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公开(公告)号：US08753087B2
公开(公告)日：2014-06-17
申请号：US12979004
申请日：2010-12-27
申请人： Naoki Shibukawa , Yoriharu Murata , Akihiro Onoda , Daisuke Nomura , Tomohiro Tejima , Osamu Furuya , Kenichi Imai
发明人： Naoki Shibukawa , Yoriharu Murata , Akihiro Onoda , Daisuke Nomura , Tomohiro Tejima , Osamu Furuya , Kenichi Imai
IPC分类号： F01D5/22
CPC分类号： F01D1/04 , F01D5/22 , F05D2220/31 , F05D2220/3215 , F05D2260/96
摘要： A turbine rotor assembly 10 comprises a turbine rotor and a plurality of moving blades 20 implanted in a circumferential direction of the rotor. A flow passage is formed between each of the moving blades 20 and a circumferentially adjacent moving blade 20. Each of the moving blades 20 comprises a suction side connecting member 22 protruded on a blade suction surface 21 and a pressure side connecting member 24 protruded on a blade pressure surface 23, wherein the suction side connecting member 22 of each of the moving blades 20 is configured to be connected with the pressure side connecting member 24 of the circumferentially adjacent moving blade 20 to form an intermediate connecting member 30 between the moving blade 20 and the circumferentially adjacent moving blade 20 during a rotation of the turbine rotor. A downstream side end edge 32 of the intermediate connecting member 30 is positioned at an upstream side of a throat S of the flow passage.
摘要翻译： 涡轮转子组件10包括涡轮转子和沿转子的圆周方向注入的多个活动叶片20。 在每个活动叶片20和周向相邻的活动叶片20之间形成有流动通道。每个活动叶片20包括突出在叶片吸入表面21上的吸力侧连接构件22和在叶片吸入表面21上突出的压力侧连接构件24。 叶片压力表面23，其中每个动叶片20的吸力侧连接构件22构造成与周向相邻的活动叶片20的压力侧连接构件24连接，以在动叶片20之间形成中间连接构件30 以及在涡轮机转子的旋转期间周向相邻的移动叶片20。 中间连接构件30的下游侧端缘32位于流路的喉部S的上游侧。
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公开(公告)号：US20110158810A1
公开(公告)日：2011-06-30
申请号：US12979004
申请日：2010-12-27
申请人： Naoki Shibukawa , Yoriharu Murata , Akihiro Onoda , Daisuke Nomura , Tomohiro Tejima , Osamu Furuya , Kenichi Imai
发明人： Naoki Shibukawa , Yoriharu Murata , Akihiro Onoda , Daisuke Nomura , Tomohiro Tejima , Osamu Furuya , Kenichi Imai
IPC分类号： F01D5/22
CPC分类号： F01D1/04 , F01D5/22 , F05D2220/31 , F05D2220/3215 , F05D2260/96
摘要： A turbine rotor assembly 10 comprises a turbine rotor and a plurality of moving blades 20 implanted in a circumferential direction of the rotor. A flow passage is formed between each of the moving blades 20 and a circumferentially adjacent moving blade 20. Each of the moving blades 20 comprises a suction side connecting member 22 protruded on a blade suction surface 21 and a pressure side connecting member 24 protruded on a blade pressure surface 23, wherein the suction side connecting member 22 of each of the moving blades 20 is configured to be connected with the pressure side connecting member 24 of the circumferentially adjacent moving blade 20 to form an intermediate connecting member 30 between the moving blade 20 and the circumferentially adjacent moving blade 20 during a rotation of the turbine rotor. A downstream side end edge 32 of the intermediate connecting member 30 is positioned at an upstream side of a throat S of the flow passage.
摘要翻译： 涡轮转子组件10包括涡轮转子和沿转子的圆周方向注入的多个活动叶片20。 在每个活动叶片20和周向相邻的活动叶片20之间形成有流动通道。每个活动叶片20包括突出在叶片吸入表面21上的吸力侧连接构件22和在叶片吸入表面21上突出的压力侧连接构件24。 叶片压力表面23，其中每个动叶片20的吸力侧连接构件22构造成与周向相邻的活动叶片20的压力侧连接构件24连接，以在动叶片20之间形成中间连接构件30 以及在涡轮机转子的旋转期间周向相邻的移动叶片20。 中间连接构件30的下游侧端缘32位于流路的喉部S的上游侧。
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公开(公告)号：US07645119B2
公开(公告)日：2010-01-12
申请号：US11892375
申请日：2007-08-22
IPC分类号： F01D9/02
摘要： An axial flow turbine provided with a stage composed of a turbine nozzle and a turbine rotor blade arranged in an axial flow direction. Both end portions of a nozzle blade of the turbine nozzle are supported by a diaphragm inner ring and a diaphragm outer ring, and a flow passage is formed to have its diameter expanded from an upstream stage to a downstream stage. In such axial flow turbine, trailing edges at ends of the nozzle blade supported by the diaphragm inner ring and the diaphragm outer ring are curved as a curvature to an outlet side, and an intermediate portion between the trailing edges is formed to be straight.
