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61. 发明授权

US09193591B2 Ozone gas generator and method for manufacturing the same 有权
标题翻译：臭氧气体发生器及其制造方法
公开(公告)号：US09193591B2
公开(公告)日：2015-11-24
申请号：US13499675
申请日：2010-09-21
申请人： Takashi Matsuno , Osamu Takemura
发明人： Takashi Matsuno , Osamu Takemura
IPC分类号： B01J19/08 , C01B13/11
CPC分类号： C01B13/11 , C01B2201/32 , C01B2201/34 , C01B2201/64 , C01B2201/90
摘要： A dielectric 13 is provided on each of opposing surfaces of a pair of electrodes 14. Discharge gaps 20 communicating with a raw material gas supply path and an ozone gas removal path are formed between the pair of dielectrics 13. A functional film 17 is formed on each of the pair of dielectrics 13 so as to face the discharge gaps 20. The functional film 17 contains a first metal oxide of one or more metals selected from a group consisting of niobium, tantalum, molybdenum, and chromium, and a second metal oxide of one or more metals selected from a group consisting of titanium, tungsten, zinc, and iron.
摘要翻译：在一对电极14的每个相对表面上设置有电介质13.在一对电介质13之间形成有与原料气体供给路径连通的排出间隙20和臭氧气体除去路径。功能膜17形成在一对电介质13中的每一个与放电间隙20相对。功能膜17含有选自铌，钽，钼和铬中的一种或多种金属的第一金属氧化物和第二金属氧化物的一种或多种选自钛，钨，锌和铁的金属。

62. 发明授权

US08813832B2 Heat sink 有权
标题翻译：散热器
公开(公告)号：US08813832B2
公开(公告)日：2014-08-26
申请号：US13257387
申请日：2010-03-12
申请人： Keiji Miki , Kenji Ando
发明人： Keiji Miki , Kenji Ando
IPC分类号： B60H3/00 , F28F1/30 , F28F1/14 , B61C17/00 , H05K7/20 , H01L23/467
CPC分类号： B61C17/00 , H01L23/467 , H01L2924/0002 , H05K7/209 , Y02T30/10 , H01L2924/00
摘要： A heat sink which is mounted in a movable body and which is to be exposed to a traveling air stream generated while the movable body moves includes a base and a heat dissipating portion having a plurality of fins. At least in a front end portion of the heat dissipating portion, the heat dissipating portion includes a rectifying portion provided so as to extend across a predetermined area in a longitudinal direction in front portions of slit-shaped flow paths at an upstanding end (i.e., an end apart from the base).
摘要翻译：安装在可移动体中并且暴露于可移动体移动时产生的行进气流的散热器包括基部和具有多个翅片的散热部。至少在散热部的前端部，散热部包括整流部，该整流部设置成在直立端部的狭缝状流路的前方在长度方向上延伸规定的区域（即，距离基地的一端）。

63. 发明申请

US20140224445A1 Metal Filling Device 有权
标题翻译：金属灌装装置
公开(公告)号：US20140224445A1
公开(公告)日：2014-08-14
申请号：US14343650
申请日：2012-09-14
申请人： Tatsuo Kikuchi
发明人： Tatsuo Kikuchi
IPC分类号： H01L21/3205 , B22D19/00 , B22D45/00 , H01L21/768
CPC分类号： H01L21/32051 , B22D19/00 , B22D19/08 , B22D39/02 , B22D45/00 , C23C6/00 , H01L21/768 , H01L21/76898
摘要： A metal filling apparatus 1 fills a molten metal M into a minute space formed on a surface of a semiconductor wafer K. The metal filling apparatus 1 has a processor body 2 having a processing chamber 5 in which the semiconductor wafer K is held, a molten metal supply mechanism 10, and a molten metal recovery mechanism 20. The molten metal supply mechanism 10 includes a supply tank 11 in which the molten metal M is stored, a supply pipe 13 connected to the processing chamber 5 of the processor body 11 and the supply tank 11, and a supplier 12 interposed in the supply pipe 13 and supplying the molten metal M in the supply tank 11 into the processing chamber 5 through the supply pipe 13, and the molten metal recovery mechanism 20 recovers the molten metal M supplied into the processing chamber 5 from the processing chamber 5.
摘要翻译：金属填充装置1将熔融金属M填充到形成在半导体晶片K的表面上的微小空间中。金属填充装置1具有处理体2，处理室2具有保持半导体晶片K的处理室5，金属供给机构10和熔融金属回收机构20.熔融金属供给机构10包括供给槽11，熔融金属M被储存在该供给槽11中，供给管13与处理体11的处理室5连接，供给罐11和供给管12，插入到供给管13中，通过供给管13将供给槽11内的熔融金属M供给到处理室5，熔融金属回收机构20回收供给到的供给槽来自处理室5的处理室5。

