专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08973869B2 Landing gear retraction/extension device of aircraft 有权
标题翻译：飞机起落架撤离/延伸装置
公开(公告)号：US08973869B2
公开(公告)日：2015-03-10
申请号：US13618540
申请日：2012-09-14
申请人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
发明人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
IPC分类号： B64C25/22 , F15B21/04 , F15B7/00 , B64C13/50 , F15B1/26
CPC分类号： B64C25/22 , B64C13/504 , F15B1/26 , F15B7/006 , F15B21/042 , F15B2211/20515 , F15B2211/20538 , F15B2211/20561 , F15B2211/27 , F15B2211/3058 , F15B2211/411 , F15B2211/4159 , F15B2211/6343 , F15B2211/6651 , F15B2211/8752
摘要： A landing gear retraction/extension device includes a hydraulic actuator, a hydraulic circuit, a hydraulic pump, an electric motor, and a driver. Part of the hydraulic circuit is provided such that heat is exchangeable between operation oil and each of the electric motor and the driver. The driver supplies power to the electric motor before landing of an aircraft such that an operation oil temperature is higher than a predetermined temperature upon the landing of the aircraft.
摘要翻译：起落架缩回/延伸装置包括液压致动器，液压回路，液压泵，电动马达和驱动器。设置液压回路的一部分，使得在操作油和电动马达和驱动器中的每一个之间可以更换热量。驾驶员在飞机着陆之前向电动机供电，使飞机降落时操作油温度高于预定温度。

2. 发明授权

US09057390B2 Electro hydrostatic actuator 有权
标题翻译：静电静电执行机构
公开(公告)号：US09057390B2
公开(公告)日：2015-06-16
申请号：US13617444
申请日：2012-09-14
申请人： Takaaki Onishi , Taku Kondo , Yasuto Onomichi , Shogo Hagihara , Ryo Takaki
发明人： Takaaki Onishi , Taku Kondo , Yasuto Onomichi , Shogo Hagihara , Ryo Takaki
IPC分类号： F15B15/18 , B64C13/50
CPC分类号： F15B15/18 , B64C13/504
摘要： An electro hydrostatic actuator includes an actuator body, a hydraulic pump driven to supply operation oil to the actuator body, and an electric motor configured to drive the hydraulic pump. Each of the hydraulic pump and the electric motor is placed so as to surround the outer periphery of the actuator body, and the hydraulic pump and the electric motor are arranged in a direction along a center axis.
摘要翻译：电静液压致动器包括致动器主体，被驱动以向致动器主体供应操作油的液压泵和构造成驱动液压泵的电动机。每个液压泵和电动机被放置成围绕致动器主体的外周，并且液压泵和电动机沿着中心轴线的方向设置。

3. 发明授权

US06996447B2 Group management apparatus 失效
标题翻译：集团管理设备
公开(公告)号：US06996447B2
公开(公告)日：2006-02-07
申请号：US10798755
申请日：2004-03-10
申请人： Takaaki Onishi , Takahiro Komuro
发明人： Takaaki Onishi , Takahiro Komuro
IPC分类号： G06F19/00
CPC分类号： G05B23/0283 , G05B19/41865 , G05B2219/32232 , Y02P90/14 , Y02P90/20
摘要： A lump management apparatus comprising a management computer which is connected with inspection/manufacturing apparatus computers, and includes a transmission/reception function to transmit/receive each information item of the operation conditions set to the respective inspection/manufacturing apparatuses or the maintenance information from each sensor unit to/from the respective apparatus computers, a change function to intensively manage the operation conditions set to the respective apparatus computers in a lump and change the operation conditions in a lump with respect to the computer of the specified each inspection/manufacturing apparatus, a notification function to intensively manage the maintenance information from each sensor unit in a lump, predict an abnormality of the respective inspection/manufacturing apparatuses, and notify a warning at the time of occurrence of the abnormality, and a display function to display each information item of the operation conditions of the respective inspection/manufacturing apparatuses and the like on the same screen of a monitor device.
摘要翻译：一种管理计算机，包括与检查/制造设备计算机连接的管理计算机，并且包括发送/接收功能，用于发送/接收从各检查/制造设备设置的操作条件或每个维护信息的每个信息项传感器单元到各个设备计算机，改变功能，以集中地管理设置到各个设备计算机的操作条件，并相对于指定的每个检查/制造设备的计算机改变一次的操作条件，一个通知功能，用于集中地管理来自每个传感器单元的维护信息，预测各个检查/制造设备的异常，并且在异常发生时通知警告，以及显示每个信息项的显示功能的操作条件观察检查/制造设备等在监视器装置的同一屏幕上。

4. 发明申请

US20130067898A1 ELECTRO HYDROSTATIC ACTUATOR 有权
标题翻译：电动液压致动器
公开(公告)号：US20130067898A1
公开(公告)日：2013-03-21
申请号：US13617444
申请日：2012-09-14
申请人： Takaaki Onishi , Taku Kondo , Yasuto Onomichi , Shogo Hagihara , Ryo Takaki
发明人： Takaaki Onishi , Taku Kondo , Yasuto Onomichi , Shogo Hagihara , Ryo Takaki
IPC分类号： F15B15/18
CPC分类号： F15B15/18 , B64C13/504
摘要： An electro hydrostatic actuator includes an actuator body, a hydraulic pump driven to supply operation oil to the actuator body, and an electric motor configured to drive the hydraulic pump. Each of the hydraulic pump and the electric motor is placed so as to surround the outer periphery of the actuator body, and the hydraulic pump and the electric motor are arranged in a direction along a center axis.
摘要翻译：电静液压致动器包括致动器主体，被驱动以向致动器主体供应操作油的液压泵和构造成驱动液压泵的电动机。每个液压泵和电动机被放置成围绕致动器主体的外周，并且液压泵和电动机沿着中心轴线的方向设置。

5. 发明申请

US20130068885A1 LANDING GEAR RETRACTION/EXTENSION DEVICE OF AIRCRAFT 有权
标题翻译：起落架齿轮减速/飞机延伸装置
公开(公告)号：US20130068885A1
公开(公告)日：2013-03-21
申请号：US13618540
申请日：2012-09-14
申请人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
发明人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
IPC分类号： B64C25/22
CPC分类号： B64C25/22 , B64C13/504 , F15B1/26 , F15B7/006 , F15B21/042 , F15B2211/20515 , F15B2211/20538 , F15B2211/20561 , F15B2211/27 , F15B2211/3058 , F15B2211/411 , F15B2211/4159 , F15B2211/6343 , F15B2211/6651 , F15B2211/8752
摘要： A landing gear retraction/extension device includes a hydraulic actuator, a hydraulic circuit, a hydraulic pump, an electric motor, and a driver. Part of the hydraulic circuit is provided such that heat is exchangeable between operation oil and each of the electric motor and the driver. The driver supplies power to the electric motor before landing of an aircraft such that an operation oil temperature is higher than a predetermined temperature upon the landing of the aircraft.
摘要翻译：起落架缩回/延伸装置包括液压致动器，液压回路，液压泵，电动马达和驱动器。设置液压回路的一部分，使得在操作油和电动马达和驱动器中的每一个之间可以更换热量。驾驶员在飞机着陆之前向电动机供电，使飞机降落时操作油温度高于预定温度。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式