摘要翻译： 一种轴流涡轮机，其具有由涡轮喷嘴构成的台架和沿轴向流动方向配置的涡轮机转子叶片。 涡轮喷嘴的喷嘴叶片的两端部由隔膜内圈和隔膜外圈支撑，形成从上游侧到下游侧的直径扩大的流路。 在这种轴流式涡轮机中，由隔膜内圈和隔膜外圈支撑的喷嘴的端部处的后缘作为曲率弯曲到出口侧，并且后缘之间的中间部分形成为直的。
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公开(公告)号：US07300247B2
公开(公告)日：2007-11-27
申请号：US11392956
申请日：2006-03-30
IPC分类号： F01D9/02
摘要： An axial flow turbine provided with a stage composed of a turbine nozzle and a turbine rotor blade arranged in an axial flow direction. Both end portions of a nozzle blade of the turbine nozzle are supported by a diaphragm inner ring and a diaphragm outer ring, and a flow passage is formed to have its diameter expanded from an upstream stage to a downstream stage. In such axial flow turbine, trailing edges at ends of the nozzle blade supported by the diaphragm inner ring and the diaphragm outer ring are curved as a curvature to an outlet side, and an intermediate portion between the trailing edges is formed to be straight.
摘要翻译： 一种轴流涡轮机，其具有由涡轮喷嘴构成的台架和沿轴向流动方向配置的涡轮机转子叶片。 涡轮喷嘴的喷嘴叶片的两端部由隔膜内圈和隔膜外圈支撑，形成从上游侧到下游侧的直径扩大的流路。 在这种轴流式涡轮机中，由隔膜内圈和隔膜外圈支撑的喷嘴的端部处的后缘作为曲率弯曲到出口侧，并且后缘之间的中间部分形成为直的。
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公开(公告)号：US20090110550A1
公开(公告)日：2009-04-30
申请号：US12243642
申请日：2008-10-01
IPC分类号： F01D1/02
CPC分类号： F01D1/02 , F01D5/145 , F01D9/02 , F01D11/10 , Y10S415/914
摘要： An axial flow turbine stage structure has: an annular diaphragm inner ring; an annular diaphragm outer ring arranged radially outside and coaxially with the diaphragm inner ring and separated from the diaphragm inner ring by an annular flow path interposed between them; stationary blades arranged peripherally at intervals in the annular flow path and rigidly secured to the diaphragm inner ring and the diaphragm outer ring; and moving blades rigidly secured to the outer periphery of a rotatable rotor and arranged peripherally at intervals respectively at axially downstream sides of the stationary blades. Through holes are formed in the diaphragm outer ring so as to allow axial upstream side and axially downstream side of the stationary blades to communicate with each other.
摘要翻译： 轴流涡轮机级结构具有：环形隔膜内圈; 环形隔膜外环，其设置在隔膜内环的径向外侧并与隔膜内圈同轴，并通过插入其间的环形流路与隔膜内圈分离; 固定叶片在环形流动路径中间隔设置并刚性地固定到隔膜内环和隔膜外圈; 以及刚性地固定到可旋转转子的外周并且周向地间隔地设置在固定叶片的轴向下游侧的移动叶片。 在隔膜外圈中形成通孔，以使固定叶片的轴向上游侧和轴向下游侧彼此连通。
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公开(公告)号：US08147180B2
公开(公告)日：2012-04-03
申请号：US12243642
申请日：2008-10-01
IPC分类号： F01D11/00
CPC分类号： F01D1/02 , F01D5/145 , F01D9/02 , F01D11/10 , Y10S415/914
摘要： An axial flow turbine stage structure has: an annular diaphragm inner ring; an annular diaphragm outer ring arranged radially outside and coaxially with the diaphragm inner ring and separated from the diaphragm inner ring by an annular flow path interposed between them; stationary blades arranged peripherally at intervals in the annular flow path and rigidly secured to the diaphragm inner ring and the diaphragm outer ring; and moving blades rigidly secured to the outer periphery of a rotatable rotor and arranged peripherally at intervals respectively at axially downstream sides of the stationary blades. Through holes are formed in the diaphragm outer ring so as to allow axial upstream side and axially downstream side of the stationary blades to communicate with each other.
摘要翻译： 轴流涡轮机级结构具有：环形隔膜内圈; 环形隔膜外环，其设置在隔膜内环的径向外侧并与隔膜内圈同轴，并通过插入其间的环形流路与隔膜内圈分离; 固定叶片在环形流动路径中间隔设置并刚性地固定到隔膜内环和隔膜外圈; 以及刚性地固定到可旋转转子的外周并且周向地间隔地设置在固定叶片的轴向下游侧的移动叶片。 在隔膜外圈中形成通孔，以使固定叶片的轴向上游侧和轴向下游侧彼此连通。
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公开(公告)号：US20080199310A1
公开(公告)日：2008-08-21
申请号：US11892375
申请日：2007-08-22
IPC分类号： F01D9/02
摘要： An axial flow turbine provided with a stage composed of a turbine nozzle and a turbine rotor blade arranged in an axial flow direction. Both end portions of a nozzle blade of the turbine nozzle are supported by a diaphragm inner ring and a diaphragm outer ring, and a flow passage is formed to have its diameter expanded from an upstream stage to a downstream stage. In such axial flow turbine, trailing edges at ends of the nozzle blade supported by the diaphragm inner ring and the diaphragm outer ring are curved as a curvature to an outlet side, and an intermediate portion between the trailing edges is formed to be straight.
