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1. 发明授权

US09490241B2 Semiconductor device comprising a first inverter and a second inverter 有权
标题翻译：半导体器件包括第一反相器和第二反相器
公开(公告)号：US09490241B2
公开(公告)日：2016-11-08
申请号：US13533113
申请日：2012-06-26
申请人： Masumi Nomura , Tatsuji Nishijima , Kosei Noda
发明人： Masumi Nomura , Tatsuji Nishijima , Kosei Noda
IPC分类号： H01L29/10 , H01L27/02 , H01L27/11
CPC分类号： H01L27/0207 , H01L27/1108
摘要： A semiconductor device which is downsized while a short-channel effect is suppressed and whose power consumption is reduced is provided. A downsized SRAM circuit is formed, which includes a first inverter including a first transistor and a second transistor overlapping with each other; a second inverter including a third transistor and a fourth transistor overlapping with each other; a first selection transistor; and a second selection transistor. An output terminal of the first inverter, an input terminal of the second inverter, and one of a source and a drain of the first selection transistor are connected to one another, and an output terminal of the second inverter, an input terminal of the first inverter, and one of a source and a drain of the second selection transistor are connected to one another.
摘要翻译：提供了在抑制短通道效应并且其功耗降低的同时小型化的半导体器件。形成了小型SRAM电路，其包括第一反相器，其包括彼此重叠的第一晶体管和第二晶体管; 第二反相器，包括彼此重叠的第三晶体管和第四晶体管; 第一选择晶体管; 和第二选择晶体管。第一反相器的输出端子，第二反相器的输入端子和第一选择晶体管的源极和漏极之一彼此连接，第二反相器的输出端子，第一反相器的输入端子，第一反相器的输入端子，反相器和第二选择晶体管的源极和漏极之一彼此连接。

2. 发明授权

US08643007B2 Semiconductor device 有权
标题翻译：半导体器件
公开(公告)号：US08643007B2
公开(公告)日：2014-02-04
申请号：US13397838
申请日：2012-02-16
申请人： Masumi Nomura , Kosei Noda
发明人： Masumi Nomura , Kosei Noda
IPC分类号： H01L29/786
CPC分类号： H01L29/7869 , H01L29/42384 , H01L29/78624
摘要： It is an object to reduce concentration of an electric field on an end of a drain electrode of a semiconductor device. A semiconductor device includes an oxide semiconductor film including a first region and a second region; a pair of electrodes which is partly in contact with the oxide semiconductor film; a gate insulating film over the oxide semiconductor film; and a gate electrode that overlaps with part of one of the pair of electrodes and the first region with the gate insulating film provided therebetween. At least part of the first region and part of the second region are between the pair of electrodes. The gate electrode does not overlap with the other of the pair of electrodes.
摘要翻译：本发明的目的是减少半导体器件的漏电极端部的电场浓度。半导体器件包括包括第一区域和第二区域的氧化物半导体膜; 一部分与氧化物半导体膜接触的电极; 氧化物半导体膜上的栅极绝缘膜; 以及栅极电极，其与所述一对电极中的一个电极的一部分和所述第一区域重叠，并且所述栅极绝缘膜设置在所述第一区域之间。第一区域的至少一部分和第二区域的一部分位于该对电极之间。栅极电极不与另一对电极重叠。

