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公开(公告)号：US07654094B2
公开(公告)日：2010-02-02
申请号：US10589976
申请日：2004-03-09
IPC分类号： F02C6/08
CPC分类号： F01D1/08 , F01D5/187 , F01D17/165 , F02C3/00
摘要： A turbine nozzle (2) that, among components constructing a turbine, reaches particularly high temperature is efficiently cooled with a relatively simple structure. A double casing structure in which a turbine casing (7) is provided outside a turbine shell (5) is formed. The turbine casing (7) functions as a flow path (24) for compressed air (20→21) before combustion. The turbine shell (5) covers a turbine nozzle (2) and a radial turbine impeller (3) and forms flow paths (15, 16) for combustion gas (10→11→12→13). The compressed air (21) before combustion flowing in the flow path (24), for compressed air, having air-tightness between itself and the outside air is blown to the turbine nozzle (2) through a through-hole (51) penetrating both wall surfaces of the turbine shell (5) so that the turbine nozzle (2) is evenly cooled and the compressed air used to cool the turbine nozzle is made to flow toward the turbine impeller (3).
摘要翻译： 在构成涡轮机的部件达到特别高的温度下的涡轮喷嘴（2）以相对简单的结构被有效地冷却。 形成涡轮壳体（7）外侧的涡轮壳体（5）的双壳体结构。 在燃烧之前，涡轮机壳体（7）用作用于压缩空气（20-> 21）的流动路径（24）。 涡轮壳体（5）覆盖涡轮喷嘴（2）和径向涡轮叶轮（3）并形成用于燃烧气体（10-> 11-> 12-> 13）的流动路径（15,16）。 在流动路径（24）中流动的压缩空气（21）之间的压缩空气（其自身与外部空气之间具有气密性）通过贯穿两者的通孔（51）吹送到涡轮喷嘴（2） 涡轮壳体（5）的壁表面，使得涡轮喷嘴（2）被均匀地冷却，并且使用于冷却涡轮喷嘴的压缩空气流向涡轮机叶轮（3）。
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公开(公告)号：US08308420B2
公开(公告)日：2012-11-13
申请号：US12183443
申请日：2008-07-31
申请人： Manabu Yagi , Tadaharu Kishibe , Takanori Shibata , Hideo Nishida , Hiromi Kobayashi , Tetsuya Kuwano
发明人： Manabu Yagi , Tadaharu Kishibe , Takanori Shibata , Hideo Nishida , Hiromi Kobayashi , Tetsuya Kuwano
IPC分类号： F04D27/00
CPC分类号： F04D29/284 , F04D29/30
摘要： A centrifugal compressor is equipped with an impeller having a blade angle distribution that makes it possible to achieve a relatively wide operating range. The blade angle of a shroud side facing a circular plate of a blade is termed a first angle and a blade angle of a hub side disposed at the circular plate is a second. The shroud side is formed in a curved shape having an angle distribution from a front area in a shaft direction toward a centrifugal direction in which the first angle is the local maximum point before a substantially middle portion and the local minimum point after the substantially middle point. The hub side is formed in a curved shape having an angle distribution from the front area in the shaft direction toward the centrifugal direction in which the second angle is the maximum local point before the substantially middle portion.
