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11. 发明申请

US20050107576A1 Polyester resin and catalyst for polyester production, process for producing polyester resin with the catalyst, polyester resin obtained with the catalyst, and hollow molded container comprising the polyester resins 有权
标题翻译：用于聚酯生产的聚酯树脂和催化剂，用催化剂生产聚酯树脂的方法，用催化剂获得的聚酯树脂和包含聚酯树脂的中空成型容器
公开(公告)号：US20050107576A1
公开(公告)日：2005-05-19
申请号：US10504529
申请日：2003-02-13
申请人： Hideshi Hori , Fujito Ehara , Shouji Hiraoka , Ken Maeda , Tomohiro Suzuki , Nobumasa Mukai
发明人： Hideshi Hori , Fujito Ehara , Shouji Hiraoka , Ken Maeda , Tomohiro Suzuki , Nobumasa Mukai
IPC分类号： C08G63/80 , C08G63/82 , C08G63/83 , C08G63/84 , C08G63/85 , C08G63/78
CPC分类号： C08G63/82 , C08G63/80 , C08G63/83 , C08G63/84 , C08G63/85 , Y10T428/1352
摘要： The object of the present invention is to provide a high quality polyester resin having high productivity, stability and safety, a catalyst for polyester production with high catalytic activity, a method for producing the polyester resin with the catalyst, a polyester resin obtained with the catalyst, and a hollow molded container comprising the polyester resin. The polyester resin of the present invention satisfies specific parameters regarding polymerizability, stability, and metal content. The catalyst for polyester production satisfies specific parameters. The catalyst particularly preferably comprises: (a) a solid titanium-containing compound which has a maximum solubility in ethylene glycol of 1,000 ppm or more in terms of converted titanium amount when dissolved in ethylene glycol with heating at 150° C., and which comprises titanium, oxygen, carbon, and hydrogen, and optionally alkali metal, and has a Ti—O—C bond; and (b) an alkali metal compound, the molar ratio of the alkali metal atoms to the titanium atom in the catalyst being in the range of 20/1 to 0.1/1.
摘要翻译：本发明的目的是提供一种具有高生产率，稳定性和安全性的高品质聚酯树脂，具有高催化活性的聚酯生产催化剂，用催化剂生产聚酯树脂的方法，用催化剂得到的聚酯树脂和包含聚酯树脂的中空成型容器。本发明的聚酯树脂满足关于聚合性，稳定性和金属含量的具体参数。聚酯生产催化剂满足具体参数。催化剂特别优选包括：（a）当在150℃下加热溶解在乙二醇中时，以乙二醇的最大溶解度为1000ppm以上的固体含钛化合物以转化的钛量计，其包含钛，氧，碳和氢，以及任选的碱金属，并具有Ti-OC键; 和（b）碱金属化合物，催化剂中碱金属原子与钛原子的摩尔比在20/1至0.1 / 1的范围内。

12. 发明申请

US20140078803A1 Electric Power Converter 有权
标题翻译：电力转换器
公开(公告)号：US20140078803A1
公开(公告)日：2014-03-20
申请号：US14122713
申请日：2012-05-25
申请人： Atsuo Nishihara , Ken Maeda , Kinya Nakatsu , Yukio Hattori
发明人： Atsuo Nishihara , Ken Maeda , Kinya Nakatsu , Yukio Hattori
IPC分类号： H02M7/00
CPC分类号： H02M7/003 , H02M7/797 , H05K7/1432 , H05K7/20927
摘要： An electric power converter is provided with: a power semiconductor module, which has a power semiconductor element that converts a direct current into an alternating current; a capacitor module, which has a capacitor element that smooths the direct current; and a cooling body, which cools the power semiconductor module and the capacitor module. The capacitor module has a case, which has an approximately rectangular shape, has an opening formed in one surface, and has a space for housing the capacitor element; and a DC conductor for electrically connecting the power semiconductor element and the capacitor element to each other. The cooling body is formed to face the bottom surface on the inner wall of the case, and both the side surfaces of the case, the side surfaces facing each other. Between the capacitor element and the inner wall surfaces of the case, the direct current conductor is formed along the bottom surface and both the side surfaces of the case.
摘要翻译：电力转换器具有：功率半导体模块，具有将直流电转换为交流电的功率半导体元件; 电容器模块，其具有使直流平滑的电容器元件; 以及冷却功率半导体模块和电容器模块的冷却体。电容器模块具有大致矩形形状的壳体，具有形成在一个表面上的开口，并且具有用于容纳电容器元件的空间; 以及用于将功率半导体元件和电容器元件彼此电连接的DC导体。冷却体形成为面对壳体的内壁上的底面，并且壳体的两侧表面彼此面对。在电容器元件和壳体的内壁表面之间，直流导体沿壳体的底表面和两个侧表面形成。

