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21. 发明专利

JP2013050416A Road surface friction coefficient measurement device 审中-公开
标题翻译：道路表面摩擦系数测量装置
公开(公告)号：JP2013050416A
公开(公告)日：2013-03-14
申请号：JP2011189451
申请日：2011-08-31
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： KANDA ATSUSHI , IGAWA HIROTAKA
IPC分类号： G01N19/02
摘要： PROBLEM TO BE SOLVED: To provide a road surface friction coefficient measurement device which has a small and inexpensive configuration and is capable of accurately controlling a slip ratio while varying it in a wide range and accurately measuring a state of a road surface friction coefficient which varies depending on the slip ratio.SOLUTION: The road surface friction coefficient measurement device 100 includes driving means for rotationally driving a test wheel 120 whose outer circumference surface comes into contact with the road surface; and control means 180 which measures the friction coefficient between the test wheel 120 and the road surface. The test wheel 120, the driving means, and the control means 180 are supported by a dolly 110 that has a travelling wheel 130 and travels by towing or driving. The control means 180 optionally sets the slip ratio between the outer circumference surface of the test wheel 120 and the road surface.
摘要翻译：要解决的问题：提供一种路面摩擦系数测量装置，其具有小且便宜的构造，并且能够在宽范围内改变滑动率并且精确地测量路面摩擦的状态系数根据滑移率而变化。解决方案：路面摩擦系数测量装置100包括用于旋转地驱动其外周表面与路面接触的测试轮120的驱动装置; 以及控制装置180，其测量试验轮120和路面之间的摩擦系数。测试轮120，驱动装置和控制装置180由具有行进轮130并通过牵引或驾驶行进的台车110支撑。控制装置180可选地设定试验轮120的外周面与路面之间的滑移率。版权所有（C）2013，JPO＆INPIT

22. 发明专利

JP2012221206A Data collection system through satellite 有权
标题翻译：数据采集系统通过卫星
公开(公告)号：JP2012221206A
公开(公告)日：2012-11-12
申请号：JP2011086005
申请日：2011-04-08
申请人： Nec Corp , Nec Toshiba Space Systems Ltd , Japan Aerospace Exploration Agency , Nec東芝スペースシステム株式会社 , 日本電気株式会社 , 独立行政法人宇宙航空研究開発機構
发明人： KOISHI YOICHI , TSUKAJIMA TAKASHI , TSUJIHATA AKIO
IPC分类号： G06Q50/10 , B64G1/66 , G01S19/14
摘要： PROBLEM TO BE SOLVED: To provide a system capable of speedily and reliably collecting data through a satellite by a transmission signal from a sensor with a function of a compact terminal which has a reduced size and weight comparable to a portable telephone with a GPS.SOLUTION: A system enables observation data from various environment observation sensors 11 positioned on the sea or in a mountain to be effectively collected through a satellite 12 having a large-sized reflector antenna 13 excellent in reception performance. The environmental observation sensor 11 has a size as well as a transmitting/receiving function equal to a portable terminal with a GPS in addition to a predetermined environment data observation function and can obtain environment observation data as data corresponding to positional information on a position where the environment observation sensor is stationed.
摘要翻译：要解决的问题：提供一种能够通过来自具有小型终端的功能的传感器的传输信号，通过卫星快速可靠地收集数据的系统，其具有与具有相同的便携式电话相当的尺寸和重量的小型终端的功能全球定位系统。解决方案：系统使得位于海上或山上的各种环境观测传感器11的观测数据能够通过具有良好接收性能的大尺寸反射天线13的卫星12被有效地收集。除了预定的环境数据观察功能之外，环境观测传感器11还具有与具有GPS的便携式终端相同的发送/接收功能，并且可以获得环境观测数据作为与位置信息对应的数据环境观测传感器驻扎。版权所有（C）2013，JPO＆INPIT