摘要翻译： 离心压缩机配备有具有叶片角度分布的叶轮，其能够实现相对宽的操作范围。 面向叶片圆板的护罩侧的叶片角度称为第一角度，并且设置在圆板处的轮毂侧的叶片角度为第二角度。 护罩侧形成为具有从轴方向的前方区域朝向离心方向的角度分布的弯曲形状，其中第一角度在大致中间部分之前的局部最大点和大体上中点之后的局部最小点 。 毂侧形成为具有从轴方向的前方区域朝向离心方向的角度分布的弯曲形状，其中第二角度是大致中间部分之前的最大局部点。
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公开(公告)号：US20090035122A1
公开(公告)日：2009-02-05
申请号：US12183443
申请日：2008-07-31
申请人： Manabu YAGI , Tadaharu Kishibe , Takanori Shibata , Hideo Nishida , Hiromi Kobayashi , Tetsuya Kuwano
发明人： Manabu YAGI , Tadaharu Kishibe , Takanori Shibata , Hideo Nishida , Hiromi Kobayashi , Tetsuya Kuwano
CPC分类号： F04D29/284 , F04D29/30
摘要： A centrifugal compressor is equipped with an impeller having a blade angle distribution that makes it possible to achieve a relatively wide operating range. The blade angle of a shroud side facing a circular plate of a blade is termed a first angle and a blade angle of a hub side disposed at the circular plate is a second angle. The shroud side is formed in a curved shape having an angle distribution from a front area in a shaft direction toward a centrifugal direction in which the first angle is the local maximum point before a substantially middle portion and the local minimum point after the substantially middle point. The hub side is formed in a curved shape having an angle distribution from the front area in the shaft direction toward the centrifugal direction in which the second angle is the maximum local point before the substantially middle portion.
摘要翻译： 离心压缩机配备有具有叶片角度分布的叶轮，其能够实现相对宽的操作范围。 面向叶片圆形板的护罩侧的叶片角被称为第一角度，并且设置在圆板处的轮毂侧的叶片角度为第二角度。 护罩侧形成为具有从轴方向的前方区域朝向离心方向的角度分布的弯曲形状，其中第一角度在大致中间部分之前的局部最大点和大体上中点之后的局部最小点 。 毂侧形成为具有从轴方向的前方区域朝向离心方向的角度分布的弯曲形状，其中第二角度是大致中间部分之前的最大局部点。
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公开(公告)号：US20080092515A1
公开(公告)日：2008-04-24
申请号：US10589976
申请日：2004-03-09
CPC分类号： F01D1/08 , F01D5/187 , F01D17/165 , F02C3/00
摘要： A turbine nozzle (2) that, among components constructing a turbine, reaches particularly high temperature is efficiently cooled with a relatively simple structure. A double casing structure in which a turbine casing (7) is provided outside a turbine shell (5) is formed. The turbine casing (7) functions as a flow path (24) for compressed air (20→21) before combustion. The turbine shell (5) covers a turbine nozzle (2) and a radial turbine impeller (3) and forms flow paths (15, 16) for combustion gas (10→11→12→13). The compressed air (21) before combustion flowing in the flow path (24), for compressed air, having air-tightness between itself and the outside air is blown to the turbine nozzle (2) through a through-hole (51) penetrating both wall surfaces of the turbine shell (5). By this, the turbine nozzle (2) is cooled and the compressed air used to cool the turbine nozzle is made to flow toward the turbine impeller (3). As a result, the entire volume of compressed air (20) taken into the turbine contributes to mechanical work for driving the turbine impeller (3).
摘要翻译： 在构成涡轮机的部件达到特别高的温度下的涡轮喷嘴（2）以相对简单的结构被有效地冷却。 形成涡轮壳体（7）外侧的涡轮壳体（5）的双壳体结构。 在燃烧之前，涡轮机壳体（7）用作用于压缩空气（20-> 21）的流动路径（24）。 涡轮壳体（5）覆盖涡轮喷嘴（2）和径向涡轮叶轮（3）并形成用于燃烧气体（10-> 11-> 12-> 13）的流动路径（15,16）。 在流动路径（24）中流动的压缩空气（21）之间的压缩空气（其自身与外部空气之间具有气密性）通过贯穿两者的通孔（51）吹送到涡轮喷嘴（2） 涡轮壳体（5）的壁表面。 由此，涡轮喷嘴（2）被冷却，用于冷却涡轮喷嘴的压缩空气朝向涡轮机叶轮（3）流动。 结果，进入涡轮机的整个体积的压缩空气（20）有助于驱动涡轮叶轮（3）的机械作业。
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公开(公告)号：US06981360B2
公开(公告)日：2006-01-03
申请号：US10474324
申请日：2001-04-09
申请人： Manabu Yagi , Satoshi Dodo , Kuniyoshi Tsubouchi , Yasuaki Akatsu , Hiroshi Arita , Norio Yasugahira
发明人： Manabu Yagi , Satoshi Dodo , Kuniyoshi Tsubouchi , Yasuaki Akatsu , Hiroshi Arita , Norio Yasugahira
CPC分类号： F02C7/1435 , F01D15/10 , F02C3/305 , F02C7/10 , F02C9/28 , F05D2220/76 , F05D2270/54
摘要： An object of the present invention is to provide a gas turbine power generator capable of increasing the power generation efficiency in partial load operation and decreasing a variation in the number of rotations caused by a variation in power generation load. The gas turbine power generator comprises a compressor (2) for compressing air, a combustor (5) for burning the compressed air and fuel, a turbine (6) driven by combustion gas produced in the combustor and driving the compressor (2) and a generator (7), a regenerative heat exchanger (4) for exchanging heat between exhaust gas from the turbine and the compressed air led into the combustor, an intake air sprayer (1), and a humidifier (3). Intake air flown into the regenerative heat exchanger (4) is humidified and cooled by the intake air sprayer (1) and the humidifier (3).