摘要翻译： 一种轴流涡轮机，其具有由涡轮喷嘴构成的台架和沿轴向流动方向配置的涡轮机转子叶片。 涡轮喷嘴的喷嘴叶片的两端部由隔膜内圈和隔膜外圈支撑，形成从上游侧到下游侧的直径扩大的流路。 在这种轴流式涡轮机中，由隔膜内圈和隔膜外圈支撑的喷嘴的端部处的后缘作为曲率弯曲到出口侧，并且后缘之间的中间部分形成为直的。
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公开(公告)号：US20070086891A1
公开(公告)日：2007-04-19
申请号：US11392956
申请日：2006-03-30
IPC分类号： F01D9/00
摘要： An axial flow turbine provided with a stage composed of a turbine nozzle and a turbine rotor blade arranged in an axial flow direction. Both end portions of a nozzle blade of the turbine nozzle are supported by a diaphragm inner ring and a diaphragm outer ring, and a flow passage is formed to have its diameter expanded from an upstream stage to a downstream stage. In such axial flow turbine, trailing edges at ends of the nozzle blade supported by the diaphragm inner ring and the diaphragm outer ring are curved as a curvature to an outlet side, and an intermediate portion between the trailing edges is formed to be straight.
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公开(公告)号：US20110202221A1
公开(公告)日：2011-08-18
申请号：US13025415
申请日：2011-02-11
IPC分类号： G06F17/00
CPC分类号： B60K16/00 , B60K2016/003 , B60L8/003 , B60L11/1861 , B60L15/2045 , B60W50/0097 , B60W2550/12 , B60W2550/402 , H02J7/35 , Y02T10/6269 , Y02T10/645 , Y02T10/7011 , Y02T10/7016 , Y02T10/7044 , Y02T10/705 , Y02T10/7083 , Y02T10/72 , Y02T10/7283 , Y02T10/90 , Y02T90/14 , Y02T90/161
摘要： A charge controller for charging a battery of a plug-in vehicle with a plurality of electric power sources includes: a driving route estimation element; an estimated electric power consumption amount calculator; a weather information obtaining element; a sunshine information obtaining element; a solar photovoltaic generation electric power amount calculator; an electric power shortage amount calculator for calculating an electric power shortage amount when the solar photovoltaic generation electric power amount is smaller than an estimated electric power consumption amount; a charge schedule preparation element for preparing a charge schedule, which represents a first charge time for charging the battery with a solar photovoltaic generation system and a second charge time for charging the battery by the electric power shortage amount with another electric power source; and a charge control element for controlling to charge the battery according to the charge schedule.
摘要翻译： 一种用于对具有多个电源的插入式车辆的电池充电的充电控制器，包括：驾驶路线估计元件; 估计电力消耗量计算器; 天气信息获取元件; 阳光信息获取元素; 太阳能发电电力量计算器; 电力不足量计算器，用于当太阳能发电电力量小于估计电力消耗量时计算电力不足量; 用于制备充电时间表的充电时间表准备元件，其表示用太阳能光伏发电系统对电池充电的第一充电时间和用另一个电源通过电力不足量对电池充电的第二充电时间; 以及充电控制元件，用于根据充电时间表控制对电池充电。
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公开(公告)号：US07835855B2
公开(公告)日：2010-11-16
申请号：US11987035
申请日：2007-11-27
申请人： Daisuke Nomura
发明人： Daisuke Nomura
IPC分类号： G01C21/00
CPC分类号： G08G1/096775 , G01C21/3694 , G08G1/096716 , G08G1/09675
摘要： A navigation apparatus acquires weather information along a navigation route to a destination from an information center and calculates an importance that is assigned to the weather information based on a predetermined criterion as well as a determination mode and a travel purpose inputted from a user. The importance of the weather information may be calculated by employing an importance calculation table that defines importance of the weather information itself or the importance of the weather information relative to the navigation route. The importance of the weather information is used to extract a required part of the weather information for providing the user with the information. The weather information extraction may be performed according to a criterion such as extracting the weather information with a certain importance level or higher, extracting the weather information of top n th importance, or the like.
摘要翻译： 导航装置从信息中心获取沿着到目的地的导航路线的天气信息，并且基于预定标准计算分配给天气信息的重要性以及从用户输入的确定模式和旅行目的。 天气信息的重要性可以通过使用定义天气信息本身的重要性的重要性计算表或相对于导航路线的天气信息的重要性来计算。 使用天气信息的重要性来提取用于向用户提供信息的天气信息的所需部分。 天气信息提取可以根据诸如提取具有一定重要程度或更高的天气信息的标准来执行，提取上述第n个重要性的天气信息等。
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