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1. 发明授权

US07165943B2 Geothermal turbine 有权
公开(公告)号：US07165943B2
公开(公告)日：2007-01-23
申请号：US10928212
申请日：2004-08-30
申请人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
发明人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
IPC分类号： F01D5/22
CPC分类号： F01D11/08 , F01D5/225 , F01D5/288 , F01D9/02 , F01D11/001 , F01D11/02 , F01D17/145 , F02C1/05 , F05D2220/31 , F05D2230/232 , F05D2230/90 , F05D2250/182 , F05D2260/607 , F05D2300/611 , Y02T50/673 , Y02T50/675
摘要： A geothermal turbine comprises a turbine casing, a turbine rotor shaft, a plurality of nozzle diaphragm outer rings fixed to the turbine casing, a plurality of nozzle diaphragm inner rings located radially inside the nozzle diaphragm outer rings, a plurality of nozzles placed between the nozzle diaphragm outer rings and the nozzle diaphragm inner rings, which form a steam passage, a plurality of rotor blades mounted on the turbine rotor shaft, which face the nozzles and form a blade cascade in a circumferential direction, a shroud arranged on tip of the rotor blade, an overhang attached to the nozzle diaphragm outer ring, which extends downstream of the nozzles and has an inner surface facing radially outside the shroud, and a plurality of sealing fins which protrude radially outward from the shroud and face the overhang.

2. 发明申请

US20070224037A1 Geothermal turbine 审中-公开
标题翻译：地热涡轮机
公开(公告)号：US20070224037A1
公开(公告)日：2007-09-27
申请号：US11642829
申请日：2006-12-21
申请人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
发明人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
IPC分类号： F03B11/00
CPC分类号： F01D11/08 , F01D5/225 , F01D5/288 , F01D9/02 , F01D11/001 , F01D11/02 , F01D17/145 , F02C1/05 , F05D2220/31 , F05D2230/232 , F05D2230/90 , F05D2250/182 , F05D2260/607 , F05D2300/611 , Y02T50/673 , Y02T50/675
摘要： A geothermal turbine comprises a turbine casing, a turbine rotor shaft, a plurality of nozzle diaphragm outer rings fixed to the turbine casing, a plurality of nozzle diaphragm inner rings located radially inside the nozzle diaphragm outer rings, a plurality of nozzles placed between the nozzle diaphragm outer rings and the nozzle diaphragm inner rings, which form a steam passage, a plurality of rotor blades mounted on the turbine rotor shaft, which face the nozzles and form a blade cascade in a circumferential direction, a shroud arranged on tip of the rotor blade, an overhang attached to the nozzle diaphragm outer ring, which extends downstream of the nozzles and has an inner surface facing radially outside the shroud, and a plurality of sealing fins which protrude radially outward from the shroud and face the overhang.
摘要翻译：地热涡轮机包括涡轮机壳体，涡轮转子轴，固定到涡轮机壳体的多个喷嘴隔膜外环，位于喷嘴隔膜外环径向内侧的多个喷嘴隔膜内圈，多个喷嘴，位于喷嘴隔膜外圈和形成蒸汽通道的喷嘴隔膜内圈，安装在涡轮转子轴上的多个转子叶片，其面对喷嘴并在圆周方向上形成叶片级联;罩体，布置在转子的顶端叶片，附着在喷嘴隔膜外环上的悬臂，其延伸到喷嘴的下游并且具有面向径向外侧的内表面，以及多个从护罩径向向外突出并面向突出端的密封翅片。

3. 发明授权

US06860718B2 Geothermal turbine 有权
标题翻译：地热涡轮机
公开(公告)号：US06860718B2
公开(公告)日：2005-03-01
申请号：US10351613
申请日：2003-01-27
申请人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
发明人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
IPC分类号： B23K9/00 , B23K9/04 , B23K10/02 , B23K35/30 , B23K35/32 , C22C14/00 , C22C19/00 , C22C32/00 , C22C38/00 , C23C4/04 , C23C4/08 , F01D5/06 , F01D5/20 , F01D5/22 , F01D5/28 , F01D9/04 , F01D11/02 , F01D11/08 , F03G4/00
CPC分类号： F01D11/08 , F01D5/225 , F01D5/288 , F01D9/02 , F01D11/001 , F01D11/02 , F01D17/145 , F02C1/05 , F05D2220/31 , F05D2230/232 , F05D2230/90 , F05D2250/182 , F05D2260/607 , F05D2300/611 , Y02T50/673 , Y02T50/675
摘要： A geothermal turbine comprises a turbine casing, a turbine rotor shaft, a plurality of nozzle diaphragm outer rings fixed to the turbine casing, a plurality of nozzle diaphragm inner rings located radially inside the nozzle diaphragm outer rings, a plurality of nozzles placed between the nozzle diaphragm outer rings and the nozzle diaphragm inner rings, which form a steam passage, a plurality of rotor blades mounted on the turbine rotor shaft, which face the nozzles and form a blade cascade in a circumferential direction, a shroud arranged on tip of the rotor blade, an overhang attached to the nozzle diaphragm outer ring, which extends downstream of the nozzles and has an inner surface facing radially outside the shroud, and a plurality of sealing fins which protrude radially outward from the shroud and face the overhang.
摘要翻译：地热涡轮机包括涡轮机壳体，涡轮转子轴，固定到涡轮机壳体的多个喷嘴隔膜外环，位于喷嘴隔膜外环径向内侧的多个喷嘴隔膜内圈，多个喷嘴，位于喷嘴隔膜外圈和形成蒸汽通道的喷嘴隔膜内圈，安装在涡轮转子轴上的多个转子叶片，其面对喷嘴并在圆周方向上形成叶片级联;罩体，布置在转子的顶端叶片，附着在喷嘴隔膜外环上的悬臂，其延伸到喷嘴的下游并且具有面向径向外侧的内表面，以及多个从护罩径向向外突出并面向突出端的密封翅片。

