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51. 发明专利

JP2009197831A Sphere levitation device 有权
标题翻译：球形钻石装置
公开(公告)号：JP2009197831A
公开(公告)日：2009-09-03
申请号：JP2008037557
申请日：2008-02-19
申请人： Japan Aerospace Exploration Agency , Ono Denki Seisakusho:Kk , 株式会社小野電機製作所 , 独立行政法人宇宙航空研究開発機構
发明人： TSUDA YUICHI , SHIRASAWA YOJI , TSUCHIYA TOSHIO
IPC分类号： F16C32/06
摘要： PROBLEM TO BE SOLVED: To provide a design method and a mechanism of a sphere levitation device for implementing a sphere levitation by an infinitesimal differential pressure and a minute flow rate compared with a conventional sphere levitation device.
SOLUTION: The design method for "discoid slot throttle thrust bearing" used in a conventional flat gas bearing is expanded for a spherical bearing. It is known that a slot throttle having a cylindrical shape in the air supply throttle is operated by an infinitesimal differential pressure and a minute flow rate. Mathematical expression expansion and physical formulation are performed to expand the bearing type for the spherical bearing, so as to obtain a method for quantatively determining a main parameter which is important for design. In order to implement the infinitesimal differential pressure or minute flow rate, it is necessary to control the width of an air injection groove in the slot throttle with higher precision. For this purpose, the design and processing method are obtained with sufficient precision in the spherical thrust bearing.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种球形悬浮装置的设计方法和机构，用于与常规的球悬浮装置相比，通过无穷小的压差和微小的流速实现球悬浮。
解决方案：在常规扁平气体轴承中使用的“盘状节流阀推力轴承”的设计方法为球面轴承而扩展。已知在空气供给节流阀中具有圆筒形状的槽口节流阀由无穷小的压差和微小的流量运行。进行数学表达扩展和物理配方以扩大球面轴承的轴承类型，以获得对设计重要的主要参数进行定量确定的方法。为了实现无穷小的压差或微小的流量，需要以更高的精度控制狭槽节流阀中的空气注入槽的宽度。为此，在球面止推轴承中获得足够的精度的设计和加工方法。版权所有（C）2009，JPO＆INPIT

52. 发明专利

JP2009068359A Performance estimation system of gas turbine engine 有权
标题翻译：气体涡轮发动机性能评估系统
公开(公告)号：JP2009068359A
公开(公告)日：2009-04-02
申请号：JP2007234912
申请日：2007-09-11
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： TAGASHIRA TAKESHI , SUGIYAMA SHICHIKEI , MIZUNO TAKUYA , KO MASAHARU
IPC分类号： F02C9/00 , F01D25/00 , F02C7/00
摘要： PROBLEM TO BE SOLVED: To provide a performance estimation system of a gas turbine engine incorporable in a controller of the engine, estimating immeasurable items from measurable items online and in real time and fulfilling proper engine control using the estimation result. SOLUTION: The performance estimation system uses a constant gain extended Kalman filter (CGEKF) comprised of a Kalman filter gain K designed to be optimum at an operation point of the engine and a nonlinear dynamic simulation model modeled faithfully after the actual engine. When a difference is caused between an observed variable and an observed variable estimation value, a turning parameter forming a part of a state variable of the model is adjusted to minimize the difference, so that the nonlinear dynamic simulation model is always made to be the model faithful to the actual engine. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供可并入发动机的控制器中的燃气涡轮发动机的性能估计系统，在线和实时地估计不可衡量的物品，并使用估计结果实现适当的发动机控制。解决方案：性能估计系统使用由发动机工作点设计为最佳的卡尔曼滤波器增益K组成的恒定增益扩展卡尔曼滤波器（CGEKF），以及在实际发动机之后忠实建模的非线性动态仿真模型。当在观测变量和观测到的可变估计值之间产生差异时，调整形成模型的状态变量的一部分的转弯参数以最小化差异，使得非线性动态模拟模型总是作为模型忠实于实际发动机。版权所有（C）2009，JPO＆INPIT

