公开(公告)号：US5323614A

公开(公告)日：1994-06-28

申请号：US3608

申请日：1993-01-13

申请人： Satoshi Tsukahara ,  Hiroshi Inoue ,  Noriyuki Hayashi ,  Kazumi Iwai ,  Tamio Innami ,  Yoji Ishibashi ,  Michio Kuroda ,  Yasuhiko Otawara ,  Hiraku Ikeda ,  Kazuyuki Itoh ,  Shozo Nakamura ,  Hidekazu Fujimura ,  Kazuhito Koyama

发明人： Satoshi Tsukahara ,  Hiroshi Inoue ,  Noriyuki Hayashi ,  Kazumi Iwai ,  Tamio Innami ,  Yoji Ishibashi ,  Michio Kuroda ,  Yasuhiko Otawara ,  Hiraku Ikeda ,  Kazuyuki Itoh ,  Shozo Nakamura ,  Hidekazu Fujimura ,  Kazuhito Koyama

IPC分类号： F02C9/28 ,  F23R3/28 ,  F23R3/34 ,  F02C1/00

CPC分类号： F23R3/286 ,  F23R3/34

摘要： A premixed combustor for a gas turbine, comprises, a combustion chamber for burning a fuel with an air therein, at least two premixed fuel/air mixture outlets which are juxtaposed with each other, and through each of which a premixed fuel/air mixture flows out into the combustion chamber, and a flow deflection member arranged between the premixed fuel/air mixture outlets, urging the permixed fuel/air mixture from one of the premixed fuel/air mixture outlets to go away from another one of the premixed fuel/air mixture outlets, and terminating in the combustion chamber so that the premixed fuel/air mixture from the one of the premixed fuel/air mixture outlets is permitted to move toward the premixed fuel/air mixture flowing out from the another one of the premixed fuel/air mixture outlets after going away from the another one of the premixed fuel/air mixture outlets.

摘要翻译： 一种用于燃气轮机的预混合燃烧器包括：用于燃烧燃料的燃烧室，其中具有空气的至少两个预混合燃料/空气混合物出口彼此并置，并且通过其中预混燃料/空气混合物流动 并且设置在预混燃料/空气混合物出口之间的流动偏转构件，从预混合的燃料/空气混合物出口之一推动经过混合的燃料/空气混合物以远离另一种预混燃料/空气 混合物出口，并且终止于燃烧室，使得来自预混燃料/空气混合物出口之一的预混合燃料/空气混合物被允许朝向从另一个预混燃料/空气混合物出口流出的预混燃料/空气混合物移动， 在离开另一个预混合燃料/空气混合物出口之后的空气混合物出口。

公开(公告)号：US5319936A

公开(公告)日：1994-06-14

申请号：US948225

申请日：1992-09-21

申请人： Hiraku Ikeda ,  Michio Kuroda ,  Nobuyuki Iizuka ,  Yasutaka Komatsu ,  Isao Sato ,  Masayuki Taniguchi ,  Yasuhiko Ootawara ,  Noriyuki Hayashi

发明人： Hiraku Ikeda ,  Michio Kuroda ,  Nobuyuki Iizuka ,  Yasutaka Komatsu ,  Isao Sato ,  Masayuki Taniguchi ,  Yasuhiko Ootawara ,  Noriyuki Hayashi

IPC分类号： F23R3/18 ,  F23D23/00 ,  F23R3/28 ,  F23R3/32 ,  F23R3/34 ,  F23R3/20

CPC分类号： F23R3/286 ,  F23D23/00 ,  F23R3/34

摘要： First and second premixed burners having annular injection slots are concentrically adjacent and the injection slots are substantially aligned with each other in a longitudinal direction of the burners. A pilot burner is provided substantially in the center of the annular first premixed burner so that the injection slot of the pilot burner is substantially aligned with the injection slot of the first premixed burner in a longitudinal direction of the burner. A flame holder which forms a circulating flow of combusted gas Gh downstream of the flame holder is disposed at the downstream end of a boundary wall between the premixed burners so that the flame holder is co-used by the premixed burners. Flow rate adjusting means for adjusting the flow rate of fuel supplied to the first, second premixed burner and the pilot burner, respectively are provided. The fuel can be substantially uniformly mixed with a combustion gas. Reduction in NOx and stabilization of premixed flame can be achieved.