3. 发明授权

US06721631B2 Method for remote monitoring of gas turbine 有权
标题翻译：燃气轮机远程监控方法
公开(公告)号：US06721631B2
公开(公告)日：2004-04-13
申请号：US10031329
申请日：2002-01-18
申请人： Yujiro Shimizu , Masumi Nomura , Shigeo Okamoto , Yasuhiko Ikegami , Isao Sagawa , Tsutomu Sakagami , Katsunori Tanaka
发明人： Yujiro Shimizu , Masumi Nomura , Shigeo Okamoto , Yasuhiko Ikegami , Isao Sagawa , Tsutomu Sakagami , Katsunori Tanaka
IPC分类号： G05D1100
CPC分类号： F02C9/00 , F02C9/16 , F02C9/46 , F05D2270/301 , F05D2270/303 , G01H1/006 , G05B23/0291 , H04L29/06 , H04L67/12 , H04L69/329
摘要： The state of combustion oscillation in the combustor of a turbine of a power plant is monitored from a remote monitoring center. To monitor the combustion oscillation state, combustion oscillation data on the combustor is separated into two types of data: the first data obtained on a real-time basis, and the second data including representative values within a predetermined period of time obtained from the first data. In the normal state, a low-speed communications mode is used to send the second data, which is monitored at the monitoring center. If an abnormal state is predicted as a result of monitoring the second data, the high-speed communications mode is used to send the first data, and more detailed combustion oscillation data is monitored at the monitoring center. When a critical state is predicted, an instruction is sent to the local site to switch the operation mode over to the low load operation mode.
摘要翻译：从远程监控中心监测发电厂涡轮机燃烧器内的燃烧振荡状态。为了监视燃烧振荡状态，燃烧器上的燃烧振动数据被分成两种类型的数据：实时获得的第一数据，以及包括从第一数据获得的预定时间段内的代表值的第二数据。在正常状态下，使用低速通信模式发送监视中心监视的第二数据。如果作为监视第二数据的结果预测到异常状态，则使用高速通信模式发送第一数据，并且在监视中心监视更详细的燃烧振荡数据。当预测到临界状态时，将指令发送到本地站点，以将操作模式切换到低负载运行模式。

4. 发明授权

US06672055B1 Hydraulic pump control device 失效
标题翻译：液压泵控制装置
公开(公告)号：US06672055B1
公开(公告)日：2004-01-06
申请号：US09869924
申请日：2001-07-09
申请人： Hideo Konishi , Kenji Arai , Seiichi Akiyama , Masumi Nomura
发明人： Hideo Konishi , Kenji Arai , Seiichi Akiyama , Masumi Nomura
IPC分类号： F16D3102
CPC分类号： E02F9/2292 , E02F9/2235 , E02F9/2296 , F04B49/08 , F04B2201/1203 , F04B2203/0604
摘要： Disclosed herein is a hydraulic-pump controller that is capable of controlling absorbed pump torque in good balance against engine output at all times. In this hydraulic-pump controller, the discharge flow rates of the operating oil that are discharged from hydraulic pumps (9, 10) according to manipulation of manipulation units (12, 13) are predicted based on the discharge pressure of the hydraulic pumps (9, 10) that are driven by an engine (1), and based on the manipulation amount of the manipulation units (12, 13) that manipulate hydraulic actuators (27, 28), or a physical quantity correlating with the manipulation amount. Based on the predicted discharge flow rates and the discharge pressure, the absorbed torque of the hydraulic pumps is computed. Then, the predictive engine speed of the engine (11) is computed from the absorbed torque of the hydraulic pumps (9, 10) computed. Based on the deviation between the computed predictive engine speed and the actual engine speed of the engine (11), the regulators (12, 13) of the hydraulic pumps (9, 10) are controlled.
摘要翻译：本文公开了一种液压泵控制器，其能够始终控制吸收的泵扭矩与发动机输出的良好平衡。在该液压泵控制器中，基于操作单元（12,13）的操作从液压泵（9,10）排出的工作油的排出流量基于液压泵（9）的排出压力，10），并且基于操纵液压致动器（27,28）的操作单元（12,13）的操作量或与操作量相关的物理量。基于预测的排放流量和排放压力，计算出液压泵的吸收扭矩。然后，从计算出的液压泵（9,10）的吸收转矩算出发动机（11）的预测发动机转速。基于计算出的预测发动机速度与发动机（11）的实际发动机转速之间的偏差，控制液压泵（9,10）的调节器（12,13）。