13. 发明授权

US08038101B2 Attitude change control method, attitude change control system, attitude change control program and program recording medium 有权
标题翻译：姿态改变控制方法，姿态变化控制系统，姿态变化控制程序和程序记录介质
公开(公告)号：US08038101B2
公开(公告)日：2011-10-18
申请号：US12027769
申请日：2008-02-07
申请人： Keita Ogo , Toshio Kamiya , Ken Maeda
发明人： Keita Ogo , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28
CPC分类号： B64G1/286 , G05D1/0883
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

14. 发明申请

US20110052897A1 THERMAL INSULATION MATERIAL 审中-公开
标题翻译：热绝缘材料
公开(公告)号：US20110052897A1
公开(公告)日：2011-03-03
申请号：US12874393
申请日：2010-09-02
申请人： Yoshihiko Goto , Yasuo Ito , Ken Maeda , Akifumi Sakamoto
发明人： Yoshihiko Goto , Yasuo Ito , Ken Maeda , Akifumi Sakamoto
IPC分类号： B32B7/08
CPC分类号： B32B7/04 , B32B3/08 , B32B5/16 , B32B5/22 , B32B5/245 , B32B5/26 , B32B5/30 , B32B7/08 , B32B2262/10 , B32B2264/02 , B32B2266/025 , B32B2266/0278 , B32B2307/304 , B32B2307/546 , B32B2307/72 , B32B2419/00 , Y10T428/249923
摘要： The present invention relates to a thermal insulation material including a first molded article formed by compression-molding inorganic nanoparticles, a second molded article laminated on at least one side of the first molded article and having a bending strength of at least 0.4 MPa, and an accouplement coupling the first molded article and the second molded article.
摘要翻译：本发明涉及一种绝热材料，其包括通过压缩无机纳米颗粒而形成的第一模塑制品，在第一模塑制品的至少一侧层叠的第二模塑制品，并且具有至少0.4MPa的弯曲强度，以及耦合第一模制品和第二模塑制品的交流电耦合。

15. 发明申请

US20090218449A1 ATTITUDE CONTROL DATA CREATING METHOD, AND ATTITUDE CONTROL SYSTEM APPLYING THE METHOD 有权
标题翻译：态度控制数据创建方法以及应用方法的态度控制系统
公开(公告)号：US20090218449A1
公开(公告)日：2009-09-03
申请号：US12300449
申请日：2007-05-02
申请人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
发明人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
IPC分类号： B64G1/28 , B64G1/24
CPC分类号： B64G1/24 , B64G1/283 , B64G1/286 , B64G1/36 , B64G1/38 , G05D1/0883
摘要： In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.
摘要翻译：为了通过姿态机动来控制具有柔性构件（50）的可移动物体的姿态，首先，基于姿态机动时的柔性构件的振动，例如，不包括频率成分相等的取样函数达到或高于特定频率。利用采样功能，创建控制目标值作为先前频率整形型的前馈控制定律。基于控制目标值，创建姿态控制数据。姿态控制数据可以用于相对于可移动物体的姿态操纵。

16. 发明申请

US20090039202A1 Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium 审中-公开
标题翻译：态度变化控制方法，态度变化控制系统，态度变化控制程序和程序记录介质
公开(公告)号：US20090039202A1
公开(公告)日：2009-02-12
申请号：US12191389
申请日：2008-08-14
申请人： Keita Ogo , Toshio Kamiya , Ken Maeda
发明人： Keita Ogo , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28 , B64G1/24
CPC分类号： B64G1/286 , B64G2001/245
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

17. 发明申请

US20080203230A1 ATTITUDE CHANGE CONTROL METHOD, ATTITUDE CHANGE CONTROL SYSTEM, ATTITUDE CHANGE CONTROL PROGRAM AND PROGRAM RECORDING MEDIUM 有权
标题翻译：态度变化控制方法，态度变化控制系统，态度变化控制程序和程序记录介质
公开(公告)号：US20080203230A1
公开(公告)日：2008-08-28
申请号：US12027769
申请日：2008-02-07
申请人： KEITA OGO , Toshio Kamiya , Ken Maeda
发明人： KEITA OGO , Toshio Kamiya , Ken Maeda
IPC分类号： B64G1/28
CPC分类号： B64G1/286 , G05D1/0883
摘要： Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.
摘要翻译：公开了一种姿态改变控制系统，其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩，通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态，从而控制CMG 40改变姿态太空工艺动力50目标方向。