摘要翻译： 具有环形注入槽的第一和第二预混合燃烧器同心地相邻并且喷射槽在燃烧器的纵向方向上彼此基本对齐。 主要燃烧器基本上设置在环形第一预混合燃烧器的中心，使得引燃燃烧器的喷射槽在燃烧器的纵向方向上基本上与第一预混燃烧器的喷射槽对准。 形成火焰保持器下游的燃烧气体Gh的循环流的火焰保持器设置在预混合燃烧器之间的边界壁的下游端，使得火焰保持器由预混燃烧器共同使用。 提供了用于分别调节供应到第一，第二预混合燃烧器和引燃燃烧器的燃料的流量的流量调节装置。 燃料可以与燃烧气体基本均匀地混合。 可以实现NOx的还原和预混火焰的稳定化。

公开(公告)号：US4603548A

公开(公告)日：1986-08-05

申请号：US647658

申请日：1984-09-06

申请人： Yoji Ishibashi ,  Isao Sato ,  Fumio Kato ,  Takashi Ohmori ,  Noriyuki Hayashi

发明人： Yoji Ishibashi ,  Isao Sato ,  Fumio Kato ,  Takashi Ohmori ,  Noriyuki Hayashi

IPC分类号： F02C7/22 ,  F02C9/28 ,  F23N1/00 ,  F23R3/28 ,  F23R3/34 ,  F02C9/00

CPC分类号： F23R3/346 ,  F02C7/22 ,  F23R3/28

摘要： A fuel supply method for a gas turbine combustor having first and second stage combustion chambers. The method comprises supplying the fuel from only first stage fuel supply from the start of the gas turbine until its low output range so as to operate only the first stage combustion chamber, supplying the fuel from both first and second stage fuel supply in a high output range of the gas turbine including its maximum output so as to operate both first and second stage combustion chambers. The method makes it possible to reduce NO.sub.x without deteriorating the combustion performance by step-wise supplying a predetermined flow rate of the fuel when the second stage fuel is to be supplied and at the same time, step-wise reducing the same quantity of the fuel that is being supplied from the first stage fuel supply.

摘要翻译： 一种具有第一和第二级燃烧室的燃气轮机燃烧器的燃料供给方法。 该方法包括仅将燃料从燃气轮机的起始点供给燃料，直到其低的输出范围，以便仅操作第一级燃烧室，从第一和第二级燃料供应源的燃料以高输出 包括其最大输出的燃气轮机的范围，以便操作第一和第二级燃烧室。 该方法可以在不降低燃烧性能的同时，通过在供给第二级燃料时逐步提供燃料的预定流量，同时逐步减少相同量的燃料 这是从第一级燃料供应提供的。

公开(公告)号：US5343693A

公开(公告)日：1994-09-06

申请号：US947828

申请日：1992-09-21

申请人： Yasutaka Komatsu ,  Michio Kuroda ,  Yasuhiko Ootawara ,  Nobuyuki Iizuka ,  Isao Sato ,  Masayuki Taniguchi ,  Noriyuki Hayashi

发明人： Yasutaka Komatsu ,  Michio Kuroda ,  Yasuhiko Ootawara ,  Nobuyuki Iizuka ,  Isao Sato ,  Masayuki Taniguchi ,  Noriyuki Hayashi

IPC分类号： F23D14/70 ,  F23R3/22 ,  F23R3/26 ,  F23R3/28 ,  F23R3/32 ,  F23C3/00

CPC分类号： F23R3/26 ,  F23D14/70 ,  F23R3/22 ,  F23D2209/20

摘要： A combustor comprises a passage area changing mechanism which relatively moves a flame holder relative to a premixed combustion nozzle in an axial direction so that the area of passage for premixed gas between an injection edge of the premixed combustion nozzle and a peripheral edge of the flame holder can be changed. Stable combustion can be maintained over a wide load range and reduction in NOx can be achieved.

