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1. 发明申请

US20100221089A1 SUBSTRATE SUPPORT APPARATUS, SUBSTRATE TRANSPORT APPARATUS, AND ELECTRICAL DEVICE MANUFACTURING METHOD 有权
标题翻译：基板支撑装置，基板运输装置和电气装置制造方法
公开(公告)号：US20100221089A1
公开(公告)日：2010-09-02
申请号：US12706901
申请日：2010-02-17
申请人： Masahiro Atsumi , Masaaki Ishida
发明人： Masahiro Atsumi , Masaaki Ishida
IPC分类号： H01L21/673 , H01L21/677
CPC分类号： H01L21/67742
摘要： A substrate support apparatus which inserts a substrate holding portion into a center hole formed in a substrate, and supports the substrate in a vertical orientation by the substrate holding portion, comprises a first connecting plate connected to the substrate holding portion, a second connecting plate which faces the first connecting plate and is connected to a transport robot that transports the substrate to a substrate holder, at least three linear support members configured to connect the first connecting plate to the second connecting plate, and an elastic shock absorbing member inserted between the first connecting plate and the second connecting plate.
摘要翻译：一种基板支撑装置，其将基板保持部插入到形成在基板上的中心孔中，并且通过基板保持部沿垂直取向支撑基板，包括连接到基板保持部的第一连接板，第二连接板，面向第一连接板并且连接到运输机器人，其将基板传送到基板保持器，至少三个线性支撑构件，其构造成将第一连接板连接到第二连接板，以及弹性冲击吸收构件，其插入在第一连接板之间连接板和第二连接板。

2. 发明授权

US10501210B2 Aerospace vehicle system 有权
公开(公告)号：US10501210B2
公开(公告)日：2019-12-10
申请号：US12254456
申请日：2008-10-20
申请人： Yoshikatsu Kuroda , Masahiro Atsumi , Naohiko Abe , Masahiro Kato
发明人： Yoshikatsu Kuroda , Masahiro Atsumi , Naohiko Abe , Masahiro Kato
IPC分类号： B64G1/24 , B64G1/00
CPC分类号： B64G1/002
摘要： In an aerospace vehicle in which a satellite is detachably adapted to the first stage rocket and the second stage rocket, an electronic device 65 is installed in the satellite 60, wherein the electronic device 65 controls the first stage rocket 10 and the second stage rocket 20 before the satellite is detached from the first stage rocket 10 and the second stage rocket 20. Thereby, it is unnecessary to provide sensors, radio devices and electronic devices for exclusive use with respect to the first stage rocket 10 and the second stage rocket 20 so that a manufacturing cost of the rockets 10 and 20 can be reduced and a total weight of the rockets 10 and 20 can become lighter by omitting these equipments. Thus, an aerospace vehicle system within the rockets 10 and 20 can be simplified and a launch of the aerospace vehicle can be prepared within a short period.

3. 发明授权

US08770906B2 Substrate support apparatus and substrate transport apparatus having shock absorption 有权
标题翻译：具有减震功能的基板支撑装置和基板输送装置
公开(公告)号：US08770906B2
公开(公告)日：2014-07-08
申请号：US12706901
申请日：2010-02-17
申请人： Masahiro Atsumi , Masaaki Ishida
发明人： Masahiro Atsumi , Masaaki Ishida
IPC分类号： H01L21/763 , H01L21/677
CPC分类号： H01L21/67742
摘要： A substrate support apparatus has a substrate holding portion to be inserted into a center hole formed in a substrate to support the substrate in a vertical orientation, and includes a first connecting plate connected to the substrate holding portion and a second connecting plate which faces the first connecting plate and is connectable to a transport robot that transports the substrate to a substrate holder. In addition, a shock absorbing member is arranged between the first connecting plate and the second connecting plate so as to allow a movement of the first connecting plate relative to the second connecting plate in horizontal and vertical directions. Support members are configured to connect the first connecting plate to the second connecting plate while allowing the movement of the first connecting plate relative to the second connecting plate.
摘要翻译：基板支撑装置具有基板保持部，其插入到形成在基板上的中心孔中，以在垂直方向上支撑基板，并且包括连接到基板保持部的第一连接板和面向第一连接板，并且可连接到将基板传送到基板保持器的运输机器人。此外，在第一连接板和第二连接板之间布置有减震构件，以允许第一连接板相对于第二连接板在水平和垂直方向上的移动。支撑构件被构造成将第一连接板连接到第二连接板，同时允许第一连接板相对于第二连接板的移动。

