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1. 发明专利

JP2014222973A 熱伝導性耐熱絶縁材充填コイル、その製造方法、モータ、及びトランス有权
标题翻译：带有导热耐热绝缘材料的线圈，其制造方法，电动机和变压器
公开(公告)号：JP2014222973A
公开(公告)日：2014-11-27
申请号：JP2013101644
申请日：2013-05-13
申请人：日本化薬株式会社 , Nippon Kayaku Co Ltd , 独立行政法人宇宙航空研究開発機構 , Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： UCHIDA MAKOTO , AKATSUKA YASUMASA , MOGI SHIGERU , MIZUTANI TAKESHI , KOBAYASHI CHU , SHIMIZU TAKAO , ARAI KAZUO
IPC分类号： H02K3/30
摘要：【課題】絶縁性及び耐熱性を確保しつつ、通電に伴う温度上昇を抑制することができる熱伝導性耐熱絶縁材充填コイル、その製造方法、並びにこの熱伝導性耐熱絶縁材充填コイルを用いたモータ及びトランスを提供する。【解決手段】本発明に係る熱伝導性耐熱絶縁材充填コイルは、鉄心と、上記鉄心に巻かれた巻線と、上記鉄心と上記巻線との間及び/又は上記巻線同士の間に充填された熱伝導性耐熱絶縁材とを備える熱伝導性耐熱絶縁材充填コイルであって、上記熱伝導性耐熱絶縁材は、フェノール性水酸基含有ポリアミド樹脂(A)、エポキシ樹脂(B)、及び熱伝導率20W/m・K以上の無機フィラー(C)を含有する熱硬化性樹脂組成物の硬化物からなる。【選択図】図1
摘要翻译：要解决的问题：提供：一种填充有导热耐热绝缘材料的线圈，其能够在确保绝缘性能和耐热性的同时，抑制与通电相关的温度升高及其制造方法; 以及电动机和变压器，其包括填充有导热耐热绝缘材料的线圈。解决方案：根据本发明的填充有导热耐热绝缘材料的线圈包括：铁芯; 缠绕在铁芯上的绕组; 以及填充在铁芯和绕组之间和/或在相互绕组之间的导热耐热绝缘材料。导热性耐热绝缘材料包含含有含酚羟基的聚酰胺树脂（A）的热固性树脂组合物的固化物; 环氧树脂（B）; 以及导热率为20W / m·K以上的无机填料（C）。

2. 发明专利

JP2014172435A Motor-driven propulsion controller 有权
标题翻译：电机驱动控制器
公开(公告)号：JP2014172435A
公开(公告)日：2014-09-22
申请号：JP2013044244
申请日：2013-03-06
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： B64D31/06 , B64D27/24
CPC分类号： B64D31/06 , B64D27/24 , H02P23/00 , Y02T50/62
摘要： PROBLEM TO BE SOLVED: To provide a motor-driven propulsion controller capable of suppressing affection applied to weight or cost by only electrical means, capable of detecting properly even there is binary in the relationship between propeller torque and rotation number, and air speed, and capable of improving detection accuracy and responsibility.SOLUTION: Provided is a motor-driven propulsion controller 100 for rotating and driving a propulsion propeller 101. The motor-driven propulsion controller 100 is configured so that the air speed is estimated based on plural estimated values of torque and a rotation number which are detected under a drive condition different from a data group related to air speed and propeller characteristic which are stored in advance.
摘要翻译：要解决的问题：提供一种电动推进控制器，其能够仅通过电气方式抑制对重量或成本的影响，即使在螺旋桨转矩和转速之间的关系以及空气速度上也能够二次检测，以及能够提高检测精度和责任。解决方案：提供一种用于旋转和驱动推进推进器101的电动推进控制器100.电动推进控制器100构造成使得基于多个估计值在与预先存储的与空气速度和螺旋桨特性相关的数据组不同的驱动条件下检测的转矩和转数。

3. 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

4. 发明专利

JP2008164495A Method for measuring multi-component force, and device thereof 有权
标题翻译：用于测量多组分力的方法及其装置
公开(公告)号：JP2008164495A
公开(公告)日：2008-07-17
申请号：JP2006355856
申请日：2006-12-28
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： KOBAYASHI CHU , NISHIZAWA HIROSHI
IPC分类号： G01L5/16
摘要： PROBLEM TO BE SOLVED: To provide a method capable of accurately measuring each force component acting on a model, by providing arbitrariness in the position of sensor so as to strictly exclude the effects of inertial force that originate in vibration from a force measurement system, to flexibly cope with constitutions of various measurement systems, and also to provide a device implementing the same, in multi-component force measurement by combining a force detection sensor and an acceleration sensor.
SOLUTION: The force measurement method using a force detector detecting the force in a prescribed direction acting on the measurement object via a connection member fixed to the object and the acceleration sensor fixed to the connection member or the measurement object, calculates a correlation time, in which an autocorrelation coefficient of time series signals of the acceleration sensor and the force detector is at the maximum value; detects the time when the acceleration detected by the acceleration sensor is at preset acceleration to specify the time when the time at which the autocorrelation coefficient is the maximum value has elapsed from the detection time; and adopts the detection value of the force detector in a prescribed direction at the specified time, as the value at which the inertial force due to the vibration acting on the measurement object does not affect the force detector.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够精确地测量作用在模型上的每个力分量的方法，通过在传感器的位置提供任意性，以便严格排除来自力测量的起源于振动的惯性力的影响系统，以灵活应对各种测量系统的结构，并且还通过组合力检测传感器和加速度传感器来提供实现相同的装置的多分力测量。解决方案：使用力检测器，其通过固定到物体的连接构件和固定到连接构件或测量对象的加速度传感器来检测沿规定方向作用在测量对象上的力的力检测方法，计算相关性时间，其中加速度传感器和力检测器的时间序列信号的自相关系数处于最大值; 检测由加速度传感器检测到的加速度处于预设加速度的时间，以指定从检测时间起经过自相关系数为最大值的时间的时间; 并且在规定的时刻将规定的方向的力检测器的检测值作为在作用于测定对象物上的振动的惯性力不影响力检测器的值。版权所有（C）2008，JPO＆INPIT