64. 发明授权

US08701400B2 Electro-hydrostatic actuator excellent in snubbing characteristic, and drive device used for the same, and control method used for the same 有权
标题翻译：具有优良的缓冲特性的静电静电致动器及其驱动装置及其控制方法
公开(公告)号：US08701400B2
公开(公告)日：2014-04-22
申请号：US12943452
申请日：2010-11-10
申请人： Taku Kondo , Toshiyuki Kumada , Masayuki Takada , Kazuhiro Masutani , Masaaki Monte , Hiroshi Saito , Satoshi Ihara
发明人： Taku Kondo , Toshiyuki Kumada , Masayuki Takada , Kazuhiro Masutani , Masaaki Monte , Hiroshi Saito , Satoshi Ihara
IPC分类号： F15B11/028
CPC分类号： F15B7/006 , B64C13/504 , B64C25/22 , F15B15/222
摘要： The present invention is to provide an electro hydrostatic actuator excellent in a snubbing characteristic including a cylinder type actuator main body 1, a piston 2 having a piston rod, the piston slidingly moving in a cylinder of the actuator main body, a motor 18, a pump 19 for supplying fluid according to the rotation of the motor, a mechanism for adjusting a running amount of the fluid into and from the cylinder according to the motion of the piston, and a reservoir 8 for adjusting the supply of the fluid corresponding to a volume difference generated according to the motion of the piston, and a controller 17 which controls the number of revolutions of the motor according to the calculated load torque, and a snubbing control method used for this. An electro hydrostatic actuator of realizing a snubbing mechanism capable of increasing energy efficiency, when used for a landing gear retraction/extension device of an airplane, can be provided.
摘要翻译：本发明提供一种具有优良的缓冲特性的静电静电执行机构，其特征在于：包括气缸式致动器主体1，具有活塞杆的活塞2，在致动器主体的气缸中滑动运动的活塞，马达18，用于根据电动机的旋转供给流体的泵19，用于根据活塞的运动来调节流入和流出气缸的流体的运动量的机构;以及用于调节与a相对应的流体供应的储存器8 根据活塞的运动产生的体积差;以及根据计算出的负载转矩来控制电动机的转数的控制器17，以及用于此的缓冲控制方法。可以提供一种当用于飞机的起落架缩回/延伸装置时，实现能够提高能量效率的缓冲机构的静电静电致动器。

65. 发明授权

US08630750B2 Method of controlling steering control equipment for aircraft, and steering control equipment for aircraft and aircraft provided therewith 有权
标题翻译：控制飞机转向控制设备的方法以及为此提供的飞机和飞机的转向控制设备
公开(公告)号：US08630750B2
公开(公告)日：2014-01-14
申请号：US13275571
申请日：2011-10-18
申请人： Kazunari Tada , Kazushi Furuichi , Yutaro Minami
发明人： Kazunari Tada , Kazushi Furuichi , Yutaro Minami
IPC分类号： G01C23/00 , B64C25/50
CPC分类号： B64C25/50 , G05D1/0083
摘要： A steering control equipment has a controller having a provisional-target-angular-position calculating section calculating a provisional target angular position of a steering mechanism corresponding to the operation amounts of a steering handle and rudder pedals, a speed setting section setting the aircraft speed on the basis of detected ground speed and airspeed, a target-angular-position limiting section outputting the provisional target angular position as a final target angular position when the calculated provisional target angular position is equal to or lower than a limit value corresponding to the set speed and outputting the limit value as a final target angular position when the calculated provisional target angular position is larger than the limit value, and a actuating control section controlling an actuating mechanism for actuating the steering mechanism so that the output final target angular position and the actual angular position of the steering mechanism detected coincide with each other.
摘要翻译：转向控制装置具有控制器，该控制器具有临时目标角位置计算部，计算与转向手柄和方向舵踏板的操作量对应的转向机构的临时目标角位置，设定飞行器速度的速度设定部作为检测到的地面速度和空速的基础，当所计算的临时目标角位置等于或低于对应于设定速度的极限值时，将临时目标角位置输出为最终目标角位置的目标角位置限制部以及当所计算的临时目标角位置大于所述极限值时，将所述极限值作为最终目标角位置输出;以及致动控制部，其控制用于致动所述转向机构的致动机构，使得所述输出的最终目标角位置和实际转向机构的角位置被检测到相互否认。