摘要翻译： 燃烧器包括通道区域改变机构，该通道区域改变机构使火焰保持器相对于预混合燃烧喷嘴沿轴向方向相对移动，使得预混合燃烧喷嘴的注射边缘与火焰保持器的周边边缘之间的预混合气体的通道面积 可以改变 可以在宽的负载范围内保持稳定的燃烧，并且可以实现NOx的还原。

公开(公告)号：US5349812A

公开(公告)日：1994-09-27

申请号：US10576

申请日：1993-01-28

申请人： Masayuki Taniguchi ,  Hironobu Kobayashi ,  Kiyoshi Narato ,  Tadayoshi Murakami ,  Shigeru Azuhata ,  Michio Kuroda ,  Noriyuki Hayashi

发明人： Masayuki Taniguchi ,  Hironobu Kobayashi ,  Kiyoshi Narato ,  Tadayoshi Murakami ,  Shigeru Azuhata ,  Michio Kuroda ,  Noriyuki Hayashi

IPC分类号： F23R3/26 ,  F23R3/28 ,  F02C9/50

CPC分类号： F23R3/26

摘要： A gas turbine combustor is capable of reducing NOx over a whole load range of a gas turbine. The combustor comprises two burner systems. It is possible to independently control a flow rate of combustion air supplied to a burner of the respective systems and a flow rate of bypass air jetted from through a bypass air port. The air supplied to the burners is mixed with fuel in a mixing chamber and then ejected into a combustion chamber so as to form a flame. The amount of bypass air is controlled in accordance with an operation load, a humidity of air and a heating value of fuel. It is therefore possible to prevent any blow off and reduce NOx over the whole load range of the gas turbine.

摘要翻译： 燃气轮机燃烧器能够在燃气轮机的整个负载范围内减少NOx。 燃烧器包括两个燃烧器系统。 可以独立地控制供给到各个系统的燃烧器的燃烧空气的流量和从旁通空气口喷射的旁路空气的流量。 供给燃烧器的空气与混合室中的燃料混合，然后喷射到燃烧室中以形成火焰。 旁路空气的量根据操作负荷，空气湿度和燃料的热值来控制。 因此，可以防止在燃气轮机的整个负载范围内的任何吹出和减少NOx。

公开(公告)号：US10148141B2

公开(公告)日：2018-12-04

申请号：US14122601

申请日：2012-06-04

申请人： Yukio Yamashita ,  Noriyuki Hayashi ,  Seiichi Ibaraki ,  Katsuyuki Osako ,  Motoki Ebisu ,  Byeongil An ,  Hiroshi Suzuki ,  Hideaki Arita ,  Takashi Goto ,  Toshihiko Miyake

发明人： Yukio Yamashita ,  Noriyuki Hayashi ,  Seiichi Ibaraki ,  Katsuyuki Osako ,  Motoki Ebisu ,  Byeongil An ,  Hiroshi Suzuki ,  Hideaki Arita ,  Takashi Goto ,  Toshihiko Miyake

IPC分类号： H02K1/22 ,  F02C6/12 ,  H02K7/08 ,  H02K15/02 ,  H02K1/28 ,  H02K1/30 ,  H02K11/21

摘要： A motor rotor structure for an electric turbo charger is manufactured at low cost with good quality by fixedly fitting, over a shaft, a rotor core having electromagnetic steel sheets pre-formed as an integrated stack. The rotor structure includes a rotor core which is rotated by a magnetic field formed by a stator in a housing; a shaft configured to rotate a compressor impeller and the rotor core together; and a bearing supporting the shaft. The rotor includes the rotor core including the electromagnetic steel sheets; a stopper portion formed at an intermediate portion of the shaft to restrict axial movement of the rotor core; and a pressing unit which presses the rotor core fitted over the shaft against the stopper portion. The pressing unit prevents a circumferential phase shift between the shaft and the rotor core by a pressing force thereof.

