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1. 发明授权

US09234440B2 Structure for gas turbine casing 有权
标题翻译：燃气轮机外壳结构
公开(公告)号：US09234440B2
公开(公告)日：2016-01-12
申请号：US13383637
申请日：2010-09-09
申请人： Yukihiro Hashimoto , Shinya Hashimoto
发明人： Yukihiro Hashimoto , Shinya Hashimoto
IPC分类号： F01D25/24
CPC分类号： F01D25/243 , F05D2240/55 , F05D2260/941
摘要： A structure for a gas turbine casing, capable of preventing gas from leaking when the structure is subjected to pressure. A structure for a gas turbine casing, divided by a horizontal plane at flange sections into two halves comprising an upper-half casing (10) and a lower-half casing (11). The structure is provided with bolts (12) which are disposed in the inner surfaces of the upper-half casing (10) and the lower-half casing (11) so as to bridge therebetween, upper nuts (13) which are disposed in the inner surface of the upper-half casing (10) and attached to the bolts (12), and lower nuts (14) which are disposed in the inner surface of the lower-half casing (11) and attached to the bolts (12).
摘要翻译：一种用于燃气轮机壳体的结构，能够防止当结构受到压力时气体泄漏。一种用于燃气涡轮机壳体的结构，其由凸缘部分处的水平面划分为包括上半壳体（10）和下半壳体（11）的两半。该结构设置有螺栓（12），其设置在上半壳体（10）和下半壳体（11）的内表面中以便在其之间桥接，上螺母（13）设置在上半壳体（10）的内表面并附接到螺栓（12），下螺母（14）设置在下半壳体（11）的内表面中并附接到螺栓（12）上，。

2. 发明申请

US20120163963A1 STRUCTURE FOR GAS TURBINE CASING 有权
标题翻译：燃气轮机结构
公开(公告)号：US20120163963A1
公开(公告)日：2012-06-28
申请号：US13383637
申请日：2010-09-09
申请人： Yukihiro Hashimoto , Shinya Hashimoto
发明人： Yukihiro Hashimoto , Shinya Hashimoto
IPC分类号： F01D25/24
CPC分类号： F01D25/243 , F05D2240/55 , F05D2260/941
摘要： A structure for a gas turbine casing, capable of preventing gas from leaking when the structure is subjected to pressure. A structure for a gas turbine casing, divided by a horizontal plane at flange sections into two halves comprising an upper-half casing (10) and a lower-half casing (11). The structure is provided with bolts (12) which are disposed in the inner surfaces of the upper-half casing (10) and the lower-half casing (11) so as to bridge therebetween, upper nuts (13) which are disposed in the inner surface of the upper-half casing (10) and attached to the bolts (12), and lower nuts (14) which are disposed in the inner surface of the lower-half casing (11) and attached to the bolts (12).
摘要翻译：一种用于燃气轮机壳体的结构，能够防止当结构受到压力时气体泄漏。一种用于燃气涡轮机壳体的结构，其由凸缘部分处的水平面划分为包括上半壳体（10）和下半壳体（11）的两半。该结构设置有螺栓（12），其设置在上半壳体（10）和下半壳体（11）的内表面中以便在其之间桥接，上螺母（13）设置在上半壳体（10）的内表面并附接到螺栓（12），下螺母（14）设置在下半壳体（11）的内表面中并附接到螺栓（12）上，。

3. 发明申请

US20110268533A1 BOLT AND MANUFACTURING METHOD OF BOLT 有权
标题翻译：螺栓的螺栓和制造方法
公开(公告)号：US20110268533A1
公开(公告)日：2011-11-03
申请号：US13178928
申请日：2011-07-08
申请人： Norikazu TEZUKA , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
发明人： Norikazu TEZUKA , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
IPC分类号： F16B35/04 , C21D7/06
CPC分类号： B24C1/10 , B23G9/001 , B23P9/04 , B23P15/00 , C21D9/0093 , F01D5/066 , F05D2230/311 , F05D2230/90 , F05D2260/941 , F05D2300/211 , F05D2300/2112 , F05D2300/2261 , F16B33/06 , Y10T29/479
摘要： A bolt has a male screw with a surface hardening portion that has an increased surface hardness and that is applied with a compressive residual stress. The male screw is formed by cutting the bolt, and performing a process to provide at least on the surface of the male screw of the bolt the surface hardening portion that has increased hardness and that is applied with a compressive residual stress. As a result, the fatigue resistance of the male screw is improved and the bolt is effective for use in a portion where the male screw is subject to a repetitive stress.
摘要翻译：螺栓具有具有表面硬化部分的外螺纹，其具有增加的表面硬度并且施加有压缩残余应力。通过切割螺栓形成外螺纹，并且执行至少在螺栓的外螺纹的表面上提供具有增加的硬度并施加有压缩残余应力的表面硬化部的工艺。结果，提高了外螺纹的耐疲劳性，并且螺栓对于使用阳螺纹受到重复应力的部分是有效的。