23. 发明专利

JP2012189010A Nozzle for liquid rocket engine 有权
标题翻译：液体发动机喷嘴
公开(公告)号：JP2012189010A
公开(公告)日：2012-10-04
申请号：JP2011053802
申请日：2011-03-11
申请人： Ihi Aerospace Co Ltd , Japan Aerospace Exploration Agency , 株式会社Ihiエアロスペース , 独立行政法人宇宙航空研究開発機構
发明人： ISHII MASAHIRO , TATE ISAO , TORII YOSHIHIRO
IPC分类号： F02K9/64 , F02K9/48 , F02K9/97
摘要： PROBLEM TO BE SOLVED: To solve such a problem that, in a conventional nozzle for a liquid rocket engine, the man-hour or cost of manufacturing is high for a nozzle requiring regeneration cooling or a nozzle using a heat-resistant metal such as columbium.SOLUTION: A nozzle N for a liquid rocket engine includes an annular manifold 1 on a circumference downstream from a throat T, the manifold making a cooling fluid introduced from the outside of the nozzle flow out along the nozzle inner face. By making the cooling fluid flow out of the annular manifold 1 along the nozzle inner face, film-cooling is carried out by the cooling fluid to maintain a sufficient heat-resistant function, and moreover, reduction in the man-hour of manufacturing or reduction in the cost of manufacturing is achieved.
摘要翻译：要解决的问题为了解决这样的问题，在传统的液体火箭发动机喷嘴中，对于需要再生冷却的喷嘴或使用耐热金属的喷嘴，制造时间或制造成本高如ium。。解决方案：用于液体火箭发动机的喷嘴N包括在喉部T下游的圆周上的环形歧管1，使得从喷嘴外部引入的冷却流体的歧管沿喷嘴内表面流出。通过使冷却流体沿着喷嘴内表面流出环状歧管1，通过冷却流体进行膜冷却，以保持足够的耐热功能，而且减少制造或还原的工时在制造成本上实现。版权所有（C）2013，JPO＆INPIT

24. 发明专利

JP2012186881A One piece voltage equalization circuit of storage cells connected in series 有权
标题翻译：一系列存储电池的一个电压电平均衡电路
公开(公告)号：JP2012186881A
公开(公告)日：2012-09-27
申请号：JP2011046468
申请日：2011-03-03
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： UNO MASATOSHI , KUKITA AKIO
IPC分类号： H02J7/02 , H01M2/10 , H01M10/44 , H01M10/48
CPC分类号： Y02E60/12
摘要： PROBLEM TO BE SOLVED: To provide an equalization circuit which can be configured of one piece (one switch) without using a multi-winding transformer, and is simplified significantly when compared with prior art.SOLUTION: The equalization circuit comprises an input circuit to which the total voltage of storage cells connected in series and subjected to voltage equalization is input, and an output circuit configured to equalize the storage cell voltage by outputting the total voltage while converting to the storage cell of lowest voltage thereby outputting a current preferentially to the storage cell of lowest voltage.
摘要翻译：要解决的问题：提供一种不使用多绕组变压器可以由一体式（一个开关）构成的均衡电路，并且与现有技术相比被大大简化。解决方案：均衡电路包括输入串联连接并进行电压均衡的存储单元的总电压的输入电路，以及输出电路，其被配置为通过在将转换为最低电压的存储单元，从而优选地将电流输出到最低电压的存储单元。版权所有（C）2012，JPO＆INPIT