公开(公告)号：US09726189B2

公开(公告)日：2017-08-08

申请号：US13993275

申请日：2012-02-13

申请人： Hideaki Nishida ,  Keitaro Kamata ,  Isao Tomita ,  Takashi Shiraishi ,  Noriyuki Hayashi ,  Motoki Ebisu ,  Hiroshi Suzuki ,  Hiroshi Ogita

发明人： Hideaki Nishida ,  Keitaro Kamata ,  Isao Tomita ,  Takashi Shiraishi ,  Noriyuki Hayashi ,  Motoki Ebisu ,  Hiroshi Suzuki ,  Hiroshi Ogita

IPC分类号： F04D29/05 ,  F04D29/056 ,  F16C17/18 ,  F16C43/02 ,  F16C33/10 ,  F01D25/16 ,  F01D1/24 ,  F01D25/18 ,  F16C17/02 ,  F16C17/26 ,  F16C33/14

CPC分类号： F04D29/056 ,  F01D1/24 ,  F01D25/16 ,  F01D25/162 ,  F01D25/166 ,  F01D25/186 ,  F05D2220/40 ,  F05D2250/14 ,  F05D2250/70 ,  F05D2260/96 ,  F16C17/028 ,  F16C17/18 ,  F16C17/26 ,  F16C33/1075 ,  F16C33/14 ,  F16C43/02 ,  F16C2220/40 ,  F16C2220/60 ,  F16C2220/70 ,  F16C2360/24 ,  Y10T29/49668

摘要： A turbocharger and a method of manufacturing a floating bush with which noise can be reduced, and the rotation speed can be increased. In a turbocharger in which a rotating shaft having a circular cross-section and connecting a turbine rotor and a compressor rotor is supported in a freely rotatable manner, at two axially separated positions via floating bushes, by an inner circumferential surface disposed so as to surround the rotating shaft in a bearing housing, an inner circumferential surface of each of the floating bushes has a non-circular shape in which the curvature of the cross-sectional shape varies in the circumferential direction.

公开(公告)号：US20130220285A1

公开(公告)日：2013-08-29

申请号：US13807568

申请日：2011-10-14

申请人： Noriyuki Hayashi ,  Yukio Yamashita ,  Byeongil An

发明人： Noriyuki Hayashi ,  Yukio Yamashita ,  Byeongil An

IPC分类号： F02B37/00

CPC分类号： F04D29/057 ,  F02B37/10 ,  F02B39/10 ,  F04D25/06 ,  F04D25/08 ,  F04D29/047 ,  F04D29/063 ,  F16C17/02 ,  F16C27/02 ,  F16C33/1045 ,  F16C2360/44 ,  Y02T10/144

摘要： A rotation shaft supporting structure for an electric supercharger is provided with: a rotation shaft to which a compressor wheel is attached, the compressor wheel being a wheel of a supercharging side; an electric motor including a motor rotator securely installed to the rotation shaft, and a stator for applying torque to the motor rotator; a bearing provided on a bearing side closer to the compressor wheel than the motor rotator so as to support the rotation shaft; and a damper unit for absorbing shaft vibration of the rotation shaft, the damper unit being provided at a shaft end on an opposite side to the bearing side.

摘要翻译： 一种用于电动增压器的旋转轴支撑结构设置有：连接有压缩机叶轮的旋转轴，所述压缩机叶轮是增压侧的轮; 包括牢固地安装在旋转轴上的电动机转子的电动机和向电动机转子施加转矩的定子; 设置在比马达转子更靠近压缩机叶轮的轴承侧以支撑旋转轴的轴承; 以及用于吸收所述旋转轴的轴振动的阻尼器单元，所述阻尼单元设置在与所述轴承侧相反侧的轴端。

