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1. 发明授权

US08525621B2 Boundary acoustic wave filter 有权
标题翻译：边界声波滤波器
公开(公告)号：US08525621B2
公开(公告)日：2013-09-03
申请号：US12398237
申请日：2009-03-05
申请人： Takashi Yamane , Masaru Yata
发明人： Takashi Yamane , Masaru Yata
IPC分类号： H03H9/46 , H03H9/64
CPC分类号： H03H9/0222 , H03H9/0038 , H03H9/0071 , H03H9/0085 , H03H9/14582 , H03H9/14588
摘要： A boundary acoustic wave filter device includes an electrode structure provided at a boundary between a piezoelectric body and a dielectric body laminated on the piezoelectric body and utilizes an SH-type boundary acoustic wave that propagates along the boundary. In the boundary acoustic wave filter device, the electrode structure includes a longitudinally coupled resonator boundary acoustic wave filter portion that has a first IDT and second and third IDTs arranged respectively on both sides of the IDT in a direction in which the boundary acoustic wave propagates. At portions at which two IDTs are located adjacent to each other in the direction in which the boundary acoustic wave propagates, narrow pitch electrode finger portions are provided in the IDTs, and the pitch of the electrode fingers of the narrow pitch electrode finger portion is different from the pitch of the electrode fingers of each of the narrow pitch electrode finger portions.
摘要翻译：一种边界声波滤波器装置，包括设置在压电体和层叠在压电体上的电介质体之间的边界处的电极结构，利用沿边界传播的SH型边界声波。在边界声波滤波器装置中，电极结构包括纵向耦合的谐振器边界弹性波滤波器部分，其具有在边界声波传播的方向上分别布置在IDT的两侧上的第一IDT和第二和第三IDT。在两个IDT彼此相邻的部分，在声波传播的方向上，在IDT中设置窄间距电极指部分，窄间距电极指部分的电极指的间距不同从每个窄间距电极指部分的电极指的间距开始。

2. 发明授权

US09133717B2 Cooling structure of turbine airfoil 有权
标题翻译：涡轮机翼的冷却结构
公开(公告)号：US09133717B2
公开(公告)日：2015-09-15
申请号：US12812227
申请日：2009-01-08
申请人： Chiyuki Nakamata , Takashi Yamane , Yoshitaka Fukuyama , Takahiro Bamba
发明人： Chiyuki Nakamata , Takashi Yamane , Yoshitaka Fukuyama , Takahiro Bamba
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/186 , F05D2240/121 , F05D2240/122 , F05D2240/303 , F05D2240/304 , F05D2260/201 , F05D2260/205 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141
摘要： A cooling structure of a turbine airfoil cools a turbine airfoil (10) exposed to hot gas (1), using cooling air (2) of a temperature lower than that of the hot gas. The turbine airfoil (10) includes an external surface (11), an internal surface (12) opposite to the external surface, a plurality of film-cooling holes (13) blowing the cooling air from the internal surface toward the external surface to film-cool the external surface, and a plurality of heat-transfer promoting projections (14) integrally formed with the internal surface and protruding inwardly from the internal surface. The turbine airfoil further includes a hollow cylindrical insert (20) which is positioned inside the internal surface of the turbine airfoil and to which the cooling air is supplied. The insert has a plurality of impingement holes (21) for impingement-cooling the internal surface (12).
摘要翻译：涡轮翼型件的冷却结构使用比热气体的温度低的冷却空气（2）冷却暴露于热气体（1）的涡轮机翼型件（10）。涡轮机翼（10）包括外表面（11），与外表面相对的内表面（12），多个薄膜冷却孔（13），其将冷却空气从内表面向外表面吹向薄膜 - 冷却外表面，以及多个传热促进突起（14），其与内表面整体形成并从内表面向内突出。涡轮机翼片还包括中空圆柱形插入件（20），该中空圆柱形插入件位于涡轮机翼片的内表面内部，并且供应冷却空气。插入件具有用于冲击冷却内表面（12）的多个冲击孔（21）。