5. 发明授权

US06566440B2 Polytetrafluoroethylene agglomerated product and its molded product 有权
标题翻译：聚四氟乙烯凝聚体及其成型体
公开(公告)号：US06566440B2
公开(公告)日：2003-05-20
申请号：US09987255
申请日：2001-11-14
申请人： Satoru Kuroki , Takamichi Ishikawa , Masumi Nomura , Tadao Chiba
发明人： Satoru Kuroki , Takamichi Ishikawa , Masumi Nomura , Tadao Chiba
IPC分类号： C08J316
CPC分类号： C08K3/04 , C08L27/18 , C08L2205/02 , Y10T428/2982
摘要： A polytetrafluoroethylene agglomerated product obtained from a polytetrafluoroethylene powder and a coke powder, wherein the polytetrafluoroethylene powder contains at least 8.3 mass % of a polytetrafluoroethylene fine powder having a particle diameter of from 0.1 to 9.5 &mgr;m, and the mass ratio of the polytetrafluoroethylene powder/the coke powder is 95-60/5-40.
摘要翻译：由聚四氟乙烯粉末和焦炭粉末得到的聚四氟乙烯凝聚体，其中聚四氟乙烯粉末含有至少8.3质量％的粒径为0.1〜9.5μm的聚四氟乙烯细粉末，聚四氟乙烯粉末/ 焦粉为95-60 / 5-40。

6. 发明授权

US08701420B2 Gas turbine control method and device 有权
标题翻译：燃气轮机控制方法及装置
公开(公告)号：US08701420B2
公开(公告)日：2014-04-22
申请号：US12673932
申请日：2009-02-23
申请人： Masumi Nomura , Kotaro Miyauchi
发明人： Masumi Nomura , Kotaro Miyauchi
IPC分类号： F02C9/52 , F02C9/00
CPC分类号： F02C9/52 , F02C9/28 , F02C9/54 , F05D2270/114 , F05D2270/14 , F05D2270/301 , F05D2270/3061 , F05D2270/332 , F05D2270/334
摘要： A gas turbine control device having a gas turbine control unit for the gas turbine operation control that computes adjustment increments regarding at least one of the airflow rate into the combustor and the pilot ratio, and makes revisions to the actuating variables comprising the airflow rate and the pilot ratio so that the actuating variables are contrasted with the status signals and the variables are modified toward initial design conditions. The gas turbine control unit resets the revisions made to the actuating variables in a case where the level of the combustion vibration is restrained below the predetermined control criterion for a predetermined time span, and the gas turbine is operated under the control settings of the initial design stage.
摘要翻译：一种燃气轮机控制装置，具有用于燃气轮机运行控制的燃气轮机控制单元，该燃气轮机控制单元计算关于进入燃烧器的气流率和导频比中的至少一个的调节增量，并且对包括气流速率和导频比，使得致动变量与状态信号形成对比，并且将变量修改为初始设计条件。燃气轮机控制单元将在燃烧振动的水平被抑制在预定控制标准下达预定时间间隔的情况下复位对致动变量的修正，并且燃气轮机在初始设计的控制设置下操作阶段。