4. 发明申请

US20050025617A1 Geothermal turbine 有权
公开(公告)号：US20050025617A1
公开(公告)日：2005-02-03
申请号：US10928212
申请日：2004-08-30
申请人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
发明人： Atsuhide Suzuki , Toshihiro Fujiwara , Masataka Fukuda , Kazuaki Ikeda , Toshihiro Matsuura , Osamu Watanabe , Hisao Fujihashi , Kentaro Takagi
IPC分类号： B23K9/00 , B23K9/04 , B23K10/02 , B23K35/30 , B23K35/32 , C22C14/00 , C22C19/00 , C22C32/00 , C22C38/00 , C23C4/04 , C23C4/08 , F01D5/06 , F01D5/20 , F01D5/22 , F01D5/28 , F01D9/04 , F01D11/02 , F01D11/08 , F03G4/00
CPC分类号： F01D11/08 , F01D5/225 , F01D5/288 , F01D9/02 , F01D11/001 , F01D11/02 , F01D17/145 , F02C1/05 , F05D2220/31 , F05D2230/232 , F05D2230/90 , F05D2250/182 , F05D2260/607 , F05D2300/611 , Y02T50/673 , Y02T50/675
摘要： A geothermal turbine comprises a turbine casing, a turbine rotor shaft, a plurality of nozzle diaphragm outer rings fixed to the turbine casing, a plurality of nozzle diaphragm inner rings located radially inside the nozzle diaphragm outer rings, a plurality of nozzles placed between the nozzle diaphragm outer rings and the nozzle diaphragm inner rings, which form a steam passage, a plurality of rotor blades mounted on the turbine rotor shaft, which face the nozzles and form a blade cascade in a circumferential direction, a shroud arranged on tip of the rotor blade, an overhang attached to the nozzle diaphragm outer ring, which extends downstream of the nozzles and has an inner surface facing radially outside the shroud, and a plurality of sealing fins which protrude radially outward from the shroud and face the overhang.

5. 发明授权

US5511948A Rotor blade damping structure for axial-flow turbine 失效
标题翻译：轴流式涡轮转子叶片阻尼结构
公开(公告)号：US5511948A
公开(公告)日：1996-04-30
申请号：US320545
申请日：1994-10-11
申请人： Atsuhide Suzuki , Hirotsugu Kodama , Toshio Suzuki
发明人： Atsuhide Suzuki , Hirotsugu Kodama , Toshio Suzuki
IPC分类号： F01D5/26 , F01D5/22 , F01D5/30 , F01D5/32 , F03G4/00
CPC分类号： F01D5/3046 , F01D5/225
摘要： In an axial-flow turbine, at least one of front and rear side contact surfaces of shrouds (3a or 3b) of blades (1a or 1b) with respect to the turbine rotational direction is formed at certain angle with respect to a radial line connecting the rotor center and the contact surface. The shroud (3a) of the blade (1a) of a first kind is formed in a trapezoidal shape converging radially outward in cross section taken in a plane perpendicular to the turbine axial direction, and the shroud (3b) of the blade (1b) of a second kind is formed in an inverted trapezoidal shape converging radially inward in the cross section. Further, half of an angle (2.alpha.) between the front and rear side contact surfaces of the shrouds (3a or 3b) is made smaller than a static frictional angle of the contact surface. Since the shroud contact surfaces of two adjacent blades can be kept in pressure contact with each other under all operating conditions, a large dynamic stress reduction and superior damping properties can be obtained without producing excessive initial stresses at the blade airfoil and blade dovetail attachment portion.
摘要翻译：在轴流涡轮机中，相对于涡轮机旋转方向，叶片（1a或1b）的护罩（3a或3b）的前后侧接触表面中的至少一个相对于连接到涡轮机的径向线形成一定角度转子中心和接触面。第一种叶片（1a）的护罩（3a）形成为在垂直于涡轮轴线方向的平面截取的横截面中径向向外收敛的梯形形状，并且叶片（1b）的护罩（3b）第二种形式在横截面中以径向向内收敛的倒梯形形状。此外，使护罩（3a或3b）的前侧和后侧接触表面之间的角度（2α）的一半被制成小于接触表面的静摩擦角。由于两个相邻叶片的护罩接触表面可以在所有操作条件下彼此保持压力接触，所以可以获得大的动态应力减小和优异的阻尼性能，而不会在叶片翼型和叶片燕尾形连接部分处产生过大的初始应力。

