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1. 发明申请

US20080280159A1 Copper Foil and Method of Manufacturing the Same 失效
标题翻译：铜箔及其制造方法
公开(公告)号：US20080280159A1
公开(公告)日：2008-11-13
申请号：US11547517
申请日：2005-03-31
申请人： Kenichiro Iwakiri , Seiji Nagatani
发明人： Kenichiro Iwakiri , Seiji Nagatani
IPC分类号： B23P9/00 , C25F3/00
CPC分类号： C25D7/06 , H05K3/382 , H05K2201/0355 , Y10T428/12438 , Y10T428/12569 , Y10T428/1291 , Y10T428/12993
摘要： The object is to provide copper foil of high adhesion even when the roughness Rz of a nodular surface of the copper foil is low, and a method of manufacturing the copper foil. To achieve this object, there is adopted a copper foil which is characterized in that an area coefficient C(S), which is defined by A(S)/B(S) from a three-dimensional surface area A(S), which is obtained by performing three-dimensional measurement of a surface area of a nodular surface of a copper foil sample S under a laser microscope, and from a measuring region area B(S), which is an area of a measuring region of the three-dimensional surface area A(S), and a roughness Rz(S) of a nodular surface of the copper foil sample S, which is measured by a stylus-type roughness meter, have a relationship of equation (1) below, and in that the roughness Rz(S) is 1.0 μm to 3.0 μm, 0.5×Rz(S)+0.5≦C(S) (1) where Rz(S) is a numerical value represented by μm.
摘要翻译：本发明的目的是为了提供铜箔的高粘合性，即使铜箔的结节面的粗糙度R z较低，也可以提供铜箔的制造方法。为了实现该目的，采用铜箔，其特征在于，由三维表面积A（S）由A（S）/ B（S）定义的面积系数C（S），其中通过在激光显微镜下对铜箔样品S的结节面的表面积进行三维测量，并且从作为三维测量区域的测量区域的面积的测量区域B（S）获得，通过针式粗糙度计测量的铜箔样品S的结节表面的尺寸表面积A（S）和粗糙度R z（S）具有等式（1），并且粗糙度R z（S）为1.0μm〜3.0μm，<？在线式描述=“In-line Formulas”end =“lead”？ > 0.5xR z（S）+0.5 <= C（S）（1）<？在线公式描述=“在线公式”end =“tail”？>其中R < （S）是由mum表示的数值。

2. 发明授权

US07749610B2 Copper foil and method of manufacturing the same 失效
标题翻译：铜箔及其制造方法
公开(公告)号：US07749610B2
公开(公告)日：2010-07-06
申请号：US11547517
申请日：2005-03-31
申请人： Kenichiro Iwakiri , Seiji Nagatani
发明人： Kenichiro Iwakiri , Seiji Nagatani
IPC分类号： B32B15/20 , C25D7/06 , C25D3/38 , H05K1/09
CPC分类号： C25D7/06 , H05K3/382 , H05K2201/0355 , Y10T428/12438 , Y10T428/12569 , Y10T428/1291 , Y10T428/12993
摘要： The object is to provide copper foil of high adhesion even when the roughness Rz of a nodular surface of the copper foil is low, and a method of manufacturing the copper foil. To achieve this object, there is adopted a copper foil which is characterized in that an area coefficient C(S), which is defined by A(S)/B(S) from a three-dimensional surface area A(S), which is obtained by performing three-dimensional measurement of a surface area of a nodular surface of a copper foil sample S under a laser microscope, and from a measuring region area B(S), which is an area of a measuring region of the three-dimensional surface area A(S), and a roughness Rz(S) of a nodular surface of the copper foil sample S, which is measured by a stylus-type roughness meter, have a relationship of equation (1) below, and in that the roughness Rz(S) is 1.0 μm to 3.0 μm, 0.5×Rz(S)+0.5≦C(S) (1) where Rz(S) is a numerical value represented by μm.
摘要翻译：本发明的目的是提供铜箔的结节面的粗糙度Rz低的高粘合性的铜箔及其制造方法。为了实现该目的，采用铜箔，其特征在于，由三维表面积A（S）由A（S）/ B（S）定义的面积系数C（S），其中通过在激光显微镜下对铜箔样品S的结节面的表面积进行三维测量，并且从作为三维测量区域的测量区域的面积的测量区域B（S）获得，通过触针式粗糙度计测量的铜箔样品S的结节面的尺寸表面积A（S）和粗糙度Rz（S）具有以下等式（1）的关系，并且因此粗糙度Rz（S）为1.0μm〜3.0μm，0.5×Rz（S）+ 0.5＆amp; NlE; C（S）（1）其中，Rz（S）为由μm表示的数值。