5. 发明专利

JP2014004875A Noise reducing method and noise reducing device of rotating body 审中-公开
标题翻译：噪声减少方法和噪声减少装置的旋转体
公开(公告)号：JP2014004875A
公开(公告)日：2014-01-16
申请号：JP2012140566
申请日：2012-06-22
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： B64C11/30 , F03D1/06 , F03D11/00 , F04D29/36 , F04D29/66
CPC分类号： Y02E10/721
摘要： PROBLEM TO BE SOLVED: To provide a noise reducing method and a noise reducing device of a rotating body capable of reducing substantively observed noise by changing a distribution of sound pressure at a periphery of the rotating body without performing a special design on a surface of a blade and without lowering an efficiency.SOLUTION: In the rotating body including a blade radially attached to a rotation shaft, the pressure distribution at the surface of the blade when the rotation shaft is rotated is actively changed in correspondence with the rotation phase of the rotation shaft.
摘要翻译：要解决的问题：提供一种旋转体的降噪方法和降噪装置，其能够通过改变旋转体周围的声压分布而不会在其表面上进行特殊设计来减少实质上观察到的噪声并且不降低效率。解决方案：在包括径向附接到旋转轴的叶片的旋转体中，当旋转轴旋转时叶片表面的压力分布与旋转的旋转相位相应地主动地改变轴。

6. 发明专利

JP2009023629A Stol aircraft 有权
标题翻译： STOL飞机
公开(公告)号：JP2009023629A
公开(公告)日：2009-02-05
申请号：JP2007191773
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： B64C25/36 , B64C25/42
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: To overcome the above problem, the present invention applies drive wheels driven by motors of electric vehicles improved in performance dramatically in recent years to aircraft landing gears, and uses drive wheel thrust for taxiing and the combination of propeller thrust and drive wheel thrust for takeoff running, thereby solving a problem of reducing a takeoff run distance. Although an airframe may unfavorably pitch up due to drive wheel thrust in such cases, the present invention dynamically controls the drive wheel torque within a range in which the above pitch-up movement does not occur, thereby avoiding the pitch-up movement and a resulting contact of a tail portion of the airframe with the ground.
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：为了克服上述问题，本发明将电动汽车电机驱动的驱动轮近年来的性能显着提高到飞机起落架，并且使用驱动轮推力用于滑行和螺旋桨推力与驱动的组合用于起飞行驶的轮推力，从而解决了降低起飞行驶距离的问题。虽然在这种情况下机身可能由于驱动轮推力而不利地向上俯仰，但是本发明在不发生上述俯仰运动的范围内动态地控制驱动轮扭矩，从而避免俯仰运动，从而产生机身尾部与地面接触。版权所有（C）2009，JPO＆INPIT

7. 发明专利

JP2008206294A Self-powered servo motor system 审中-公开
标题翻译：自动伺服电机系统
公开(公告)号：JP2008206294A
公开(公告)日：2008-09-04
申请号：JP2007039174
申请日：2007-02-20
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： KOBAYASHI CHU , NISHIZAWA HIROSHI
IPC分类号： H02P5/00 , H02J7/00 , H02J13/00
摘要： PROBLEM TO BE SOLVED: To simplify wiring from a control unit to multiple servo motors disposed in arbitrary positions in equipment to more efficiently operate the servo motors, and to provide a servo motor system having the functions of: charging multiple batteries for servo motors placed at various points of the equipment body from a charging terminal; charging a weak battery and driving the corresponding servo motor; and suppressing the power consumption of motors when they are not driven.
SOLUTION: The servo motor system is so constructed that actuators are disposed at multiple points in the equipment. A control unit and a charging battery are installed in the center. In each actuator, a servo motor unit is installed. Each servo motor unit incorporates a battery as a motor power supply integrated with a servo motor and a motor control unit. As a preferred embodiment, the control unit in the center and each actuator are connected with each other by a line that is used both as a signal line and a supply line for charging the battery.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了简化从控制单元到设置在设备中任意位置的多个伺服电机的布线，以更有效地操作伺服电机，并且提供具有以下功能的伺服电机系统：具有以下功能的功能：为多个电池供给伺服从充电终端放置在设备主体的各个点的电机; 对弱电池充电并驱动相应的伺服电机; 并且在不驱动时抑制电动机的功率消耗。
解决方案：伺服电机系统的结构使得致动器设置在设备的多个点处。中央安装有控制单元和充电电池。在每个执行器中，安装有伺服电机单元。每个伺服电机单元包含一个电池作为与伺服电机和电动机控制单元集成的电动机电源。作为优选实施例，中心的控制单元和每个致动器通过用作信号线和用于对电池充电的供给线的线相互连接。版权所有（C）2008，JPO＆INPIT

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