25. 发明专利

JP2012103050A Method for remote detection of air turbulence, and execution device thereof 有权
标题翻译：远程检测空气湍流的方法及其执行装置
公开(公告)号：JP2012103050A
公开(公告)日：2012-05-31
申请号：JP2010250072
申请日：2010-11-08
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： ASAHARA TAKASHI , INOKUCHI HAMAKI
IPC分类号： G01S17/58
CPC分类号： Y02A90/18 , Y02A90/19
摘要： PROBLEM TO BE SOLVED: To provide a small-size air turbulence remote detection device of energy saving type, even if measuring a long-distance region, capable of measuring a further distance while suppressing deterioration in the measuring reliability, and also improving the measuring accuracy in the short-distance region.SOLUTION: This method for remote detection of air turbulence, or an optical type air turbulence telemetry, according to present invention radiates (transmits) laser light to atmosphere as a transmission signal, receives laser scattering light of the laser light by aerosol in the atmosphere as a receiving signal, and measuring wind velocity of the air flow in the long-distance region based on Doppler shift amount of frequency between the transmission signal and the receiving signal. In the optical type air turbulence telemetry, the wind velocity width is found by curve fitting of the received power spectrum of the scattering light in a range bin to the Gaussian distribution curve, so as to highly accurately detect the air turbulence by the wind velocity width.
摘要翻译：要解决的问题：为了提供节能型小型空气湍流遥测装置，即使测量长距离区域，能够在抑制测量可靠性的劣化的同时测量更远的距离，并且还提高在短距离区域的测量精度。解决方案：根据本发明的用于远程检测空气湍流或光学式空气湍流遥测的方法将大气中的激光照射（发射）为传输信号，通过气溶胶接收激光的激光散射光作为接收信号的气氛，并且基于发送信号和接收信号之间的频率的多普勒偏移量来测量长距离区域中的空气流的风速。在光学型空气湍流遥测中，通过将散射光的接收功率谱在范围仓中与高斯分布曲线拟合，发现风速宽度，以便通过风速宽度高精度地检测空气湍流。版权所有（C）2012，JPO＆INPIT

26. 发明专利

JP2012041504A Silicone adhesive article for cosmic space, and method for using the same 有权
标题翻译：用于空间的硅胶粘合物及其使用方法
公开(公告)号：JP2012041504A
公开(公告)日：2012-03-01
申请号：JP2010186328
申请日：2010-08-23
申请人： Japan Aerospace Exploration Agency , Shin-Etsu Chemical Co Ltd , 信越化学工業株式会社 , 独立行政法人宇宙航空研究開発機構
发明人： YANO SO , AOKI SHUNJI , TAKARADA MITSUHIRO
IPC分类号： C09J183/07 , B64G4/00 , C09J7/02 , C09J11/02 , C09J183/05 , C09J183/06
摘要： PROBLEM TO BE SOLVED: To provide a silicone adhesive article for cosmic space, which has flexibility, adhesiveness and good tack, can be used for pasting and temporarily fixing members used in cosmic space in a spacecraft or the like, particularly can be used as an adhesive member for collecting samples from solid celestial body surfaces such as asteroids and the moon; and to provide a method for using the same.SOLUTION: The silicone adhesive article for cosmic space is obtained by curing a non-solvent addition-type silicone adhesive composition containing the following (A) to (D) components: (A) a polydiorganosiloxane containing an alkenyl group; (B) a condensation reaction product of (a) a polydiorganosiloxane having a hydroxyl group or an alkoxy group at both terminals of the molecular chain and (b) a polyorganosiloxane having an RSiOunit and a SiOunit as essential units, and a HOSiOunit in the molecule; (C1) a polyorganohydrosiloxane having at least three SiH groups in one molecule thereof; (C2) a polydiorganohydrosiloxane having a SiH group at both terminals thereof; and (D) a platinum group metal-based catalyst. Use of the silicone adhesive article can provide an adhesive article capable of withstanding cosmic radiation and temperature cycle in the cosmic environment.
摘要翻译：要解决的问题：为了提供具有柔性，粘合性和良好粘性的用于宇宙空间的硅氧烷粘合剂制品，可以用于在宇宙飞船等中用于宇宙空间的粘贴和临时固定构件，特别是可以用作从固体天体表面如小行星和月亮收集样品的粘合剂; 并提供使用该方法。解决方案：通过固化含有以下（A）至（D）成分的非溶剂加成型硅氧烷粘合剂组合物获得宇宙空间的硅氧烷粘合剂制品：（A）含有烯基的聚二有机硅氧烷; （B）（a）分子链两端具有羟基或烷氧基的聚二有机硅氧烷的缩合反应产物和（b）具有R分子链的两个末端的聚有机硅氧烷， 3 单位为SiO 1/2 单位，以SiO 2 < ，和分子中的HOSiO 3/2 单元; （C1）在其一分子中具有至少三个SiH基团的聚有机氢硅氧烷; （C2）二末端具有SiH基的聚二氢代氢硅氧烷; 和（D）铂族金属类催化剂。使用硅酮粘合剂制品可以提供能够在宇宙环境中承受宇宙辐射和温度循环的粘合剂制品。版权所有（C）2012，JPO＆INPIT

