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    • 44. 发明授权
    • Connector mating structure
    • 连接器配套结构
    • US06193530B1
    • 2001-02-27
    • US09293988
    • 1999-04-19
    • Kazuaki SakuraiYoshinori UchidaHirofumi YamauchiYoko NakamuraAtsushi SasakiHiroyuki Kanbayashi
    • Kazuaki SakuraiYoshinori UchidaHirofumi YamauchiYoko NakamuraAtsushi SasakiHiroyuki Kanbayashi
    • H01R1362
    • H01R13/62905
    • A female connector is provided with a first moving member and a second moving member which are capable of moving independently of each other, and the female connector is further provided with an operating member which is rotatable. The operating member is provided with a pair of first cam grooves whose spiral groove shapes are formed oppositely, while the first and second moving members are provided with first cam pins which are respectively inserted in the pair of first cam grooves. As the operating member is rotated, the first and second moving members are moved in mutually opposite directions. The first and second moving members are each provided with a pair of second cam grooves whose angles of inclination are opposite, while a male connector is provided with second cam pins which are inserted in the second cam grooves. As the first and second moving members are moved in the mutually opposite directions, a moving force acting in a connector-inserting direction is applied to the male connector through the cooperative movement of the first and second moving members.
    • 阴连接器设置有能够彼此独立地移动的第一移动构件和第二移动构件,并且阴连接器还设置有可旋转的操作构件。 操作构件设置有一对第一凸轮槽,其螺旋形槽形状相对地形成,而第一和第二移动构件设置有分别插入在该对第一凸轮槽中的第一凸轮销。 当操作构件旋转时,第一和第二移动构件沿彼此相反的方向移动。 第一移动构件和第二移动构件各自设置有一对第二凸轮槽,其倾斜角相反,而阳连接器设置有插入第二凸轮槽中的第二凸轮销。 随着第一和第二移动构件在相互相反的方向上移动,通过第一和第二移动构件的协作运动,沿着连接器插入方向作用的移动力施加到阳连接器。
    • 48. 发明授权
    • Method for the preparation of powder mixtures
    • 粉末混合物的制备方法
    • US5320796A
    • 1994-06-14
    • US55483
    • 1993-04-29
    • Asao HarashimaKaoru KunimatsuAtsushi SasakiRyuji Tachibana
    • Asao HarashimaKaoru KunimatsuAtsushi SasakiRyuji Tachibana
    • B01F3/18B01F7/10B29B7/42
    • B29B7/421B01F7/10B29B7/402B29B7/428B29C47/385B29C47/666B01F3/18
    • A method for producing powder mixtures capable of inducing an even more intimate, microhomogeneous intermixing in a heterogeneous powder composed of at least two types of powders. The method is effective even for the mixing of an aggregable powder and a nonaggregable powder. According to the method, a heterogeneous powder composed of at least two type of powders that have been preliminarily mixed by stirring is introduced into an inlet while a rotating axle is turning and is axially transported within a cylinder by a screw. As the heterogeneous powder passes between rotating disks and fixed disks, it is subjected to a highly efficient mixing by compression and shear forces due to a sliding-shear action exerted between depressions and elevations installed on the opposing surfaces of the rotating disks and fixed disks. The mixture passes in sequence through multiple stages of the rotating and fixed disks. A powder mixture, which has been microhomogeneously interdispersed, is discharged from the outlet.
    • 一种生产粉末混合物的方法,所述粉末混合物能够在由至少两种类型的粉末组成的非均质粉末中引起更加紧密,微均匀的混合。 该方法即使对于可聚集粉末和不可聚集粉末的混合也是有效的。 根据该方法,通过搅拌预先混合的至少两种粉末组成的非均相粉末在旋转轴转动的同时被引入入口,并通过螺杆在气缸内轴向传送。 当异质粉末通过旋转盘和固定盘之间时,由于在安装在旋转盘和固定盘的相对表面上的凹陷和高度之间施加的滑动剪切作用,它受到压缩和剪切力的高效混合。 混合物依次通过旋转和固定盘的多个阶段。 已经微分散分散的粉末混合物从出口排出。
    • 50. 发明授权
    • Flight control device, spacecraft, and reference trajectory correcting method
    • 飞行控制装置,航天器和参考轨迹校正方法
    • US09045240B2
    • 2015-06-02
    • US14131502
    • 2012-07-11
    • Tetsuya NagaseAtsushi Sasaki
    • Tetsuya NagaseAtsushi Sasaki
    • G01C23/00B64G1/24
    • B64G1/242B64G1/24B64G1/62
    • A flight control method and device for correcting a reference trajectory based on a distance from a current position to a target position in a spacecraft in flight. A CPU included in the spacecraft generates a reference trajectory which is a trajectory for allowing the spacecraft in flight to arrive at the target position on a celestial body with the atmosphere, and which is identified based on velocity or energy of the spacecraft and on drag acceleration of the spacecraft. The CPU calculates a ratio between the range that is a distance from the current position based on the reference trajectory to the target position, and the real range that is a real distance from a current position to the target position, and corrects the reference trajectory by calculating the drag acceleration in the reference trajectory using the calculated ratio.
    • 一种飞行控制方法和装置,用于基于从飞行中的航天器中的当前位置到目标位置的距离来校正参考轨迹。 包括在航天器中的CPU产生参考轨迹,该轨迹是允许飞行中的航天器到达具有大气的天体上的目标位置的轨迹,并且基于航天器的速度或能量以及拖曳加速度来识别 的航天器。 CPU根据基准轨迹计算与当前位置距离的距离与目标位置之间的距离,以及作为从当前位置到目标位置的实际距离的实际范围,并将基准轨迹修正为 使用计算的比率计算参考轨迹中的拖动加速度。