3. 发明授权

US09546568B2 Cooling structure of bearing housing for turbocharger 有权
标题翻译：涡轮增压器轴承箱冷却结构
公开(公告)号：US09546568B2
公开(公告)日：2017-01-17
申请号：US14117795
申请日：2012-06-22
申请人： Tadashi Kanzaka , Kenichiro Iwakiri , Hiroshi Ogita
发明人： Tadashi Kanzaka , Kenichiro Iwakiri , Hiroshi Ogita
IPC分类号： F02B33/44 , F01D25/12 , F01D25/14 , F02B39/00
CPC分类号： F01D25/125 , F01D25/14 , F02B39/005 , F05D2220/40 , F05D2260/232
摘要： A cooling structure for a bearing housing for a turbocharger is provided. The cooling structure is configured so that the cooling structure has improved productivity, the occurrence of heat soak-back is reduced, and the cooling structure has improved cooling performance. The cooling structure cools both a bearing housing 13 and a bearing 52 by cooling water flowing through an annular cooling water path 13f formed in the bearing housing 13, and is provided with: a water path inlet 13h for supplying the cooling water and a water path outlet 13j for discharging the cooling water, which are provided in the bearing housing 13 to communicate with the annular cooling water path 13f; and a partial partition 14a in the bearing housing 13 to partially close a water path which forms the shortest route between the water path inlet 13h and the water path outlet 13j.
摘要翻译：提供了一种用于涡轮增压器的轴承壳体的冷却结构。冷却结构被构造成使得冷却结构具有提高的生产率，减少了热浸回的发生，并且冷却结构具有改善的冷却性能。冷却结构通过冷却流过形成在轴承箱13中的环形冷却水路径13f的水来冷却轴承壳体13和轴承52，并且设置有：用于供给冷却水的水路入口13h和水路出口13j，用于排出设置在轴承箱13中以与环形冷却水通道13f连通的冷却水; 以及轴承壳体13中的部分分隔部14a，以部分地闭合在水路入口13h与水路出口13j之间形成最短路线的水路。

4. 发明授权

US09366265B2 Scroll shape of centrifugal compressor 有权
标题翻译：涡旋式离心压缩机
公开(公告)号：US09366265B2
公开(公告)日：2016-06-14
申请号：US13978897
申请日：2012-01-27
申请人： Isao Tomita , Takashi Shiraishi , Kenichiro Iwakiri
发明人： Isao Tomita , Takashi Shiraishi , Kenichiro Iwakiri
IPC分类号： F04D29/42 , F04D29/40 , F04D29/44 , F04D29/68
CPC分类号： F04D29/4206 , F04D29/403 , F04D29/4226 , F04D29/441 , F04D29/681 , F05D2250/52
摘要： In a scroll shape of a centrifugal compressor, an enlargement rate of a ratio A/R of a cross-sectional area A of a scroll portion 12 to a radius R from an axis L1 of a compressor impeller 3 to a centroid P0 of a cross section of the scroll portion is reduced from a winding start to a winding end of the scroll portion.
摘要翻译：在离心式压缩机的涡旋形状中，涡旋部12的截面积A与压缩机叶轮3的轴线L1的相对于半径R的比A / R的增大率相对于十字形的重心P0 涡旋部的截面从涡旋部的卷绕开始减少到卷绕端。

5. 发明申请

US20130294903A1 SCROLL SHAPE OF CENTRIFUGAL COMPRESSOR 有权
标题翻译：离心式压缩机的滚动形状
公开(公告)号：US20130294903A1
公开(公告)日：2013-11-07
申请号：US13978897
申请日：2012-01-27
申请人： Isao Tomita , Takashi Shiraishi , Kenichiro Iwakiri
发明人： Isao Tomita , Takashi Shiraishi , Kenichiro Iwakiri
IPC分类号： F04D29/42
CPC分类号： F04D29/4206 , F04D29/403 , F04D29/4226 , F04D29/441 , F04D29/681 , F05D2250/52
摘要： In a scroll shape of a centrifugal compressor, an enlargement rate of a ratio A/R of a cross-sectional area A of a scroll portion 12 to a radius R from an axis L1 of a compressor impeller 3 to a centroid P0 of a cross section of the scroll portion is reduced from a winding start to a winding end of the scroll portion.
摘要翻译：在离心式压缩机的涡旋形状中，涡旋部12的截面积A与压缩机叶轮3的轴线L1的相对于半径R的比A / R的增大率相对于十字形的重心P0 涡旋部的截面从涡旋部的卷绕开始减少到卷绕端。

