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1. 发明授权

US09201115B2 Wafer inspection apparatus 有权
标题翻译：晶圆检查仪
公开(公告)号：US09201115B2
公开(公告)日：2015-12-01
申请号：US13231341
申请日：2011-09-13
申请人： Hiroshi Yamada , Takaaki Hoshino , Shinji Kojima , Takeshi Saigusa , Hiroshi Shimoyama
发明人： Hiroshi Yamada , Takaaki Hoshino , Shinji Kojima , Takeshi Saigusa , Hiroshi Shimoyama
IPC分类号： G01R31/20 , G01R31/28
CPC分类号： G01R31/2887 , G01R31/2891 , G01R31/2893
摘要： A wafer inspection apparatus includes a first and second wafer transfer mechanisms, an alignment chamber, a second wafer transfer mechanism and a plurality of inspection chambers. The first wafer transfer mechanism is installed at a first transfer area to transfer wafers individually from a housing. The alignment chamber has an alignment mechanism configured to align the wafer at an inspection position for an electrical characteristics inspection. The second wafer transfer mechanism is configured to transfer the wafer through a wafer retaining support in a second transfer area formed along the first transfer area and an alignment area. The plurality of inspection chambers is arranged at an inspection area formed along the second transfer area and is configured to inspect electrical characteristics of the wafer transferred by the second wafer transfer mechanism through the wafer retaining support.
摘要翻译：晶片检查装置包括第一和第二晶片传送机构，对准室，第二晶片传送机构和多个检查室。第一晶片传送机构安装在第一传送区域以分别从外壳传送晶片。对准室具有对准机构，其配置成将晶片对准用于电特性检查的检查位置。第二晶片传送机构被配置为将晶片通过晶片保持支撑件传送在沿着第一传送区域形成的第二传送区域和对准区域中。多个检查室被布置在沿着第二传送区域形成的检查区域，并且被配置为检查由第二晶片传送机构通过晶片保持支撑件传送的晶片的电特性。

2. 发明授权

US06871925B2 Inkjet printing apparatus, control method therefor, and program 有权
标题翻译：喷墨打印设备，其控制方法和程序
公开(公告)号：US06871925B2
公开(公告)日：2005-03-29
申请号：US10412288
申请日：2003-04-14
申请人： Tadashi Yamamoto , Takaaki Hoshino
发明人： Tadashi Yamamoto , Takaaki Hoshino
IPC分类号： B41J2/175 , B41J29/38 , B41J29/393
CPC分类号： B41J2/17566 , B41J2002/17579
摘要： In an inkjet printing apparatus which holds a printhead for performing printing by using ink supplied from an ink tank via an ink supply channel, the ink tank has a tank-side terminal for detecting the presence state of ink in the ink tank. The printhead has a head-side terminal for detecting the presence state of ink in the printhead. The printing apparatus detects at least one of the presence state of ink in the ink tank, printhead, and ink supply channel by selecting a terminal used for detection between the tank-side terminal and the head-side terminal.
摘要翻译：在通过使用通过供墨通道从墨水盒供给的墨水保持用于执行打印的打印头的喷墨打印设备中，墨水盒具有用于检测墨水盒中的墨水的存在状态的墨盒侧端子。打印头具有头侧端子，用于检测打印头中墨的存在状态。打印装置通过选择用于罐侧端子和头侧端子之间的检测的端子来检测墨罐，打印头和供墨通道中的油墨的存在状态中的至少一种。

3. 发明授权

US5482228A Landing gear assembly for airplane 失效
标题翻译：飞机起落架总成
公开(公告)号：US5482228A
公开(公告)日：1996-01-09
申请号：US131705
申请日：1993-10-05
申请人： Takaaki Hoshino
发明人： Takaaki Hoshino
IPC分类号： B64C25/04 , B64C25/14 , B64C25/16 , B64C25/50 , B64C25/10
CPC分类号： B64C25/50 , B64C25/16
摘要： A nose landing gear assembly on an airplane with a front fuselage section having a wheel bay defined therein and a pair of laterally spaced side compartments defined therein on each side of the wheel bay by respective laterally spaced side walls. A nose landing gear is mounted on the fuselage section for pivotal lifting and lowering movement into and out of the wheel bay. The nose landing gear assembly includes an actuator disposed in one of the side compartments for lifting the nose landing gear into and lowering the nose landing gear out of the wheel bay, and a steering device disposed in the other of the side compartments for steering the nose landing gear while the airplane is taxiing. Since the actuator and the steering device are concealed in the respective side compartments, they are protected from foreign-object damage. The nose landing gear assembly allows the airplane cabin to have increased space because the actuator and the steering device are positioned laterally of the nose landing gear.
摘要翻译：飞机上的前起落架组件具有限定在其中的轮舱的前机身部分和通过相应的侧向间隔开的侧壁限定在车架隔板的每一侧上的一对横向间隔开的侧隔室。在起落架上安装了一个起落架，用于枢转提升和下降进入和离开车轮舱。前起落架组件包括一个致动器，该致动器设置在一个侧隔室中，用于将前起落架提升到起落架中并将前起落架从轮舱中降下;以及转向装置，其设置在另一个侧舱中，用于转向鼻起落架，而飞机正在滑行。由于致动器和转向装置被隐藏在相应的侧隔室中，因此它们被保护免受异物损坏。前起落架组件允许飞机机舱具有增加的空间，因为致动器和转向装置位于前起落架的侧面。

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