4. 发明申请

US20090206205A1 AEROSPACE VEHICLE SYSTEM 审中-公开
标题翻译：航空汽车系统
公开(公告)号：US20090206205A1
公开(公告)日：2009-08-20
申请号：US12254456
申请日：2008-10-20
申请人： Yoshikatsu KURODA , Masahiro ATSUMI , Naohiko ABE , Masahiro KATO
发明人： Yoshikatsu KURODA , Masahiro ATSUMI , Naohiko ABE , Masahiro KATO
IPC分类号： B64G1/40
CPC分类号： B64G1/002 , B64G1/288 , B64G1/401 , B64G1/402 , B64G1/428 , B64G1/641
摘要： In an aerospace vehicle in which a satellite is detachably adapted to the first step rocket and the second step rocket, an electronic device 65 is installed in the satellite 60, wherein the electronic device 65 controls the first step rocket 10 and the second step rocket 20 before the satellite is detached from the first step rocket 10 and the second step rocket 20. Thereby, it is unnecessary to provide sensors, radio devices and electronic devices for exclusive use with respect to the first step rocket 10 and the second step rocket so that a manufacturing cost of the rockets 10 and 20 can be reduced and a total weight of the rockets 10 and 20 can become lighter by omitting these equipments. Thus, an aerospace vehicle system within the rockets 10 and 20 can be simplified and a launch of the aerospace vehicle can be prepared within a short period.
摘要翻译：在其中卫星可拆卸地适应于第一级火箭和第二级火箭的航空航天车辆中，电子设备65安装在卫星60中，其中电子设备65控制第一级火箭10和第二级火箭20 在卫星从第一步骤火箭10和第二步骤火箭20分离之前。因此，不需要提供关于第一步骤火箭10和第二步骤火箭专用的传感器，无线电装置和电子装置，使得可以减少火箭10和20的制造成本，并且通过省略这些设备，火箭10和20的总重量可以变轻。因此，可以简化火箭10和20内的航空航天系统，并且可以在短时间内准备航空航天车辆的发射。

5. 发明授权

US5407331A Motor-driven pump 失效
标题翻译：电动泵
公开(公告)号：US5407331A
公开(公告)日：1995-04-18
申请号：US3612
申请日：1993-01-13
申请人： Masahiro Atsumi
发明人： Masahiro Atsumi
IPC分类号： F04D13/06 , H02K7/14 , F04B17/03
CPC分类号： F02M37/048 , F04D13/0646 , F04D13/0666 , H02K7/14
摘要： An integrated motor-driven pump includes an electromagnet disposed in the pump casing opposite a magnet mounted to an impeller of the pump. The impeller is rotatably supported within the casing, and is rotated by inducing a repulsion force in the magnet. In addition, a bearing rotatably supporting the impeller is provided in a portion of the casing formed with a flow passageway which leads working fluid handled by the pump flow to both sides of the bearing so that the bearing can be lubricated and cooled by the working fluid.
摘要翻译：集成电动泵包括设置在泵壳体中的电磁体，该电磁铁安装在泵的叶轮上。叶轮可旋转地支撑在壳体内，并通过在磁体中引起排斥力而旋转。此外，在壳体的一部分中设置有可旋转地支撑叶轮的轴承，该部分形成有将由泵流处理的工作流体引导到轴承两侧的流动通道，使得轴承能够被工作流体润滑和冷却。

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