53. 发明专利

JP2009023628A Stol aircraft 有权
标题翻译： STOL飞机
公开(公告)号：JP2009023628A
公开(公告)日：2009-02-05
申请号：JP2007191772
申请日：2007-07-24
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： KOBAYASHI CHU , NISHIZAWA HIROSHI
IPC分类号： B64C25/34
摘要： PROBLEM TO BE SOLVED: To provide a short take-off and landing (STOL) aircraft capable of takeoff running in a short distance using a combination of the propulsion of drive wheels and the propulsion of a propulsion unit, and of landing running in a short distance using a driving force of the drive wheels.
SOLUTION: A movable gear 13 is disposed as a fourth gear behind the center of gravity of an airframe and behind left and right main gears 21, 31. Note that the movable gear 13 is configured such that the distance to ground can be changed arbitrarily. The aircraft performs takeoff running using the combination of the propulsion of left and right engines 24, 34 on the airframe and the driving propulsion of the left and right drive wheels 22, 23. If the airframe starts pitching up, a torque control system 200 controls the torques of left and right motors 23, 33 separately and independently.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够在短距离内起飞的短距离起飞和降落（STOL）飞机，其结合驱动轮的推进和推进单元的推进，以及着陆运行在较短距离内使用驱动轮的驱动力。解决方案：可动齿轮13作为机身重心后方的第四齿轮设置在左右主齿轮21和31的后面。注意，可动齿轮13构造成使得到地面的距离可以任意改变飞机使用机身上的左右发动机24,34的推进和左右驱动轮22,23的驱动推进的组合来执行起飞运行。如果机身开始俯仰，则转矩控制系统200控制左右电机23,33的转矩分开独立。版权所有（C）2009，JPO＆INPIT

54. 发明专利

JP2008302830A Traveling mechanism provided with rocker crawler 有权
标题翻译：提供摇摆机的旅行机构
公开(公告)号：JP2008302830A
公开(公告)日：2008-12-18
申请号：JP2007152484
申请日：2007-06-08
申请人： Japan Aerospace Exploration Agency , Shimizu Corp , 清水建設株式会社 , 独立行政法人宇宙航空研究開発機構
发明人： WAKABAYASHI SACHIKO , NISHIDA SHINICHIRO , SATO HITOSHI
IPC分类号： B62D55/116 , B25J5/00
摘要： PROBLEM TO BE SOLVED: To provide an energy-saving travel mechanism by means of a suspension method, or a simple and highly reliable suspension mechanism, capable of both avoiding getting stuck and traveling through rocky ups and downs on a sandy ground or the like with extremely small tolerable support force, while reducing drive components by utilizing passive mechanisms.
SOLUTION: The travel mechanism with rocker crawlers is provided with front and rear right and left crawlers 1, 2, 3, and 4. The front and the rear crawlers are coupled with each other by a rocker 5 through free joints 8, and the right and the left lockers 5 and 6 are rotatably connected to each other through a vehicle main body to form a rocker bogie suspension.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：通过悬挂方法或简单高度可靠的悬挂机构来提供节能旅行机构，能够避免卡住并在沙地上经历岩石上下颠簸行驶，具有非常小的可承受的支撑力，同时通过利用被动机构来减少驱动部件。解决方案：具有摇臂履带的行走机构设置有前后左右履带1,2,3和4.前履带和后履带通过自由接头8的摇杆5彼此联接，左右的储物柜5和6通过车辆本体可旋转地连接以形成摇臂转向架悬架。版权所有（C）2009，JPO＆INPIT

55. 发明专利

JP2008286564A Compound molecular sensor 有权
标题翻译：化合物分子传感器
公开(公告)号：JP2008286564A
公开(公告)日：2008-11-27
申请号：JP2007129965
申请日：2007-05-16
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： MITSUO KAZUNORI
IPC分类号： G01K11/12 , G01N21/64
摘要： PROBLEM TO BE SOLVED: To provide a compound molecular sensor having high performance capable of accurately correcting temperature measurement errors included in emission data of a pressure-sensitive pigment in the compound molecular sensor composed by mixing a temperature-sensitive pigment and the pressure-sensitive pigment.
SOLUTION: The compound molecular sensor including: an Eu four-kernel complex compound 100 having a structure formula [Eu
4 (μ-0)(L
1 )
10 ] (L
1 =2-hydroxy-4-octyloxybenzophenone) as the temperature-sensitive pigment; and a polphyrin compound as the pressure-sensitive pigment is regarded as a compound pressure-sensitive paint by using fluorine polymer as a binder and toluene as a solvent. The compound pressure-sensitive paint is applied on a model to successively expose excitation illumination so as to measure a light emitting image by a CCD camera. Then, in order to measure two-color emission, the two CCD cameras are used or the two-color emission is alternately measured by mounting a flywheel capable of switching an optical filter on the front face of the CCD camera.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种具有高性能的复合分子传感器，其能够精确地校正由混合感温颜料组成的复合分子传感器中的压敏颜料的发射数据中包含的温度测量误差，并且压力敏感色素。解决方案：所述复合分子传感器包括：具有结构式[Eu 4 （μ-0）（L 1 ）的Eu四核络合物100 SB> 10 ]（L 1 = 2-羟基-4-辛氧基二苯甲酮）作为感温颜料; 通过使用氟聚合物作为粘合剂，将甲苯作为溶剂，将作为压敏颜料的卟啉化合物视为复合压敏涂料。将复合压敏涂料施加在模型上以连续曝光激发照明，以便通过CCD照相机测量发光图像。然后，为了测量双色发射，使用两个CCD照相机，或者通过在CCD照相机的正面安装能够切换滤光器的飞轮来交替测量双色发射。版权所有（C）2009，JPO＆INPIT