66. 发明申请

US20130255090A1 SIX-DIRECTION DIRECTING DEVICE 有权
标题翻译：六方向指导设备
公开(公告)号：US20130255090A1
公开(公告)日：2013-10-03
申请号：US13824334
申请日：2011-09-26
申请人： Futoshi Magosaki
发明人： Futoshi Magosaki
IPC分类号： G01C19/38
CPC分类号： G01C19/38
摘要： The six direction directing device includes a shaft, a rotation member, a driving source, and a guide member. The shaft extends in an X axis direction. The rotation member is rotatable around an inclined axis inclined at α deg with respect to the shaft. The rotation member has an xyz rectangular coordinate system. The rotation member further includes a spherical surface and an orbit portion formed around an x axis of the spherical surface. The guide member is fixed to an XYZ rectangular coordinate system. The orbit portion has such a shape that the y axis of the rotation member is sequentially directed in + and − directions on the U, V, and W axes that cross one another at intervals of 60 deg around the X axis when the rotation member is rotated in contact with the guide member by the rotation of the shaft.
摘要翻译：六方向定向装置包括轴，旋转构件，驱动源和引导构件。轴沿X轴方向延伸。旋转构件可以相对于轴倾斜为α°的倾斜轴线旋转。旋转构件具有xyz直角坐标系。旋转构件还包括球形表面和围绕球形表面的x轴形成的轨道部分。导向件固定在XYZ直角坐标系上。轨道部具有这样的形状，使得旋转构件的y轴在U轴，V轴和W轴上以+和 - 方向依次指向，当旋转构件为通过轴的旋转与导向构件接触地旋转。

67. 发明申请

US20130068885A1 LANDING GEAR RETRACTION/EXTENSION DEVICE OF AIRCRAFT 有权
标题翻译：起落架齿轮减速/飞机延伸装置
公开(公告)号：US20130068885A1
公开(公告)日：2013-03-21
申请号：US13618540
申请日：2012-09-14
申请人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
发明人： Yasuto Onomichi , Taku Kondo , Shogo Hagihara , Ryo Takaki , Takaaki Onishi
IPC分类号： B64C25/22
CPC分类号： B64C25/22 , B64C13/504 , F15B1/26 , F15B7/006 , F15B21/042 , F15B2211/20515 , F15B2211/20538 , F15B2211/20561 , F15B2211/27 , F15B2211/3058 , F15B2211/411 , F15B2211/4159 , F15B2211/6343 , F15B2211/6651 , F15B2211/8752
摘要： A landing gear retraction/extension device includes a hydraulic actuator, a hydraulic circuit, a hydraulic pump, an electric motor, and a driver. Part of the hydraulic circuit is provided such that heat is exchangeable between operation oil and each of the electric motor and the driver. The driver supplies power to the electric motor before landing of an aircraft such that an operation oil temperature is higher than a predetermined temperature upon the landing of the aircraft.
摘要翻译：起落架缩回/延伸装置包括液压致动器，液压回路，液压泵，电动马达和驱动器。设置液压回路的一部分，使得在操作油和电动马达和驱动器中的每一个之间可以更换热量。驾驶员在飞机着陆之前向电动机供电，使飞机降落时操作油温度高于预定温度。

68. 发明授权

US08381590B2 Vibrating gyroscope using piezoelectric film and method for manufacturing same 有权
标题翻译：使用压电薄膜的振动陀螺仪及其制造方法
公开(公告)号：US08381590B2
公开(公告)日：2013-02-26
申请号：US12863639
申请日：2008-11-26
申请人： Takashi Ikeda , Hiroshi Nishida , Osamu Torayashiki , Mitsuhiko Takemura , Tsuyoshi Fujimura , Ryuta Araki , Takafumi Moriguchi , Nobutaka Teshima , Yasuyuki Hirata
发明人： Takashi Ikeda , Hiroshi Nishida , Osamu Torayashiki , Mitsuhiko Takemura , Tsuyoshi Fujimura , Ryuta Araki , Takafumi Moriguchi , Nobutaka Teshima , Yasuyuki Hirata
IPC分类号： G01C19/56
CPC分类号： G01C19/5684
摘要： A vibrating gyroscope comprises a ring-shaped vibrating body (11) a leg portion (15) flexibly supporting the body (11) and having a fixed end, a fixed potential electrode (16), and a plurality of electrodes (13a-13d) with a piezoelectric film sandwiched between an upper and a lower-layer metallic film in a thickness direction thereof. When N is a natural number of 2 or more, the plurality of electrodes (13a-13d) include driving electrodes (13a) for a primary vibration in a vibration mode of cosNθ, which are each disposed (360/N)° apart from each other in a circumferential direction, first detection electrodes (13b) and second detection electrodes (13d) for detecting a secondary vibration generated when an angular velocity is applied to the body (11), which are each disposed in a certain region related to the driving electrode (13a) Each of the electrodes is also disposed in a certain region of the body (11).
摘要翻译：振动陀螺仪包括环形振动体（11），柔性地支撑主体（11）并具有固定端的腿部（15），固定电位电极（16）和多个电极（13a-13d）其中压电薄膜夹在上下金属薄膜的厚度方向上。当N为2以上的自然数时，多个电极（13a-13d）包括用于主要振动的驱动电极（13a），其以cosN＆amp;θ的振动模式分别设置（360 / N）° 第一检测电极（13b）和第二检测电极（13d），用于检测当对体（11）施加角速度时产生的二次振动，所述二次振动分别设置在与驱动电极（13a）每个电极也设置在主体（11）的某个区域中。