摘要翻译： 本发明的目的是提供一种燃气轮机发电机，其能够提高部分负荷运转中的发电效率，并减少由发电负荷的变化引起的转数的变化。 燃气轮机发电机包括用于压缩空气的压缩机（2），用于燃烧压缩空气和燃料的燃烧器（5），由燃烧器中产生的燃烧气体驱动并驱动压缩机（2）的涡轮机（6）和 发电机（7），用于在来自涡轮机的废气与引入燃烧器的压缩空气之间进行热交换的再生式热交换器（4），进气喷射器（1）和加湿器（3）。 进入再生式热交换器（4）的进气通过进气喷雾器（1）和加湿器（3）被加湿和冷却。
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公开(公告)号：US20130259644A1
公开(公告)日：2013-10-03
申请号：US13879833
申请日：2011-10-17
IPC分类号： F04D17/12
CPC分类号： F04D17/122 , F04D29/444 , F05D2240/122 , F05D2250/70
摘要： A multi-stage impeller is configured in a multi-stage centrifugal compressor by fixing and attaching a plurality of centrifugal impellers to one rotating shaft. Diffusers and return channels are provided in order downstream from each impeller. The centrifugal impellers, the diffusers and the return channel are housed within a compressor casing. The return channels have a plurality of vanes positioned at intervals from one another in a circumferential direction, and at least two stages are provided. The vane exit angles monotonically increase toward the downstream stage.
摘要翻译： 多级叶轮通过将多个离心式叶轮固定并附接到一个旋转轴上而配置在多级离心式压缩机中。 扩散器和返回通道按每个叶轮的下游顺序设置。 离心式叶轮，扩散器和返回通道容纳在压缩机壳体内。 返回通道具有沿圆周方向彼此间隔设置的多个叶片，并且至少设有两个台阶。 叶片出口角度向下游阶段单调增加。
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公开(公告)号：US20110097203A1
公开(公告)日：2011-04-28
申请号：US12907126
申请日：2010-10-19
IPC分类号： F04D29/44
CPC分类号： F04D29/444 , F04D17/12 , F04D29/681 , F05D2250/52
摘要： Turbo machinery comprising an impeller and a diffuser positioned on a downstream side of the impeller that a channel wall surface of the diffuser is composed of a pair of a shroud side diffuser plate and a hub side diffuser plate which surface each other and a channel width is formed so as to be increased downstream, characterized in that guide vanes in a circular arc shape lower in height than the channel width are installed in a line of a plurality of vanes on both channel walls of the shroud side diffuser plate and hub side diffuser plate of the diffuser, and a total of vane heights of the two guide vanes at an outlet of the diffuser is set so as to be within a range from 30 to 70% of the channel width at the outlet of the diffuser.