56. 发明专利

JP2008282218A Disaster rescue support system and disaster rescue support method 审中-公开
标题翻译：灾难救援支援系统和灾难救援支援方法
公开(公告)号：JP2008282218A
公开(公告)日：2008-11-20
申请号：JP2007125807
申请日：2007-05-10
申请人： Japan Aerospace Exploration Agency , Mitsubishi Space Software Kk , 三菱スペース・ソフトウエア株式会社 , 独立行政法人宇宙航空研究開発機構
发明人： FUKANOGI HIROKAZU , SUGIMOTO YOSHIO
IPC分类号： G06Q10/00 , G06Q50/00 , G06Q50/10 , G06Q50/22 , G06Q50/26 , G08B25/00 , G08B25/04
摘要： PROBLEM TO BE SOLVED: To rescue as many injured or sick persons as possible by transmitting triage information of each injured or sick person to a server at disaster medical care and rescue headquarters 110 promptly, which controls each hospital appropriately based on the collected triage information. SOLUTION: A triage tag 600 with a built-in IC to which an IC tag is added is allocated to each injured or sick person at a first-aid station 130 when a disaster strikes. A health worker writes triage information in the triage tag 600 with a built-in IC and records the information in the IC tag using a triage information terminal 200. The triage information terminal 200 transmits the triage information recorded in the IC tag to a server 400 for the rescue headquarters through a satellite communication terminal 300 and a communication satellite 120. The server 400 for the rescue headquarters transmits rescue instruction information inputted by personnel based on the collected triage information to the first-aid station 130 and disaster key hospitals 131. The first-aid station 130 and disaster key hospitals 131 treat each injured or sick person according to the rescue instruction. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：尽快通过将受伤或病人的分诊信息传送到灾区医疗救护总部110的服务器，尽快拯救受伤害人员，并根据收集的情况适当控制各医院分诊资料。解决方案：当灾难发生时，在急救站130处向每个受伤或患病的人分配具有添加有IC标签的内置IC的分类标签600。卫生工作人员使用内置IC在分类标签600中写入分类信息，并使用分类信息终端200将信息记录在IC标签中。分类信息终端200将记录在IC标签中的分类信息发送到服务器400 用于通过卫星通信终端300和通信卫星120的救援总部。救援总部的服务器400将收集到的分类信息的人员输入的救援指示信息发送到急救站130和灾难关键医院131。急救站130和灾区重点医院131按照拯救指示对待受伤者或病人。版权所有（C）2009，JPO＆INPIT

57. 发明专利

JP2008281505A Method of resampling 3-dimensional discrete data, and its device 审中-公开
标题翻译：重建三维离散数据的方法及其设备
公开(公告)号：JP2008281505A
公开(公告)日：2008-11-20
申请号：JP2007127716
申请日：2007-05-14
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： TAKANO TADASHI , MAEDA TAKASHI
IPC分类号： G01C7/04 , G01B21/20 , G01C5/00 , G06T3/00
CPC分类号： G06T3/0031 , B64G1/1021 , G01S13/955 , G01W1/08 , Y02A90/18
摘要： PROBLEM TO BE SOLVED: To easily estimate the fine variation of physical quantity data near a sampling point of a sensor. SOLUTION: A method is used for selecting six points in nine sampling points surrounding the point of (x, y) = (X, Y) and estimating the value on Z axis of any point in the six triangles obtained from the (X, Y) point and the six points. In the method, two points on substantially diagonal line on a rectangle partitioned by the outermost periphery of the nine points are selected, and the six triangles are formed by the six points other than the two points. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：为了容易地估计传感器采样点附近的物理量数据的微小变化。解决方案：一种方法用于在（x，y）=（X，Y）点周围的九个采样点中选择六个点，并估计从（（x，y）=（X，Y））点获得的六个三角形中任何点的Z轴上的值 X，Y）点和六点。在该方法中，选择由九个点的最外周划分的矩形上的基本上对角线上的两个点，并且六个三角形由除了两个点之外的六个点形成。版权所有（C）2009，JPO＆INPIT

