the artificial satellite with respect to each corresponding candidate, an attitude updating section for updating the value of the attitude candidate on the basis of the star images output from the star sensor and the star catalog, and an attitude propagation section for computing the value of the attitude candidate at the present sampling time from the value of the attitude candidate at the preceding sampling time and the artificial satellite's angular velocity. An attitude candidate unification section for comparing and combining the values of attitude candidates into one candidate is provided in a loop including the attitude updating section and the attitude propagation section.

    摘要翻译: 一种用于通过在短时间内将姿态候选缩小到正确的姿态来确定人造卫星的姿态的装置。 该装置具有星形传感器,星型目录数据库,星型识别部分,其中从星形传感器输出的星形图像与星形传感器相关的星形目录进行整理,以输出一组相应的候选者,姿态计算部分用于 计算人造卫星相对于每个相应候选人的姿态候选的值,姿态更新部分,用于基于从星形传感器和星形目录输出的星形图像来更新姿态候选者的值,以及姿态 传播部分,用于根据前一采样时间的姿态候选值和人造卫星的角速度计算当前采样时间的姿态候选值。 在姿态更新部和姿态传播部的回路中设置用于将姿态候选的值进行比较和组合成一个候选的姿态候补统一部。

    Artificial satellite navigation system and method
    17.
    发明授权
    Artificial satellite navigation system and method 失效
    人造卫星导航系统及方法

    公开(公告)号:US06166684A

    公开(公告)日:2000-12-26

    申请号:US268129

    申请日:1999-03-15

    摘要: An artificial satellite navigation system and method. The artificial satellite navigation system includes a global positioning system (GPS) receiver, local satellite, and remote satellite absolute navigation units estimating the position and velocity of a local satellite or a remote satellite and bias and drift of a clock in the receiver. A difference calculation unit calculates differences in position and velocity from the local satellite and remote satellite absolute navigation units. A relative navigation unit estimates the relative position and velocity of the local satellite with respect to the remote satellite. The relative navigation unit navigates the local satellite relative to the remote satellite.

    摘要翻译: 人造卫星导航系统及方法。 人造卫星导航系统包括估计本地卫星或远程卫星的位置和速度的全球定位系统(GPS)接收机,本地卫星和远程卫星绝对导航单元以及接收机中时钟的偏置和漂移。 差分计算单元从本地卫星和远程卫星绝对导航单元计算位置和速度的差异。 相对导航单元估计本地卫星相对于远程卫星的相对位置和速度。 相对导航单元相对于远程卫星导航本地卫星。

    Attitude determination system for artificial satellite
    19.
    发明授权
    Attitude determination system for artificial satellite 失效
    人造卫星姿态确定系统

    公开(公告)号:US6102338A

    公开(公告)日:2000-08-15

    申请号:US919193

    申请日:1997-08-28

    摘要: An attitude determination system for an artificial satellite capable of performing star identification without need for the aid of ground station includes an image processing module (17) for processing star images observed at predetermined time points by a star sensor (16) mounted on the artificial satellite (1) for arithmetically determining direction vectors of the observed stars, a rotation estimating module (18) for estimating a rotational motion of the artificial satellite (1) between an attitude of the artificial satellite at a predetermined time point and an attitude of the artificial satellite at another time point, an elongation estimating module (19) for estimating elongations between the direction vectors of plural stars the images of which are picked up at a same time point by the star sensor and estimating the elongations between the direction vectors of plural stars the images of which are picked up at different time points by the star sensor on the basis of the estimated rotational motion, a star identifying module (20) for establishing correspondences between a plurality of the stars for which relation of the elongation has been determined and stars on a star catalog for identifying the stars, and an attitude angle estimating module (21) for estimating an attitude angle of the artificial satellite on the basis of result of identification of the stars.

    摘要翻译: 能够在不需要地面站的帮助下进行星型识别的人造卫星的姿势确定系统包括:图像处理模块(17),用于处理在预定时间点由安装在人造卫星上的星形传感器(16)观察到的星形图像 (1),用于对所述观测星的方向矢量进行算术确定;旋转估计模块,用于估计所述人造卫星在预定时间点的姿态与人造卫星的姿态之间的旋转运动; 卫星在另一个时间点,延伸率估计模块(19),用于估计多个恒星的方向向量之间的延伸,其中图像由星形传感器在同一时间点被拾取并且估计多个恒星的方向向量之间的伸长 其基于估计的星形传感器在不同时间点拾取图像 旋转运动的星形识别模块(20),用于在已经确定了伸长关系的多个星星之间建立对应关系,并且用于识别恒星的星形目录上的恒星;以及姿态角估计模块(21),用于估计 人造卫星的姿态角基于星星识别的结果。