7. 发明授权

US08560205B2 Gas turbine control device and gas turbine system 有权
标题翻译：燃气轮机控制装置和燃气轮机系统
公开(公告)号：US08560205B2
公开(公告)日：2013-10-15
申请号：US12715491
申请日：2010-03-02
申请人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
发明人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
IPC分类号： G06F17/00 , G06F19/00 , G01N9/00 , G01N33/22 , G01L23/00
CPC分类号： F02C9/00 , F02C3/22 , F02C9/28 , F05D2270/083 , F23R2900/00013
摘要： An object of the present invention is to provide a gas turbine control device which is capable of performing correction on the basis of a fuel composition of fuel gas to be supplied to a gas turbine, and is capable of changing an amount of correction in response to variation with time of the gas turbine. To attain this, a frequency analyzing unit 25 performs a frequency analysis of combustion oscillation of a combustor and splits a result of the analysis into respective frequency bands. Then, a state grasping unit 22 checks an operating state of the gas turbine on the basis of the result of the analysis of the combustion oscillation and process value of the gas turbine, and corrects the checked operating state on the basis of a fuel composition or a heat capacity of fuel gas measured by a fuel characteristic measuring unit 200. A countermeasure determining unit 23 conducts a countermeasure for controlling an operating action of the gas turbine on the basis of the operating state thus checked.
摘要翻译：本发明的目的是提供一种燃气轮机控制装置，其能够基于要供给到燃气轮机的燃料气体的燃料成分进行校正，并且能够响应于随着燃气轮机的时间变化。为了实现这一点，频率分析单元25对燃烧器的燃烧振动进行频率分析，并将分析结果分解成各个频带。然后，状态把持部22基于燃气轮机的燃烧振动和过程值的分析结果来检查燃气轮机的运转状态，根据燃料组成或者燃料组成来校正所检查的运转状态，由燃料特性测量单元200测量的燃料气体的热容量。对策确定单元23基于所检查的操作状态，进行用于控制燃气轮机的操作动作的对策。

8. 发明申请

US20100199680A1 GAS TURBINE CONTROL METHOD AND DEVICE 有权
标题翻译：气体涡轮机控制方法和装置
公开(公告)号：US20100199680A1
公开(公告)日：2010-08-12
申请号：US12673932
申请日：2009-02-23
申请人： Masumi Nomura , Kotaro Miyauchi
发明人： Masumi Nomura , Kotaro Miyauchi
IPC分类号： F02C9/50
CPC分类号： F02C9/52 , F02C9/28 , F02C9/54 , F05D2270/114 , F05D2270/14 , F05D2270/301 , F05D2270/3061 , F05D2270/332 , F05D2270/334
摘要： A gas turbine control method for preventing then operation from deviating from the operating state at the ideal fuel and air flow-rates expected when the gas turbine is designed and maintaining an efficient operating state. A gas turbine control device comprises a frequency analyzing means for analyzing the frequencies inside the combustor of a gas turbine, a state grasping means for grasping the combustion state in the gas turbine on the basis of a state signal representing the result of the analysis by frequency band, the amount of operation process including a ratio between the air flow rate and pilot fuel in the gas turbine, the atmosphere state, and the load amount, a combustion characteristic grasping means for grasping the characteristic of the combustion vibration, and a control section for calculating a correction value of at least either the air flow rate supplied to the combustor or the pilot ratio from the grasped combustion vibration characteristic and the grasped combustion state each time the degree of the combustion vibration exceeds a predetermined control value, correcting the initial design values of the air flow rate and the pilot ratio predetermined correspondingly to the amount of operation process and the state signal, and thereby driving the gas turbine. The control section resets the correction of the initial design values when the degree of combustion vibration of the gas turbine is below the predetermined control value for a given period of time and operates the gas turbine using the initial design values.
摘要翻译：一种燃气轮机控制方法，用于防止在设计燃气涡轮机时期望的理想燃料和空气流速下操作偏离操作状态并保持有效的操作状态。燃气轮机控制装置包括：频率分析装置，用于分析燃气轮机的燃烧器内部的频率;状态把持装置，用于根据表示分析结果的状态信号按照频率来获取燃气轮机中的燃烧状态包括燃气轮机中的空气流量与先导燃料之间的比例，气氛状态和负载量的运转处理量，用于掌握燃烧振动特性的燃烧特性获取装置，以及控制部每当燃烧振动的程度超过预定的控制值时，根据所掌握的燃烧振动特性和所掌握的燃烧状态来计算至少提供给燃烧器的空气流量或者先导比的校正值，校正初始设计对应于操作量的空气流量和导频比的值从而驱动燃气轮机。当燃气轮机的燃烧振动程度低于预定控制值一段给定的时间段时，控制部分复位初始设计值的校正，并且使用初始设计值来操作燃气轮机。