58. 发明专利

JP2008265522A Heat control device 审中-公开
标题翻译：热控制装置
公开(公告)号：JP2008265522A
公开(公告)日：2008-11-06
申请号：JP2007111144
申请日：2007-04-20
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： ONISHI AKIRA , NAGANO HOSEI
IPC分类号： B64G1/50 , F25B49/02 , F28D15/02
CPC分类号： B64G1/506 , F28F13/00 , F28F2013/005
摘要： PROBLEM TO BE SOLVED: To provide a new heat control device of lightweight and simple structure to be properly used for a spaceship and in the environment on the earth wherein a temperature difference is large.
SOLUTION: The heat control device includes a base plate connected to a thermally controlled object freely to exchange the heat, one or more heat exchange paddles fitted to the base plate freely to be expanded and housed, a paddle driving means provided in an end of the base plate to drive expanding operation and housing operation of the heat exchange paddles and to change angle of expansion thereof, and a heat transport element provided to connect the base plate to the heat exchange paddles. A first surface of the base plate on the opposite side to the thermally controlled object, a second surface thereof as the surface side of the paddle, and a third surface thereof as the back side of the heat exchange paddle are formed into any one of a heat radiating surface, a heat absorbing surface, a heat insulating surface and an emissivity changing surface, and angle of expansion of the heat exchange paddles can be changed.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种重量轻且结构简单的新的热控制装置，其适用于宇宙飞船和地球上的温度差大的环境中。解决方案：热控制装置包括一个与受热物体自由连接以交换热量的基板，一个或多个安装在该基板上的热交换器板自由地膨胀和收纳;桨驱动装置，以驱动热交换叶片的膨胀操作和容纳操作并改变其膨胀角;以及传热元件，其将基板连接到热交换叶片。基板的与热控制物体相反一侧的第一表面，作为桨的表面侧的第二表面和作为热交换板的后侧的第三表面形成为散热面，吸热面，隔热面和发射率变化面，热交换叶片的膨胀角度可以变化。版权所有（C）2009，JPO＆INPIT

59. 发明专利

JP2008255429A Means for uniformalizing electrochemical etching 有权
标题翻译：用于均匀化电化学蚀刻的手段
公开(公告)号：JP2008255429A
公开(公告)日：2008-10-23
申请号：JP2007099612
申请日：2007-04-05
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： SAITO TOSHIHITO , ONO FUMIE , TAKEKOSHI MASAO , UEDA SHUICHI
IPC分类号： C25F7/00 , C25F3/08 , F02K7/14
摘要： PROBLEM TO BE SOLVED: To provide a method by which etching with excellent working accuracy as a whole can be applied by solving a failure where a peripheral part is etched more rapidly than a center part when the whole large surface or a groove structure with a certain pitch is etched.
SOLUTION: The method of uniformalizing the electrochemical etching is carried out by arranging a block of an insulating body on the outermost part of the part-to-be-worked surface of a panel in the electrochemical etching of a hole on the surface of the panel by applying voltage between the panel used as an anode and a cathode of a counter electrode in an aqueous solution tank.
COPYRIGHT: (C)2009,JPO&INPIT

60. 发明专利

JP2008219964A Power storage module 有权
标题翻译：电源存储模块
公开(公告)号：JP2008219964A
公开(公告)日：2008-09-18
申请号：JP2007049692
申请日：2007-02-28
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 , TOYODA HIROYUKI , SONE MICHITSUGU
IPC分类号： H02J7/00 , H01G9/26 , H01G11/10 , H01M10/44 , H02J7/02
CPC分类号： Y02E60/12
摘要： PROBLEM TO BE SOLVED: To equalize voltages of power storage cells and/or a group of power storage cells connected in series and parallel.
SOLUTION: Three serial circuits composed of a plurality of cells such as B1A-B2A, B1B-B2B and B2C-B3C are connected in parallel via semiconductor switches Sa1-Sa6 and Sb1-Sb6. The semiconductor switches Sa1-Sa6 and Sb1-Sb6 are alternately turned on using a driver composed of an oscillation circuit. Thus, no cell is opened from the circuits in any connection state, and while maintaining the same synthesized capacity of each of parallel circuits in the module, charging/discharging is executed between cells to be connected in parallel to equalize the voltage of each of the cells.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了均衡串联和并联连接的蓄电单元和/或一组蓄电单元的电压。解决方案：通过半导体开关Sa1-Sa6和Sb1-Sb6并联连接由诸如B1A-B2A，B1B-B2B和B2C-B3C的多个单元组成的三个串行电路。半导体开关Sa1-Sa6和Sb1-Sb6由使用由振荡电路构成的驱动器交替地导通。因此，在任何连接状态下，没有电池从电路断开，并且在保持模块中的每个并联电路的相同合成容量的同时，在要并联的单元之间执行充电/放电以均衡每个细胞。版权所有（C）2008，JPO＆INPIT

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