公开(公告)号：US20130180847A1

公开(公告)日：2013-07-18

申请号：US13244466

申请日：2011-09-24

申请人： Takao Yonehara ,  Subramanian Tamilmani ,  Karl-Josef Kramer ,  Jay Ashjaee ,  Mehrdad M. Moslehi ,  Yasuyoshi Miyaji ,  Noriyuki Hayashi ,  Takamitsu Inahara

发明人： Takao Yonehara ,  Subramanian Tamilmani ,  Karl-Josef Kramer ,  Jay Ashjaee ,  Mehrdad M. Moslehi ,  Yasuyoshi Miyaji ,  Noriyuki Hayashi ,  Takamitsu Inahara

IPC分类号： H01L21/02

CPC分类号： C25D11/005 ,  C25D11/32 ,  C25F3/12 ,  C25F7/02 ,  H01L21/0203 ,  H01L21/67086 ,  H01L21/67781 ,  H01L21/68721 ,  H01L21/68771 ,  H01L21/68785 ,  H01L31/1804 ,  Y02E10/547 ,  Y02P70/521

摘要： This disclosure enables high-productivity fabrication of porous semiconductor layers (made of single layer or multi-layer porous semiconductors such as porous silicon, comprising single porosity or multi-porosity layers). Some applications include fabrication of MEMS separation and sacrificial layers for die detachment and MEMS device fabrication, membrane formation and shallow trench isolation (STI) porous silicon (using porous silicon formation with an optimal porosity and its subsequent oxidation). Further, this disclosure is applicable to the general fields of photovoltaics, MEMS, including sensors and actuators, stand-alone, or integrated with integrated semiconductor microelectronics, semiconductor microelectronics chips and optoelectronics.

摘要翻译： 本公开使得可以高产率地制造多孔半导体层（由诸如多孔硅的单层或多层多孔半导体制成，包括单孔隙率或多孔隙率层）。 一些应用包括制造用于脱模和MEMS器件制造，膜形成和浅沟槽隔离（STI）多孔硅的MEMS分离和牺牲层（使用具有最佳孔隙率的多孔硅形成及其随后的氧化）。 此外，本公开适用于光伏技术的MEMS领域，包括传感器和执行器，独立的或与集成半导体微电子，半导体微电子芯片和光电子集成。

公开(公告)号：US08487117B2

公开(公告)日：2013-07-16

申请号：US13122147

申请日：2009-10-07

申请人： John Nuss ,  Matthew Williams ,  Raju Mohan ,  Richard Martin ,  Tie-Lin Wang ,  Kazumasa Aoki ,  Hiroyuki Tsuruoka ,  Noriyuki Hayashi ,  Tsuyoshi Homma

发明人： John Nuss ,  Matthew Williams ,  Raju Mohan ,  Richard Martin ,  Tie-Lin Wang ,  Kazumasa Aoki ,  Hiroyuki Tsuruoka ,  Noriyuki Hayashi ,  Tsuyoshi Homma

IPC分类号： C07D207/30 ,  A61K31/40

CPC分类号： C07D207/34

摘要： The present invention comprises a compound for the prevention and/or treatment of cardiovascular diseases. The compound is an atropisomer of a compound represented by the following general formula (I): wherein R1 represents a C1-C3 alkyl group; R2 represents a 2-hydroxy-C4-C6 alkyl group; R3 represents a halogeno group, a halogeno-C1-C3 alkyl group and the like; R4 represents a hydrogen atom, a halogeno group and the like; R5 represents a C1-C3 alkyl group; and R6 represents a hydrogen atom, a halogeno group and the like] or atropisomers thereof.

摘要翻译： 本发明包括用于预防和/或治疗心血管疾病的化合物。 该化合物是由以下通式（I）表示的化合物的阻转异构体：其中R1表示C1-C3烷基; R2表示2-羟基-C4-C6烷基; R 3表示卤代基，卤代-C 1 -C 3烷基等; R4代表氢原子，卤代基等; R5代表C1-C3烷基; R6表示氢原子，卤代基等]或它们的阻转异构体。