9. 发明申请

US20090125207A1 GAS TURBINE CONTROL DEVICE AND GAS TURBINE SYSTEM 有权
标题翻译：气体涡轮控制装置和气体涡轮机系统
公开(公告)号：US20090125207A1
公开(公告)日：2009-05-14
申请号：US11993915
申请日：2006-03-29
申请人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
发明人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
IPC分类号： F02C9/00
CPC分类号： F02C9/00 , F02C3/22 , F02C9/28 , F05D2270/083 , F23R2900/00013
摘要： An object of the present invention is to provide a gas turbine control device which is capable of performing correction on the basis of a fuel composition of fuel gas to be supplied to a gas turbine, and is capable of changing an amount of correction in response to variation with time of the gas turbine. To attain this, a frequency analyzing unit 25 performs a frequency analysis of combustion oscillation of a combustor and splits a result of the analysis into respective frequency bands. Then, a state grasping unit 22 checks an operating state of the gas turbine on the basis of the result of the analysis of the combustion oscillation and process value of the gas turbine, and corrects the checked operating state on the basis of a fuel composition or a heat capacity of fuel gas measured by a fuel characteristic measuring unit 200. A countermeasure determining unit 23 conducts a countermeasure for controlling an operating action of the gas turbine on the basis of the operating state thus checked.
摘要翻译：本发明的目的是提供一种燃气轮机控制装置，其能够基于要供给到燃气轮机的燃料气体的燃料成分进行校正，并且能够响应于随着燃气轮机的时间变化。为了实现这一点，频率分析单元25对燃烧器的燃烧振动进行频率分析，并将分析结果分解成各个频带。然后，状态把持部22基于燃气轮机的燃烧振动和过程值的分析结果来检查燃气轮机的运转状态，根据燃料组成或者燃料组成来校正所检查的运转状态，由燃料特性测量单元200测量的燃料气体的热容量。对策确定单元23基于所检查的操作状态，进行用于控制燃气轮机的操作动作的对策。

10. 发明授权

US07188019B2 Gas turbine control apparatus, gas turbine system and gas turbine control method 有权
标题翻译：燃气轮机控制装置，燃气轮机系统和燃气轮机控制方法
公开(公告)号：US07188019B2
公开(公告)日：2007-03-06
申请号：US10929927
申请日：2004-08-31
申请人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
发明人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
IPC分类号： F02C9/00 , G01C19/00
CPC分类号： F02C9/28 , F05D2270/083 , F05D2270/301
摘要： A gas turbine control apparatus, etc. are provided by which combustion fluctuation, even if arising in plural frequency bands, can be effectively suppressed. If the combustion fluctuation arises in plural frequency bands, corresponding to a predetermined priority order, adjustment is done so that the combustion fluctuation of the frequency band of a high priority order is suppressed. If the gas turbine state changes after the adjustment, this is reflected on a data base 30. If no sufficient data is stored yet in the data base 30 for any the reason, such as immediately after installation of the gas turbine, correction is made using data of countermeasures based on data of another same type gas turbine contained in a basic data base 31 and data of countermeasures based on experiences of skilled adjusting operators contained in a knowledge data base 32. Also, in a stabilized operation, operation condition may be varied so that an optimal operation condition is automatically searched.
摘要翻译：提供了一种燃气轮机控制装置等，即使能够有效地抑制多个频带中产生的燃烧波动。如果根据预定的优先级顺序在多个频带中出现燃烧波动，则进行调整，使得抑制了高优先级顺序的频带的燃烧波动。如果燃气轮机状态在调整之后改变，则这反映在数据库30上。如果由于任何原因（例如在安装燃气轮机之后立即安装）而在数据库30中没有足够的数据存储，则使用基于数据库31中的另一相同类型的燃气轮机的数据的对策的数据进行校正以及基于包含在知识数据库32中的熟练调整运算符的经验的对策数据。此外，在稳定化的动作中，可以改变操作条件，从而自动搜索最佳操作条件。

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