摘要翻译： 涡轮机械包括叶轮和位于叶轮下游侧的扩散器，扩散器的通道壁表面由一对彼此面对并且沟道宽度的护罩侧扩散板和轮毂侧扩散板组成， 形成为向下游侧增加，其特征在于，在所述护罩侧扩散板和轮毂侧扩散板的两个通道壁上的多个叶片的一条线上安装有高于沟道宽度的圆弧形状的导向叶片 的扩散器的出口处的两个导向叶片的叶片高度的总和被设定为在扩散器的出口处的通道宽度的30至70％的范围内。
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公开(公告)号：US5995168A
公开(公告)日：1999-11-30
申请号：US790801
申请日：1997-01-30
申请人： Manabu Yagi
发明人： Manabu Yagi
CPC分类号： H04N5/455 , H04N21/4382 , H04N5/211 , H04N5/4401
摘要： A video receiver includes a tuner, a QAM demodulator including a selective gated PLL carrier recovery circuit, and a digital equalizer. The selective gated PLL carrier recovery circuit has a normal operation mode and a selection control mode. The channel changing of the tuner is performed after the selective gated PLL carrier recovery circuit is set to the selection control mode and the digital equalizer is held at its current state.
摘要翻译： 视频接收机包括调谐器，包括选通门控PLL载波恢复电路的QAM解调器和数字均衡器。 选择门控PLL载波恢复电路具有正常操作模式和选择控制模式。 在选择门控PLL载波恢复电路被设置为选择控制模式并且数字均衡器保持在其当前状态之后执行调谐器的频道改变。
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公开(公告)号：US4881049A
公开(公告)日：1989-11-14
申请号：US177281
申请日：1988-04-04
申请人： Manabu Yagi
发明人： Manabu Yagi
CPC分类号： H04L27/3827 , H04L27/362
摘要： A digital signal transmission system adopting a quadrature amplitude modulation and demodulation principle and feasible for large capacity data transmission in which a number of levels are used. Each of a modulating and a demodulating device of the system is constructed to shift the phase difference between two carrier waves by a suitable angle of .DELTA..theta. radian from .pi./2 radian. The tuning phase in the demodulating device is limited to one so as to allow a bit error rate characteristic to remain constant.
摘要翻译： 一种采用正交幅度调制和解调原理的数字信号传输系统，可用于使用多个级别的大容量数据传输。 系统的调制和解调装置中的每一个被构造为将两个载波之间的相位差以π/ 2弧度的DELTAθ弧度的适当角度移位。 解调装置中的调谐相位被限制为1，以便允许误码率特性保持恒定。
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公开(公告)号：US4620159A
公开(公告)日：1986-10-28
申请号：US769922
申请日：1985-08-27
申请人： Yasuharu Yoshida , Manabu Yagi
发明人： Yasuharu Yoshida , Manabu Yagi
CPC分类号： H04L7/0334
摘要： In a demodulation circuit, a timing synchronizing circuit generates a timing signal representing a sampling timing of an A/D converter and has a timing signal generator, a polarity identification circuit and a logic circuit. The timing signal generator is phase-controlled by a phase control signal and generates a timing signal. The polarity identification circuit identifies a polarity of a differential coefficient of the baseband signal at a sampling point of the A/D converter and generates a polarity identification signal. Upon logic processing, the logic circuit supplies to the timing signal generator the phase control signal representing a deviation of an actual sampling point of the baseband signal from an optimal sampling point. A carrier asynchronism detection circuit detects an asynchronism state of a carrier regenerating circuit and supplies to the timing synchronizing circuit a signal which changes its loop parameter.
摘要翻译： 在解调电路中，定时同步电路产生表示A / D转换器的采样定时的定时信号，并具有定时信号发生器，极性识别电路和逻辑电路。 定时信号发生器由相位控制信号进行相位控制，并产生定时信号。 极性识别电路识别A / D转换器的采样点处的基带信号的微分系数的极性，并生成极性识别信号。 在逻辑处理时，逻辑电路向定时信号发生器提供表示基带信号与最佳采样点的实际采样点的偏差的相位控制信号。 载波异步检测电路检测载波再生电路的异步状态，并向定时同步电路提供改变其环路参数的信号。
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