4. 发明授权

US06196798B1 Gas turbine cooling blade 有权
标题翻译：燃气轮机冷却叶片
公开(公告)号：US06196798B1
公开(公告)日：2001-03-06
申请号：US09242330
申请日：1999-02-11
申请人： Hiroki Fukuno , Yasuoki Tomita , Shigeyuki Maeda , Yukihiro Hashimoto , Kiyoshi Suenaga
发明人： Hiroki Fukuno , Yasuoki Tomita , Shigeyuki Maeda , Yukihiro Hashimoto , Kiyoshi Suenaga
IPC分类号： F01D518
CPC分类号： F01D5/186 , F01D5/18
摘要： A number of air-transpiration holes (4) are provided at a leading edge portion (2) of a cooled blade (1). Cooling air flowing through a cooling air passage (15) formed inside of the blade blows out to the blade surface of the leading edge portion (2) of the cooled blade (1) by way of the air-transpiration holes (4), to thereby shower-head cool the surface of the leading edge portion (2). The air-transpiration holes (4) are formed so as to extend substantially orthogonal to the leading edge surface of the cooled blade (1) such that the acute-angled portions are eliminated, whereby thermal stress is reduced and cracking is prevented.
摘要翻译：在冷却叶片（1）的前缘部分（2）处设置有多个空气蒸发孔（4）。流过形成在叶片内的冷却风道（15）的冷却空气通过空气蒸发孔（4）吹向冷却叶片（1）的前缘部（2）的叶片表面，至从而喷淋头对前缘部分（2）的表面进行冷却。空气蒸发孔（4）形成为基本上垂直于冷却叶片（1）的前缘表面延伸，使得锐角部分被消除，从而减少热应力并防止开裂。

5. 发明授权

US6151881A Air separator for gas turbines 有权
标题翻译：燃气轮机气分离器
公开(公告)号：US6151881A
公开(公告)日：2000-11-28
申请号：US242293
申请日：1999-02-11
申请人： Toshishige Ai , Yoichi Iwasaki , Sunao Aoki , Yukihiro Hashimoto , Kiyoshi Suenaga
发明人： Toshishige Ai , Yoichi Iwasaki , Sunao Aoki , Yukihiro Hashimoto , Kiyoshi Suenaga
IPC分类号： F01D5/08 , F01D11/02 , B63H1/14
CPC分类号： F01D11/02 , F01D5/081 , F01D5/085
摘要： An air separator for a gas turbine, in which cracks are prevented from occurring at a flange portion of the air separator due to fretting fatigue. The air separator (20) has a cylindrical split structure formed by two separator members (20-1 and 20-2), of which one of the separators (20-1) is mounted on a rotor (1) whereas the other separator member (20-2) is mounted on a disc portion (7) on a side of a moving blade (2) by bolts (28) extending through bolt holes (23) formed in a flange portion (22). Cooling air from a compressor enters a space (6) from a duct (5) and passes to a passage (32) from a clearance (33) so that it is fed to air feed holes (43) and radial holes (44) of the disc portion (7). Alternatively, air holes (50) are provided in the flange portion (22) in the form of circumferential slots for covering a plurality of radial holes to feed the cooling air homogeneously so that a prior art air separator of an existing plant can be replaced.
摘要翻译： PCT No.PCT / JP98 / 02688 Sec。 371日期1999年2月11日 102（e）1999年2月11日PCT PCT。1998年6月18日PCT公布。公开号WO98 / 59156 日期：1998年12月30日在燃气轮机的空气分离器中，由于微动疲劳，防止在空气分离器的凸缘部发生裂纹。空气分离器（20）具有由两个分离器构件（20-1和20-2）形成的圆柱形分离结构，其中一个分离器（20-1）安装在转子（1）上，而另一个分隔件（20-2）通过延伸穿过形成在凸缘部分（22）中的螺栓孔（23）的螺栓（28）安装在活动叶片（2）侧上的盘部分（7）上。来自压缩机的冷却空气从管道（5）进入空间（6）并从间隙（33）传递到通道（32），从而将其供给到空气供给孔（43）和径向孔盘部（7）。或者，空气孔（50）以周向槽的形式设置在凸缘部分（22）中，用于覆盖多个径向孔，以均匀地供给冷却空气，使得可以更换现有设备的现有技术的空气分离器。