3. 发明授权

US08515524B2 Extracorperal ultrasonic irradition of titanium oxide (TiO2) coated implant for angiogenesis stimulation 有权
标题翻译：氧化钛（TiO2）涂层植入物用于血管生成刺激的超声波超声辐照
公开(公告)号：US08515524B2
公开(公告)日：2013-08-20
申请号：US12325678
申请日：2008-12-01
申请人： Tsutomu Furuzono , Miwa Masuda , Masahiro Okada , Naotaka Nitta , Takashi Yamane
发明人： Tsutomu Furuzono , Miwa Masuda , Masahiro Okada , Naotaka Nitta , Takashi Yamane
IPC分类号： A61B5/00
CPC分类号： A61B90/40 , A61N7/00
摘要： The present invention solves the issue of bacterial infection by medical devices such as intracorporeal indwelling catheters. The present invention relates to an ultrasonic medical apparatus including a medical device (titanium oxide coated medical device 10) covered with a titanium oxide material (titanium oxide alone or a titanium oxide composite material) and ultrasonic irradiation means 20. Ultrasonic irradiation of the titanium oxide material, which exists on a surface of the medical device, causes the surface of the medical device to exert beneficial effects such as antibiotic action, the stimulation of angiogenesis, and the degradation of a blood clot and a biofilm.
摘要翻译：本发明解决了诸如体内留置导管之类的医疗装置的细菌感染问题。超声波医疗装置技术领域本发明涉及一种超声波医疗装置，其包括被钛氧化物材料（单独的氧化钛或氧化钛复合材料）覆盖的医疗装置（氧化钛被覆医用器具10）和超声波照射手段20。存在于医疗装置的表面上的材料导致医疗装置的表面发挥有益效果，例如抗生素作用，刺激血管生成以及血块和生物膜的降解。

4. 发明授权

US08179017B2 Boundary acoustic wave device having three-medium structure 有权
标题翻译：具有三介质结构的边界声波装置
公开(公告)号：US08179017B2
公开(公告)日：2012-05-15
申请号：US13172966
申请日：2011-06-30
申请人： Takashi Yamane
发明人： Takashi Yamane
IPC分类号： H03H9/25 , H01L41/08
CPC分类号： H03H9/0222 , H03H9/02559
摘要： A boundary acoustic wave device that has a three-medium structure and that prevents a high-order mode spurious response includes a piezoelectric substrate, a first dielectric layer laminated on the piezoelectric substrate, a second dielectric layer laminated on the first dielectric layer, and an IDT electrode provided at an interface between the piezoelectric substrate and the first dielectric layer. The boundary acoustic wave device utilizes a Stoneley wave that propagates along the interface. Where V1 denotes an acoustic velocity of a slow transversal bulk wave in the piezoelectric substrate and Va denotes an acoustic velocity at an anti-resonant point in a high-order mode of the Stoneley wave, Va>V1 is satisfied.
摘要翻译：具有三介质结构并且防止高阶模式杂散响应的弹性边界波装置包括压电基片，层压在压电基片上的第一电介质层，层叠在第一介电层上的第二电介质层和 IDT电极设置在压电基板和第一介电层之间的界面处。边界声波装置利用沿着界面传播的斯通利波。其中V1表示压电衬底中的慢横向体波的声速，Va表示在斯通利波的高阶模式下的反谐振点处的声速，满足Va> V1。

5. 发明授权

US06840981B2 Method of producing reduced iron and production facilities therefor 失效
标题翻译：生产还原铁及其生产设备的方法
公开(公告)号：US06840981B2
公开(公告)日：2005-01-11
申请号：US09848280
申请日：2001-05-04
申请人： Hironori Fujioka , Hideaki Mizuki , Koichi Hirata , Shigeo Itano , Susumu Kamikawa , Hisao Teramoto , Takashi Yamane , Shigeki Sueda , Tetsumasa Kawamoto
发明人： Hironori Fujioka , Hideaki Mizuki , Koichi Hirata , Shigeo Itano , Susumu Kamikawa , Hisao Teramoto , Takashi Yamane , Shigeki Sueda , Tetsumasa Kawamoto
IPC分类号： C22B1/16 , C21B13/00 , C21B13/10 , C21B13/14 , C22B1/244 , C22B1/245
CPC分类号： C21B13/14 , C21B13/008 , C21B13/10 , C21B13/105 , C22B1/244 , C22B1/245 , Y02P10/136
摘要： A method of producing reduced iron pellets including reducing raw material pellets to obtain reduced iron pellets, and rolling the reduced iron pellets at a temperature ranging between 800 and 1200° C. sufficiently such that the reduced iron pellets undergo sintering.
摘要翻译：一种生产还原铁丸的方法，包括减少原料颗粒以获得还原铁丸，并且在800和1200℃之间的温度范围内充分地轧制还原铁丸，使得还原铁颗粒经历烧结。

