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1. 发明申请

US20050145750A1 Flying body for firing from a tube with over-calibre stabilisers 有权
标题翻译：飞行体从具有超大口径稳定器的管中点燃
公开(公告)号：US20050145750A1
公开(公告)日：2005-07-07
申请号：US10504116
申请日：2003-02-06
申请人： Shinichi Okada , Sadao Okawa , Masato Shinomiya , Makoto Mochizuki
发明人： Shinichi Okada , Sadao Okawa , Masato Shinomiya , Makoto Mochizuki
IPC分类号： F42B10/16 , F42B10/20 , F41G7/00
CPC分类号： F42B10/20 , F42B10/16
摘要： A missile to be fired from a barrel contains a tail, a tail sleeve attached to the tail, a stop element fixed to the tail sleeve, and a movable structural part disposed at the tail. Fin assembly wings are provided and are to be released from a subcaliber launch position to an overcaliber functional position by the movable structural part moving toward the stop element through a given distance. A pressure area is disposed between the tail end surface and the movable structural part. A propellant gas enters the pressure area during the firing of the missile, for moving the movable structural part away from the tail end surface against the stop element after firing. Bearing shafts are supported by the tail sleeve, the fin assembly wings are configured as a wrap around tail fin assembly held about the bearing shafts.
摘要翻译：从枪管发射的导弹包含尾巴，尾巴附着在尾部，固定在尾部套筒上的止动元件和设在尾部的可移动结构部件。翅片组装翅膀被设置并且通过可移动结构部件朝着停止元件移动给定距离而从亚光子发射位置释放到超光纤功能位置。压力区域设置在尾端表面和可移动结构部件之间。在发射导弹期间，推进剂气体进入压力区域，用于将可动结构部件从射出后的尾端表面靠近止动元件移动。轴套由尾套支撑，翅片组件翼被构造成围绕轴承轴保持的尾翼组件的卷绕。

2. 发明授权

US07004425B2 Flying body for firing from a tube with over-caliber stabilizers 有权
标题翻译：飞行体从具有超大口径稳定器的管中点燃
公开(公告)号：US07004425B2
公开(公告)日：2006-02-28
申请号：US10504116
申请日：2003-02-06
申请人： Shinichi Okada , Sadao Okawa , Masato Shinomiya , Makoto Mochizuki
发明人： Shinichi Okada , Sadao Okawa , Masato Shinomiya , Makoto Mochizuki
IPC分类号： B64C5/12
CPC分类号： F42B10/20 , F42B10/16
摘要： A missile to be fired from a barrel contains a tail, a tail sleeve attached to the tail, a stop element fixed to the tail sleeve, and a movable structural part disposed at the tail. Fin assembly wings are provided and are to be released from a subcaliber launch position to an overcaliber functional position by the movable structural part moving toward the stop element through a given distance. A pressure area is disposed between the tail end surface and the movable structural part. A propellant gas enters the pressure area during the firing of the missile, for moving the movable structural part away from the tail end surface against the stop element after firing. Bearing shafts are supported by the tail sleeve, the fin assembly wings are configured as a wrap around tail fin assembly held about the bearing shafts.
摘要翻译：从枪管发射的导弹包含尾巴，尾巴附着在尾部，固定在尾部套筒上的止动元件和设在尾部的可移动结构部件。翅片组装翅膀被设置并且通过可移动结构部件朝着停止元件移动给定距离而从亚光子发射位置释放到超光纤功能位置。压力区域设置在尾端表面和可移动结构部件之间。在发射导弹期间，推进剂气体进入压力区域，用于将可动结构部件从射出后的尾端表面靠近止动元件移动。轴套由尾套支撑，翅片组件翼被构造成围绕轴承轴保持的尾翼组件的卷绕。

3. 发明申请

US20050176382A1 Mobile communication apparatus 审中-公开
标题翻译：移动通信装置
公开(公告)号：US20050176382A1
公开(公告)日：2005-08-11
申请号：US10513677
申请日：2003-04-23
申请人： Makoto Mochizuki , Tadahisa Kamiya , Masato Shinomiya
发明人： Makoto Mochizuki , Tadahisa Kamiya , Masato Shinomiya
IPC分类号： H04B1/44 , H04B7/06 , H04B7/08 , H04B7/26 , H04B1/38
CPC分类号： H04B7/0602 , H04B7/0805
摘要： A purpose of the present invention is to improve a reception sensitivity when simultaneous transmitting/receiving operations are not carried out in a mobile communication apparatus capable of performing the simultaneous transmitting/receiving operations. The mobile communication apparatus, according to the present invention, is comprised of an antenna selector (13) for switching a connection between a first antenna A (11) and a second antenna B (12), and is selectively connected with a transmission system which contains a transmission-side filter (14) and a transmitting unit (16), and with respect to a reception system which contains a reception-side filter (15) and a receiving unit (17). In the antenna selector (13), at timing for performing a transmitting operation, the transmission system is connected to any one of the antennas A (11) and B (12) by way of switches A (21) and C (23); at timing for performing a receiving operation, the reception system is connected to any one of the antennas A (11) and B (12) by way of switches B (22) and D (24); and at timing for executing transmitting/receiving operations at the same time, both the transmission-side filter (14) and the reception-side filter (15) are connected to any one of the antennas A (11) and B (12) by way of the switches A (21), B (22), C (23), and D (24), so that an antenna commonly-operable device is constructed.
摘要翻译：本发明的目的是提高在能够执行同时发送/接收操作的移动通信设备中不执行同时发送/接收操作时的接收灵敏度。根据本发明的移动通信装置包括用于切换第一天线A（11）和第二天线B（12）之间的连接的天线选择器（13），并且选择性地与传输系统连接，传输系统包含发送侧滤波器（14）和发送单元（16），并且涉及包含接收侧滤波器（15）和接收单元（17）的接收系统。在天线选择器（13）中，在执行发送操作的定时，传输系统通过开关A（21）和C（23）连接到天线A（11）和B（12）中的任一个。在接收操作的定时，接收系统通过开关B（22）和D（24）连接到天线A（11）和B（12）中的任一个。并且在同时执行发送/接收操作的定时，发送侧滤波器（14）和接收侧滤波器（15）都通过以下方式连接到天线A（11）和B（12）中的任一个：开关A（21），B（22），C（23）和D（24）的方式，构成天线共用操作装置。

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