18. 发明授权

US09246408B2 Power conversion apparatus 有权
标题翻译：电力转换装置
公开(公告)号：US09246408B2
公开(公告)日：2016-01-26
申请号：US14122800
申请日：2012-05-22
申请人： Ken Maeda , Toshiya Satoh , Hiroyuki Yamai
发明人： Ken Maeda , Toshiya Satoh , Hiroyuki Yamai
IPC分类号： H02M7/537 , H02M7/5387 , H02M7/00 , H05K7/14
CPC分类号： H02M7/5387 , H02M7/003 , H05K7/1432
摘要： The power conversion apparatus includes an inverter circuit which converts a DC current into an AC current and have a U-phase, V-phase, and w-phase power semiconductor modules, and a capacitor module for smoothing the DC current. Each of the power semiconductor modules is configured separately and connected to a first bus bar. The first bus bar is configured with a first positive side bus bar, a first negative side bus bar, and a first insulation member arranged between the first positive side bus bar and the first negative side bus bar. The first bus bar includes a first to third terminals to which the U-phase, V-phase, and W-phase power semiconductor modules are connected, respectively, and a fourth terminal connected to a terminal of the second bus bar protruding from a surface of sealing material of a second bus bar.
摘要翻译：电力转换装置包括将DC电流转换为AC电流并具有U相，V相和w相功率半导体模块的逆变器电路以及用于平滑DC电流的电容器模块。每个功率半导体模块分别配置并连接到第一母线。第一汇流条配置有第一正侧汇流条，第一负侧汇流条和布置在第一正侧汇流条和第一负侧汇流条之间的第一绝缘构件。第一母线包括分别连接有U相，V相和W相功率半导体模块的第一至第三端子，以及连接到从表面突出的第二母线的端子的第四端子的第二母线的密封材料。

19. 发明申请

US20140085955A1 Power Conversion Apparatus 有权
标题翻译：电力转换装置
公开(公告)号：US20140085955A1
公开(公告)日：2014-03-27
申请号：US14122800
申请日：2012-05-22
申请人： Ken Maeda , Toshiya Satoh , Hiroyuki Yamai
发明人： Ken Maeda , Toshiya Satoh , Hiroyuki Yamai
IPC分类号： H02M7/5387
CPC分类号： H02M7/5387 , H02M7/003 , H05K7/1432
摘要： The power conversion apparatus includes an inverter circuit which converts a DC current into an AC current and have a U-phase, V-phase, and w-phase power semiconductor modules, and a capacitor module for smoothing the DC current. Each of the power semiconductor modules is configured separately and connected to a first bus bar. The first bus bar is configured with a first positive side bus bar, a first negative side bus bar, and a first insulation member arranged between the first positive side bus bar and the first negative side bus bar. The first bus bar includes a first to third terminals to which the U-phase, V-phase, and W-phase power semiconductor modules are connected, respectively, and a fourth terminal connected to a terminal of the second bus bar protruding from a surface of sealing material of a second bus bar.
摘要翻译：电力转换装置包括将DC电流转换为AC电流并具有U相，V相和w相功率半导体模块的逆变器电路以及用于平滑DC电流的电容器模块。每个功率半导体模块分别配置并连接到第一母线。第一汇流条配置有第一正侧汇流条，第一负侧汇流条和布置在第一正侧汇流条和第一负侧汇流条之间的第一绝缘构件。第一母线包括分别连接有U相，V相和W相功率半导体模块的第一至第三端子，以及连接到从表面突出的第二母线的端子的第四端子的第二母线的密封材料。

20. 发明授权

US08186627B2 Attitude control data creating method, and attitude control system applying the method 有权
标题翻译：态度控制数据创建方法，姿态控制系统应用该方法
公开(公告)号：US08186627B2
公开(公告)日：2012-05-29
申请号：US12300449
申请日：2007-05-02
申请人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
发明人： Toshio Kamiya , Ken Maeda , Tatsuaki Hashimoto , Shinichiro Sakai
IPC分类号： B64G1/36
CPC分类号： B64G1/24 , B64G1/283 , B64G1/286 , B64G1/36 , B64G1/38 , G05D1/0883
摘要： In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.
摘要翻译：为了通过姿态机动来控制具有柔性构件（50）的可移动物体的姿态，首先，基于姿态机动时的柔性构件的振动，例如，不包括频率成分相等的取样函数达到或高于特定频率。利用采样功能，创建控制目标值作为先前频率整形型的前馈控制定律。基于控制目标值，创建姿态控制数据。姿态控制数据可以用于相对于可移动物体的姿态操纵。

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