27. 发明专利

JP2011199948A Charger for uniformly charging serially connected cells while controlling pulse width 有权
标题翻译：在控制脉冲宽度时均匀充电的连续电池充电
公开(公告)号：JP2011199948A
公开(公告)日：2011-10-06
申请号：JP2010061137
申请日：2010-03-17
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： UNO MASATOSHI
IPC分类号： H02J7/02 , H01M10/44 , H02J7/04
CPC分类号： Y02E60/12
摘要： PROBLEM TO BE SOLVED: To provide a highly efficient charger which operates using a general pulse power supply without requiring complicated circuit configuration by at least reducing a rush current generated in charging/discharging a capacitor to reduce loss during charging, in the charger using a pulse power supply.SOLUTION: In the charger, diodes and inductors are connected in parallel to serially connected cells, respectively. In addition, an equalizing capacitor is connected to an intermediate point between the diode and inductor so that either of charging/discharging current flowing between the cell and the equalizing capacitor passes through the inductor.
摘要翻译：要解决的问题：提供一种高效率的充电器，其使用通用脉冲电源进行操作，而不需要复杂的电路配置，至少减少了在充电/放电中产生的冲击电流以减少充电期间的损耗，在使用脉冲的充电器中电源。解决方案：在充电器中，二极管和电感分别与串联连接的电池并联连接。此外，均衡电容器连接到二极管和电感器之间的中间点，使得在电池和均衡电容器之间流过的充电/放电电流中的任一个通过电感器。

28. 发明专利

JP2011176937A Solar cell system using partially connected dc-dc converter and control method therefor 审中-公开
标题翻译：使用部分连接的DC-DC转换器的太阳能电池系统及其控制方法
公开(公告)号：JP2011176937A
公开(公告)日：2011-09-08
申请号：JP2010038855
申请日：2010-02-24
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： UNO MASATOSHI , KUKITA AKIO
IPC分类号： H02M3/155 , G05F1/67
CPC分类号： Y02E10/58 , Y02E10/76
摘要： PROBLEM TO BE SOLVED: To provide a power supply system which can reduce switching loss and noise and improve conversion efficiency by lowering the input/output voltage of a DC-DC converter, and an operating state determination method and the like of each power supply comprising such a power supply system.
SOLUTION: The power supply system supplies power from a power supply module including power supplies connected in series. Only some of the power supplies are connected to the input terminal of a DC-DC converter to lower the input/output voltage of the converter. Operating conditions which the operating states of each power supply constituting the power supply system and the converter should meet are determined and the operating state is determined from the operating conditions and operating characteristics.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够通过降低DC-DC转换器的输入/输出电压来降低开关损耗和噪声并提高转换效率的电源系统，以及每个的操作状态确定方法等电源包括这种电源系统。
解决方案：电源系统从包括串联电源的电源模块供电。只有一些电源连接到DC-DC转换器的输入端，以降低转换器的输入/输出电压。确定构成电源系统和变频器的每个电源的工作状态应满足的工作条件，并根据工作条件和工作特性确定工作状态。版权所有（C）2011，JPO＆INPIT