6. 发明授权

US08607604B2 Bolt and manufacturing method of bolt 有权
标题翻译：螺栓螺栓和制造方法
公开(公告)号：US08607604B2
公开(公告)日：2013-12-17
申请号：US13178928
申请日：2011-07-08
申请人： Norikazu Tezuka , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
发明人： Norikazu Tezuka , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
IPC分类号： C21D7/06
CPC分类号： B24C1/10 , B23G9/001 , B23P9/04 , B23P15/00 , C21D9/0093 , F01D5/066 , F05D2230/311 , F05D2230/90 , F05D2260/941 , F05D2300/211 , F05D2300/2112 , F05D2300/2261 , F16B33/06 , Y10T29/479
摘要： A bolt has a male screw with a surface hardening portion that has an increased surface hardness and that is applied with a compressive residual stress. The male screw is formed by cutting the bolt, and performing a process to provide at least on the surface of the male screw of the bolt the surface hardening portion that has increased hardness and that is applied with a compressive residual stress. As a result, the fatigue resistance of the male screw is improved and the bolt is effective for use in a portion where the male screw is subject to a repetitive stress.
摘要翻译：螺栓具有具有表面硬化部分的外螺纹，其具有增加的表面硬度并且施加有压缩残余应力。通过切割螺栓形成外螺纹，并且执行至少在螺栓的外螺纹的表面上提供具有增加的硬度并施加有压缩残余应力的表面硬化部的工艺。结果，提高了外螺纹的耐疲劳性，并且螺栓对于使用阳螺纹受到重复应力的部分是有效的。

7. 发明授权

US06261058B1 Stationary blade of integrated segment construction and manufacturing method therefor 有权
标题翻译：固定叶片综合分段施工及其制造方法
公开(公告)号：US06261058B1
公开(公告)日：2001-07-17
申请号：US09414394
申请日：1999-10-07
申请人： Masahito Kataoka , Masao Terazaki , Yukihiro Hashimoto
发明人： Masahito Kataoka , Masao Terazaki , Yukihiro Hashimoto
IPC分类号： F01D900
CPC分类号： F01D9/042 , F01D5/288 , F01D9/041 , F05D2230/00 , F05D2230/90 , F05D2240/12 , F05D2260/30 , F05D2300/611
摘要： The present invention provides a stationary blade of integrated segment construction, in which a thermal barrier coating can be applied to the whole blade surface and excessive stress can be avoided in a shroud. A plate seat connector is provided at each end face portion of an inside shroud and an outside shroud attached to outside and inside ends of gas turbine stationary blade. Several stationary blades are integrated by joining the plate seat connectors of the adjacent shrouds by means of bolts and nuts to provide a stationary blade of integrated segment construction.
摘要翻译：本发明提供了一种集成节段结构的固定叶片，其中可以对整个叶片表面施加热障涂层，并且可以避免在护罩中产生过大的应力。在内侧护罩的每个端面部分设置有板座连接器，以及安装在燃气轮机静止叶片的外部和内部端部的外部护罩。通过用螺栓和螺母连接相邻护罩的板座连接器来集成几个固定刀片，以提供一体化段结构的固定刀片。

8. 发明授权

US5947687A Gas turbine moving blade 失效
标题翻译：燃气轮机动叶片
公开(公告)号：US5947687A
公开(公告)日：1999-09-07
申请号：US862135
申请日：1997-05-22
申请人： Masahiko Mori , Yukihiro Hashimoto , Hiroji Tada , Ichiro Fukue , Keizo Tsukagoshi , Jyunichiro Masada
发明人： Masahiko Mori , Yukihiro Hashimoto , Hiroji Tada , Ichiro Fukue , Keizo Tsukagoshi , Jyunichiro Masada
IPC分类号： F01D5/18 , F01D5/14
CPC分类号： F01D5/147 , F05D2260/94 , F05D2260/941 , Y02T50/671
摘要： A movable gas turbine blade includes a platform (10) which is provided with a groove (15). The groove is located on a blade trailing side of the platform. Also, the groove is rounded and has a depth which does not enter a stress line of the platform caused by a load on the blade. The groove functions to suppress a high thermal stress arising at a connection portion of a blade trailing edge and the platform of the gas turbine air cooled moving blade during unsteady (start and stop) operation of the turbine.
摘要翻译：可移动燃气轮机叶片包括具有凹槽（15）的平台（10）。凹槽位于平台的叶片后侧。此外，凹槽是圆形的并且具有不会由叶片上的载荷引起的平台的压力线的深度。该凹槽用于在涡轮的不稳定（启动和停止）操作期间抑制在叶片后缘的连接部分和燃气轮机空气冷却的动叶片的平台处产生的高热应力。