6. 发明申请

US20130266432A1 SCROLL STRUCTURE OF CENTRIFUGAL COMPRESSOR 有权
标题翻译：离心式压缩机的滚动结构
公开(公告)号：US20130266432A1
公开(公告)日：2013-10-10
申请号：US13823607
申请日：2011-12-05
申请人： Kenichiro Iwakiri , Isao Tomita , Motoki Ebisu , Hiroshi Suzuki , Takashi Shiraishi
发明人： Kenichiro Iwakiri , Isao Tomita , Motoki Ebisu , Hiroshi Suzuki , Takashi Shiraishi
IPC分类号： F04D29/40
CPC分类号： F04D29/403 , F04D29/4206 , F04D29/441 , F05D2250/52
摘要： A scroll structure of a centrifugal compressor 1 having a spirally formed scroll passage 13. The scroll passage 13 includes: a flat connecting portion A at a flow passage joint 23 where a scroll start and a scroll end of the scroll passage 13 meet, this flat connecting portion having a flat cross-sectional shape with a same height as that of an outlet passage of a diffuser; and a transition part 21 where the flat cross-sectional shape of the flat connecting portion A gradually changes back to a circular cross-sectional shape along a circumferential direction.
摘要翻译：具有螺旋形涡旋通道13的离心式压缩机1的涡旋结构。涡旋通道13包括：涡卷通道13的涡卷起动和涡旋端相交的流动通道接头23处的平坦连接部分A，连接部分具有与扩散器的出口通道相同的高度的平坦的横截面形状; 以及平坦连接部A的扁平截面形状沿圆周方向逐渐变回到圆形截面形状的过渡部21。

7. 发明授权

US09541094B2 Scroll structure of centrifugal compressor 有权
标题翻译：离心压缩机的涡旋结构
公开(公告)号：US09541094B2
公开(公告)日：2017-01-10
申请号：US13823607
申请日：2011-12-05
申请人： Kenichiro Iwakiri , Isao Tomita , Motoki Ebisu , Hiroshi Suzuki , Takashi Shiraishi
发明人： Kenichiro Iwakiri , Isao Tomita , Motoki Ebisu , Hiroshi Suzuki , Takashi Shiraishi
IPC分类号： F04D29/40 , F04D29/44 , F04D29/42
CPC分类号： F04D29/403 , F04D29/4206 , F04D29/441 , F05D2250/52
摘要： A scroll structure of a centrifugal compressor 1 having a spirally formed scroll passage 13. The scroll passage 13 includes: a flat connecting portion A at a flow passage joint 23 where a scroll start and a scroll end of the scroll passage 13 meet, this flat connecting portion having a flat cross-sectional shape with a same height as that of an outlet passage of a diffuser; and a transition part 21 where the flat cross-sectional shape of the flat connecting portion A gradually changes back to a circular cross-sectional shape along a circumferential direction.
摘要翻译：具有螺旋形涡旋通道13的离心式压缩机1的涡旋结构。涡旋通道13包括：涡卷通道13的涡卷起动和涡旋端相交的流动通道接头23处的平坦连接部分A，连接部分具有与扩散器的出口通道相同的高度的平坦的横截面形状; 以及平坦连接部A的扁平截面形状沿圆周方向逐渐变回到圆形截面形状的过渡部21。