6. 发明授权

US08436510B2 Boundary acoustic wave device 有权
标题翻译：边界声波装置
公开(公告)号：US08436510B2
公开(公告)日：2013-05-07
申请号：US12913847
申请日：2010-10-28
申请人： Takashi Yamane , Takeshi Nakao
发明人： Takashi Yamane , Takeshi Nakao
IPC分类号： H01L41/083
CPC分类号： H01L41/18 , H03H9/0222 , H03H9/02559 , H03H9/02574
摘要： A boundary acoustic wave device includes a piezoelectric substrate made of single-crystalline LiTaO3, a first medium layer disposed on the piezoelectric substrate and made of a dielectric, a second medium layer disposed on the first medium layer and made of a dielectric having a sound velocity different from that of the first medium layer, and at least one interdigital electrode disposed at the boundary between the piezoelectric substrate and the first medium layer. The sound velocity of the first medium layer is less than the sound velocity of LiTaO3. The sound velocity of the second medium layer is greater than the sound velocity of LiTaO3. The inequality (h/λ)×a≦0.05 is satisfied, where H is the thickness of the first medium layer, h is the thickness of the interdigital electrode, λ is the period of electrode fingers of the interdigital electrode, and a is the ratio of the density of a metal of the interdigital electrode to the density of Au.
摘要翻译：声界面波装置包括由单晶LiTaO 3构成的压电基板，设在压电基板上的第一介质层，由电介质构成，第二介质层设置在第一介质层上，由具有声速与第一介质层的不同，以及设置在压电基板和第一介质层之间的边界处的至少一个叉指电极。第一介质层的声速小于LiTaO3的声速。第二介质层的声速大于LiTaO3的声速。满足不等式（h/lambda),a@0.05），其中H是第一介质层的厚度，h是叉指电极的厚度，λ是叉指电极的电极指的周期，a是指数电极的金属密度与Au的密度之比。

7. 发明授权

US08172505B2 Cooling structure 有权
标题翻译：冷却结构
公开(公告)号：US08172505B2
公开(公告)日：2012-05-08
申请号：US12279452
申请日：2007-02-07
申请人： Shu Fujimoto , Yoshitaka Fukuyama , Takashi Yamane , Masahiro Matsushita , Toyoaki Yoshida
发明人： Shu Fujimoto , Yoshitaka Fukuyama , Takashi Yamane , Masahiro Matsushita , Toyoaki Yoshida
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D9/041 , F05D2250/185 , F05D2250/314 , F05D2250/70 , F05D2260/202 , F05D2260/2212 , F05D2260/22141
摘要： In this cooling structure, a cooling flow path, which is meandering around a flow direction of a high temperature combustion gas, is provided in a structural body. The cooling flow path has an inflow path for a cooling air formed inside of the structural body; at least one straight flow path provided with intervals with respect to an axial line; and a turning flow path for communicating the end portions of the inflow path with the straight flow path or communicating with the end portions of the straight flow paths one after another.
摘要翻译：在这种冷却结构中，在结构体中设置有围绕高温燃烧气体的流动方向曲折的冷却流路。冷却流路具有形成在结构体内部的冷却空气的流入路径，至少一个相对于轴线设置间隔的直流道; 以及用于使流入路径的端部与直流路连通或者与直流路径的端部相互连通的回转流路。