9. 发明申请

US20090003968A1 Bolt and Manufacturing Method of Bolt 审中-公开
标题翻译：螺栓螺栓和制造方法
公开(公告)号：US20090003968A1
公开(公告)日：2009-01-01
申请号：US12087603
申请日：2007-01-25
申请人： Norikazu Tezuka , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
发明人： Norikazu Tezuka , Kazuharu Hirokawa , Keisuke Ihara , Kei Osawa , Hiroshi Ishikawa , Taiji Torigoe , Ryuichi Yamamoto , Yukihiro Hashimoto , Nobuyuki Izutsu , Koji Takahashi
IPC分类号： F16B33/06 , B21K1/56 , B24C1/10 , B23G9/00
CPC分类号： B24C1/10 , B23G9/001 , B23P9/04 , B23P15/00 , C21D9/0093 , F01D5/066 , F05D2230/311 , F05D2230/90 , F05D2260/941 , F05D2300/211 , F05D2300/2112 , F05D2300/2261 , F16B33/06 , Y10T29/479
摘要： The present invention provides a surface hardening portion 11 that has increased surface hardness and that is applied with a compressive residual stress, at least on the surface of a male screw 10 of a bolt 1. The present invention includes the steps of cutting to form the male screw 10 of the bolt 1, and processing to provide at least on the surface of the male screw 10 of the bolt 1 the surface hardening portion 11 that has increased hardness and that is applied with a compressive residual stress. As a result, the present invention can improve the fatigue resistance of the male screw 10 and the bolt is effective as a bolt to be used in a portion where the male screw 10 is subject to a repetitive stress.
摘要翻译：本发明提供了至少在螺栓1的外螺纹10的表面上具有增加的表面硬度并施加压缩残余应力的表面硬化部分11.本发明包括以下步骤：切割以形成螺栓1的外螺纹10，并且至少在螺栓1的外螺纹10的表面上提供具有增加的硬度并施加有压缩残余应力的表面硬化部11的处理。结果，本发明可以提高外螺纹10的耐疲劳性，螺栓作为在阳螺纹10受到重复应力的部分使用的螺栓是有效的。

10. 发明申请

US20080078490A1 PNEUMATIC RADIAL TIRE 审中-公开
标题翻译：气动辐射轮胎
公开(公告)号：US20080078490A1
公开(公告)日：2008-04-03
申请号：US11863576
申请日：2007-09-28
申请人： Yukihiro Hashimoto
发明人： Yukihiro Hashimoto
IPC分类号： B60C15/06
CPC分类号： B60C9/0007 , B60C9/0064 , B60C9/20 , Y10T152/10837
摘要： A pneumatic radial tire, comprising: a carcass toroidally extending across between a pair of bead cores; an outer side belt layer provided outside of the carcass in a radial direction, in which a plurality of cords extending in a direction inclined with respect to a tire equatorial plane are buried in covering rubber; an inner side belt layer provided between the outer side belt layer and the carcass, in which a plurality of cords, made of the same material as that of the cords of the outer side belt layer, and extending in a direction crossing the cords of the outer side belt layer, are buried in covering rubber; and a tread provided outside of the outer side belt layer in the radial direction; wherein a total strength of the outer side belt layer is larger than a total strength of the inner side belt layer, is provided.
摘要翻译：一种充气子午线轮胎，包括：在一对胎圈芯之间跨越延伸的胎体; 外侧带束层设置在胎体的径向外侧，其中沿相对于轮胎赤道面倾斜的方向延伸的多根绳索被埋在覆盖橡胶中; 设置在所述外侧带束层与胎体之间的内侧带束层，其中由与所述外侧带束层的帘线相同的材料制成的多根帘线沿与所述外侧带束层的帘线相交的方向延伸，外侧带层，埋在覆盖橡胶中; 以及设置在所述外侧带束层的径向外侧的胎面; 其中外侧带层的总强度大于内侧带束层的总强度。

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