6. 发明授权

US5841231A Photomultiplier having lamination structure of fine mesh dynodes 失效
标题翻译：具有细网络倍增电极层叠结构的光电倍增管
公开(公告)号：US5841231A
公开(公告)日：1998-11-24
申请号：US649305
申请日：1996-05-17
申请人： Suenori Kimura , Masuo Ito , Atsuhide Suzuki
发明人： Suenori Kimura , Masuo Ito , Atsuhide Suzuki
IPC分类号： H01J43/06 , H01J43/22 , H01J43/04
CPC分类号： H01J43/06 , H01J43/22
摘要： The present invention concerns a photomultiplier having a lamination structure of fine mesh dynodes arranged at predetermined intervals, capable of detecting photons even in a high magnetic field. This photomultiplier is arranged so that hollow pipes penetrating electrodes for supporting the fine mesh dynodes define the lamination structure of an electron multiplier unit. This arrangement permits the intervals between the fine mesh dynodes to be accurately controlled, thereby obtaining the photomultiplier production errors of which are well suppressed and preventing that the fine mesh dynodes are ripped.
摘要翻译：本发明涉及具有以预定间隔布置的细网络倍增电极的层压结构的光电倍增管，即使在高磁场中也能检测光子。该光电倍增管被布置成使得穿透用于支撑细网络倍增电极的电极的中空管限定电子倍增器单元的层叠结构。这种布置允许精细地控制细网络倍增电极之间的间隔，从而获得良好抑制的光电倍增管产生误差，并且防止细网络倍增电极被撕开。

7. 发明授权

US5388960A Forced-air cooling apparatus of steam turbine 失效
标题翻译：蒸汽轮机的强制空气冷却装置
公开(公告)号：US5388960A
公开(公告)日：1995-02-14
申请号：US131593
申请日：1993-10-05
申请人： Atsuhide Suzuki , Shinya Ayano , Yukio Shinozaki , Shigeo Hosoi
发明人： Atsuhide Suzuki , Shinya Ayano , Yukio Shinozaki , Shigeo Hosoi
IPC分类号： F01D25/12 , F01D25/26 , F01D25/34 , F01D21/00 , F01D25/08
CPC分类号： F01D25/12 , F01D25/26
摘要： A forced-air cooling apparatus is provided for a steam turbine which comprises an outer casing composed of upper and lower casing halves, an inner casing composed of upper and lower casing halves and disposed inside the outer casing and a rotor coaxially disposed inside the inner casing for forming a steam flow passage between the inner casing and the rotor and in which steam introduced into the steam flow passage from a steam inlet portion is impinged against blades of the rotor to impart a turning force thereto as a movable portion such as rotor with respect to a stationary portion such as an inner casing. The forced-air cooling apparatus comprises a cooling passage including a first cooling air passage formed between the inner casing and the rotor and a second cooling air passage formed between the outer casing and the inner casing, an external air inlet and outlet portion for charging external cooling air into the first and second cooling air passages during the turning operation period and discharging the cooling air after passing the first and second cooling air passages and a control unit for controlling the flow rate of the cooling air passing the first cooling air passage in response to a signal corresponding to a differential expansion detected by a differencial expansion detector between the movable portion and the stationary portion of the turbine and controlling a flow rate of the cooling air passing the second cooling air passage in response to a signal corresponding to a temperature difference between the upper and lower casing halves of the outer casing of the turbine.
摘要翻译：一种用于蒸汽轮机的强制空气冷却装置，包括由上下半壳构成的外壳，由上下半壳构成并设置在外壳内部的内壳和同轴地设置在内壳内的转子用于在内壳和转子之间形成蒸汽流动通道，其中从蒸汽入口部分引入蒸汽流动通道的蒸汽撞击到转子的叶片上，以将作为可转动部分的转动力作为可转动部分，例如转子相对于到诸如内壳的固定部分。强制空气冷却装置包括冷却通道，其包括形成在内壳和转子之间的第一冷却空气通道和形成在外壳和内壳之间的第二冷却空气通道，外部空气入口和出口部分，用于向外部充电在转动操作期间将空气冷却到第一和第二冷却空气通道中，并且在通过第一和第二冷却空气通道之后排出冷却空气;以及控制单元，用于控制响应于通过第一冷却空气通道的冷却空气的流量对应于由可变部分和涡轮机的静止部分之间的差分膨胀检测器检测到的差动膨胀的信号，并且响应于对应于温差的信号控制通过第二冷却空气通道的冷却空气的流量在涡轮机的外壳的上半壳体和下壳体之间。

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