69. 发明申请

US20120189504A1 OZONE GAS GENERATOR AND METHOD FOR MANUFACTURING THE SAME 有权
标题翻译：臭氧发生器及其制造方法
公开(公告)号：US20120189504A1
公开(公告)日：2012-07-26
申请号：US13499675
申请日：2010-09-21
申请人： Takashi Matsuno , Osamu Takemura
发明人： Takashi Matsuno , Osamu Takemura
IPC分类号： B01J19/08 , B32B37/02 , B32B37/06
CPC分类号： C01B13/11 , C01B2201/32 , C01B2201/34 , C01B2201/64 , C01B2201/90
摘要： A dielectric 13 is provided on each of opposing surfaces of a pair of electrodes 14. Discharge gaps 20 communicating with a raw material gas supply path and an ozone gas removal path are formed between the pair of dielectrics 13. A functional film 17 is formed on each of the pair of dielectrics 13 so as to face the discharge gaps 20. The functional film 17 contains a first metal oxide of one or more metals selected from a group consisting of niobium, tantalum, molybdenum, and chromium, and a second metal oxide of one or more metals selected from a group consisting of titanium, tungsten, zinc, and iron.
摘要翻译：在一对电极14的每个相对表面上设置有电介质13.在一对电介质13之间形成有与原料气体供给路径连通的排出间隙20和臭氧气体除去路径。功能膜17形成在一对电介质13中的每一个与放电间隙20相对。功能膜17含有选自铌，钽，钼和铬中的一种或多种金属的第一金属氧化物和第二金属氧化物的一种或多种选自钛，钨，锌和铁的金属。

70. 发明申请

US20120052688A1 Plasma Etching Method 有权
标题翻译：等离子蚀刻法
公开(公告)号：US20120052688A1
公开(公告)日：2012-03-01
申请号：US13318279
申请日：2010-09-06
申请人： Akimitsu Oishi , Shoichi Murakami , Masayasu Hatashita
发明人： Akimitsu Oishi , Shoichi Murakami , Masayasu Hatashita
IPC分类号： H01L21/302
CPC分类号： H01L21/0475 , H01L21/3065 , H01L29/1608
摘要： The present invention relates to a plasma etching method with which a wide-gap semiconductor substrate can be etched with high accuracy. An inert gas is supplied into a processing chamber and plasma is generated from the inert gas, a bias potential is applied to a platen on which a wide-gap semiconductor substrate is placed, thereby making ions generated by the generation of plasma from the inert gas incident on the semiconductor substrate on the platen to thereby heat the semiconductor substrate. After the temperature of the semiconductor substrate reaches an etching temperature between 200° C. and 400° C., an etching gas is supplied into the processing chamber and plasma is generated from the etching gas and a bias potential is applied to the platen, thereby etching the semiconductor substrate while maintaining the temperature of the semiconductor substrate at the etching temperature.
摘要翻译：本发明涉及一种可以高精度地蚀刻宽间隙半导体衬底的等离子体蚀刻方法。将惰性气体供给到处理室中，从惰性气体产生等离子体，将偏置电位施加到放置宽间隙半导体基板的压板上，由此产生由惰性气体产生等离子体产生的离子入射到压板上的半导体衬底上从而加热半导体衬底。在半导体衬底的温度达到200℃至400℃的蚀刻温度之后，将蚀刻气体供应到处理室中，并且从蚀刻气体产生等离子体，并且将偏置电位施加到压板，由此在将半导体衬底的温度保持在蚀刻温度的同时蚀刻半导体衬底。

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