8. 发明申请

US20110027102A1 COOLING STRUCTURE OF TURBINE AIRFOIL 有权
标题翻译：涡轮机空气冷却结构
公开(公告)号：US20110027102A1
公开(公告)日：2011-02-03
申请号：US12812227
申请日：2009-01-08
申请人： Chiyuki Nakamata , Takashi Yamane , Yoshitaka Fukuyama , Takahiro Bamba
发明人： Chiyuki Nakamata , Takashi Yamane , Yoshitaka Fukuyama , Takahiro Bamba
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/186 , F05D2240/121 , F05D2240/122 , F05D2240/303 , F05D2240/304 , F05D2260/201 , F05D2260/205 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141
摘要： A cooling structure of a turbine airfoil cools a turbine airfoil (10) exposed to hot gas (1), using cooling air (2) of a temperature lower than that of the hot gas. The turbine airfoil (10) includes an external surface (11), an internal surface (12) opposite to the external surface, a plurality of film-cooling holes (13) blowing the cooling air from the internal surface toward the external surface to film-cool the external surface, and a plurality of heat-transfer promoting projections (14) integrally formed with the internal surface and protruding inwardly from the internal surface. The turbine airfoil further includes a hollow cylindrical insert (20) which is positioned inside the internal surface of the turbine airfoil and to which the cooling air is supplied. The insert has a plurality of impingement holes (21) for impingement-cooling the internal surface (12).
摘要翻译：涡轮翼型件的冷却结构使用比热气体的温度低的冷却空气（2）冷却暴露于热气体（1）的涡轮机翼型件（10）。涡轮机翼（10）包括外表面（11），与外表面相对的内表面（12），多个薄膜冷却孔（13），其将冷却空气从内表面向外表面吹向薄膜 - 冷却外表面，以及多个传热促进突起（14），其与内表面整体形成并从内表面向内突出。涡轮机翼片还包括中空圆柱形插入件（20），该中空圆柱形插入件位于涡轮机翼片的内表面内部，并且供应冷却空气。插入件具有用于冲击冷却内表面（12）的多个冲击孔（21）。

9. 发明申请

US20090126335A1 COOLING STRUCTURE 有权
标题翻译：冷却结构
公开(公告)号：US20090126335A1
公开(公告)日：2009-05-21
申请号：US12279452
申请日：2007-02-07
申请人： Shu Fujimoto , Yoshitaka Fukuyama , Takashi Yamane , Masahiro Matsushita , Toyoaki Yoshida
发明人： Shu Fujimoto , Yoshitaka Fukuyama , Takashi Yamane , Masahiro Matsushita , Toyoaki Yoshida
IPC分类号： F02C7/12 , F28F7/00
CPC分类号： F01D5/187 , F01D9/041 , F05D2250/185 , F05D2250/314 , F05D2250/70 , F05D2260/202 , F05D2260/2212 , F05D2260/22141
摘要： In this cooling structure, a cooling flow path, which is meandering around a flow direction of a high temperature combustion gas, is provided in a structural body. The cooling flow path has an inflow path for a cooling air formed inside of the structural body; at least one straight flow path provided with intervals with respect to an axial line; and a turning flow path for communicating the end portions of the inflow path with the straight flow path or communicating with the end portions of the straight flow paths one after another.
摘要翻译：在这种冷却结构中，在结构体中设置有围绕高温燃烧气体的流动方向曲折的冷却流路。冷却流路具有形成在结构体内部的冷却空气的流入路径，至少一个相对于轴线设置间隔的直流道; 以及用于使流入路径的端部与直流路连通或者与直流路径的端部相互连通的回转流路。

10. 发明申请

US20080077263A1 DATA RECORDING DEVICE, DATA RECORDING METHOD, AND DATA RECORDING PROGRAM 审中-公开
标题翻译：数据记录装置，数据记录方法和数据记录程序
公开(公告)号：US20080077263A1
公开(公告)日：2008-03-27
申请号：US11851018
申请日：2007-09-06
申请人： Takashi Yamane , Susumu Ijichi , Takeshi Iwatsu
发明人： Takashi Yamane , Susumu Ijichi , Takeshi Iwatsu
IPC分类号： G06F17/00
CPC分类号： G11B27/28 , G11B27/031 , H04H60/27 , H04H60/37 , H04H60/58
摘要： Disclosed herein is a data recording device including: a feature quantity detecting unit configured to detect a predetermined feature quantity of mixed data in which a music part and a talking part are mixed; a sound volume level detecting unit configured to detect sound volume level of the mixed data; a section identifying unit configured to identify a music part section corresponding to the music part and a talking part section corresponding to the talking part in the mixed data on a basis of the feature quantity and the sound volume level; and a recording unit configured to record the mixed data including the music part section and the talking part section identified by the section identifying unit.
摘要翻译：这里公开了一种数据记录装置，包括：特征量检测单元，被配置为检测音乐部分和通话部分混合的混合数据的预定特征量; 声音量检测单元，被配置为检测所述混合数据的音量水平; 部分识别单元，被配置为基于特征量和音量水平来识别对应于音乐部分的音乐部分部分和与混合数据中的通话部分相对应的通话部分部分; 以及记录单元，被配置为记录包括由区段识别单元识别的音乐部分部分和通话部分部分的混合数据。

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