8. 发明申请

US20140090375A1 COOLING STRUCTURE OF BEARING HOUSING FOR TURBOCHARGER 有权
标题翻译：滚动轴承轴承冷却结构
公开(公告)号：US20140090375A1
公开(公告)日：2014-04-03
申请号：US14117795
申请日：2012-06-22
申请人： Tadashi Kanzaka , Kenichiro Iwakiri , Hiroshi Ogita
发明人： Tadashi Kanzaka , Kenichiro Iwakiri , Hiroshi Ogita
IPC分类号： F01D25/12 , F02B39/00
CPC分类号： F01D25/125 , F01D25/14 , F02B39/005 , F05D2220/40 , F05D2260/232
摘要： It is intended to provide a cooling structure for a bearing housing for a turbocharger, the cooling structure being configured so that the cooling structure is manufactured with improved productivity, the occurrence of heat soak-back is reduced, and the cooling structure has improved cooling performance. The cooling structure is configured to cool both a bearing housing 13 and a bearing 52 by cooling water flowing through an annular cooling water path 13f formed in the bearing housing 13, and is provided with: a water path inlet 13h for supplying the cooling water and a water path outlet 13j for discharging the cooling water, which are provided in the bearing housing 13 so as to communicate with the annular cooling water path 13f and a partial partition 14a in the bearing housing 13 to partially close a water path which forms the shortest route between the water path inlet 13h and the water path outlet 13j.
摘要翻译：旨在提供一种用于涡轮增压器的轴承壳体的冷却结构，该冷却结构被构造成使得冷却结构以提高的生产率制造，减少了热吸收的发生，并且冷却结构具有改善的冷却性能。冷却结构通过冷却流过形成在轴承箱13中的环形冷却水路13f的水而冷却轴承壳体13和轴承52，并且设置有：用于供给冷却水的水路入口13h，用于排出冷却水的水路出口13j，其设置在轴承壳体13中以与环形冷却水路径13f连通，并且在轴承箱13中与部分隔板14a连通，以部分地闭合形成最短的水路水路入口13h与水路出口13j之间的路线。

9. 发明授权

US06652962B1 Resin-coated composite foil, production and use thereof 失效
标题翻译：树脂复合箔，其生产和使用
公开(公告)号：US06652962B1
公开(公告)日：2003-11-25
申请号：US09320765
申请日：1999-05-27
申请人： Tetsuro Sato , Tsutomu Asai , Kenichiro Iwakiri
发明人： Tetsuro Sato , Tsutomu Asai , Kenichiro Iwakiri
IPC分类号： B32B736
CPC分类号： B32B15/092 , B32B15/08 , B32B15/20 , B32B27/26 , B32B27/285 , B32B27/286 , B32B27/306 , B32B27/38 , B32B27/42 , B32B2311/12 , B32B2363/00 , B32B2457/08 , H05K3/025 , H05K2201/0358 , Y10S428/901 , Y10T428/12903 , Y10T428/2839 , Y10T428/31529
摘要： The invention provides a resin-coated composite foil characterized in that an organic insulating layer is disposed on an ultra-thin copper foil is disposed on a supporting metal layer through an intermediate organic release layer. The resin-coated composite foil is free from the peeling or blistering between the supporting metal foil and the ultra-thin copper foil during the production of a copper clad laminate.
摘要翻译：本发明提供了一种树脂涂覆复合箔，其特征在于，通过中间有机剥离层将超薄铜箔上的有机绝缘层设置在支撑金属层上。在制造覆铜层压板期间，树脂涂覆的复合箔在支撑金属箔和超薄铜箔之间没有剥离或起泡。

10. 发明授权

US09562541B2 Scroll structure of centrifugal compressor 有权
标题翻译：离心压缩机的涡旋结构
公开(公告)号：US09562541B2
公开(公告)日：2017-02-07
申请号：US13981042
申请日：2012-01-27
申请人： Kenichiro Iwakiri , Isao Tomita , Takashi Shiraishi
发明人： Kenichiro Iwakiri , Isao Tomita , Takashi Shiraishi
IPC分类号： F04D29/42 , F04D29/44 , F04D29/66
CPC分类号： F04D29/44 , F04D29/4206 , F04D29/441 , F04D29/667 , F05D2250/52
摘要： An axial cross-sectional shape of a scroll flow path 13 is a roughly circular shape, a diffuser outlet connected to the roughly circular shape is shifted to a position which is closer to a circle center than to a position of a tangent line to the circular shape and which does not reach the circle center, the circular shape is formed from a scroll chamber 30 which juts out in the axial direction relative to the position of the diffuser outlet 11a and a shift chamber 32 that forms a remainder of the roughly circular shape in a direction opposite to the scroll chamber 30, and the shift chamber 32 is at least formed on the scroll flow path 13 of a winding end portion 19 in a circumferential direction of a spiral.
摘要翻译：涡旋流路13的轴向截面形状为大致圆形，与大致圆形形状连接的扩散器出口偏移到比圆心更接近圆心的位置，而与圆形切线相对的位置形状并且不到达圆心，圆形形状由相对于扩散器出口11a的位置沿轴向突出的涡旋室30和形成大致圆形形状的剩余部分的换档室32形成在与涡旋室30相反的方向上，变速室32至少形成在螺旋的圆周方向上的卷绕端部19的涡旋流路13上。

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