29. 发明专利

JP2011105248A Turbulence restricting control algorithm 有权
标题翻译：湍流限制控制算法
公开(公告)号：JP2011105248A
公开(公告)日：2011-06-02
申请号：JP2009264792
申请日：2009-11-20
申请人： Iwate Univ , Japan Aerospace Exploration Agency , 国立大学法人岩手大学 , 独立行政法人宇宙航空研究開発機構
发明人： SATO MASAYUKI , YOKOYAMA NOBUHIRO , SATO ATSUSHI
IPC分类号： B64C13/16
摘要： PROBLEM TO BE SOLVED: To develop and provide an algorithm capable of restricting influences of turbulence encountered to the minimum even in a case wherein an observation error of a predefined turbulence, an observation error of a moving condition of one's own machine, and the uncertainty of a system influence each other in the worst way by considering all of the influences of these errors and uncertainty in order to perform the turbulence restricting control considering the observation error of the predefined turbulence, the observation error of the moving condition of the own machine, and uncertainty of the system.
SOLUTION: A delay system having uncertain wasted time in a control input terminal is used to secure the robust performance relative to a modeling error of a system, and information about predefined turbulence using a previously estimated error width is used to secure the robust performance relative to the observation error of the information about predefined turbulence, and further, the control estimating a machine body moving condition using the previously estimated error width is performed to secure the robust performance relative to the observation error of the moving condition of the own machine.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：为了开发和提供一种能够限制遇到的湍流的影响的算法，即使在预定湍流的观察误差，自身机器的移动状态的观察误差和考虑到预定湍流的观测误差，本身的运动状态的观测误差，系统的不确定性通过考虑这些误差和不确定性的所有影响来相互影响，以便执行湍流限制控制机器和系统的不确定性。解决方案：在控制输入端子中具有不确定的浪费时间的延迟系统用于确保相对于系统的建模误差的鲁棒性能，并且使用先前估计的误差宽度的关于预定义湍流的信息用于保护鲁棒性执行相对于关于预定湍流的信息的观察误差的性能，此外，执行使用先前估计的误差宽度来估计机体移动条件的控制，以确保相对于本机的移动状态的观察误差的鲁棒性能。版权所有（C）2011，JPO＆INPIT

30. 发明专利

JP2011055649A Energy storage device with balancing circuit 有权
标题翻译：具有平衡电路的能源存储器件
公开(公告)号：JP2011055649A
公开(公告)日：2011-03-17
申请号：JP2009202684
申请日：2009-09-02
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： UNO MASATOSHI , KUKITA AKIO , ITO KAZUSHIGE , SEKIDO KIN
IPC分类号： H02J7/02 , H01M10/44 , H02J7/00
CPC分类号： H01M10/44 , H02J7/0016 , H02J7/0019 , H02J7/345
摘要： PROBLEM TO BE SOLVED: To provide an energy storage system which uniformly uses an energy storage bank in its charging and discharging and which suppresses fluctuation of input voltages from a charger or output voltages to a load to be within an arbitrary range with the energy storage bank uniformly used in its charging and discharging.
SOLUTION: The energy storage system includes: an energy storage module; a charger; a balancing circuit; a voltage detection unit; a plurality of taps led through switches from one terminal of the energy storage module and/or from the other terminal of the energy storage module and/or from one or more series connection points of a plurality of energy storage units; and a switch control unit changing the switches to connect one of the taps to one terminal or the other terminal of the charger. The switches are sequentially changed to control the number of the energy storage units which are directly charged from the charger based on the detection results of the voltage detection unit in accordance with progress of charging.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：为了提供一种在其充放电中均匀地使用能量储存库的能量存储系统，并且其抑制来自充电器的输入电压的波动或者将负载的输出电压输出到任意范围内，储能库在充放电中均匀使用。解决方案：能量存储系统包括：储能模块; 充电器平衡电路; 电压检测单元; 从能量存储模块的一个端子和/或来自能量存储模块的另一个端子和/或从多个能量存储单元的一个或多个串联连接点通过开关的多个抽头; 以及开关控制单元，其改变开关以将一个抽头连接到充电器的一个端子或另一个端子。根据充电进度，根据电压检测单元的检测结果，依次改变开关以控制从充电器直接充电的储能单元的数量。版权所有（C）2011，JPO＆INPIT

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