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    • 3. 发明授权
    • Elastic couple barring apparatus
    • 弹力夫妇禁止装置
    • US08549946B2
    • 2013-10-08
    • US10529283
    • 2003-09-12
    • Zijing Pang
    • Zijing Pang
    • F16H1/06F16H1/20
    • F03B11/00F03B11/006F03B11/04F05B2230/608Y02E10/226Y02P70/525Y10T74/19633Y10T74/19651Y10T74/19684
    • An elastic couple barring apparatus (i.e., an elastic couple rotor turning gear) is a special tool to drive a rotor by elastic couple for adjusting a shafting center of a vertical hydroelectric generating set and other rotating devices. The elastic couple rotor turning gear is characterized in that an elastic support is mounted on a frame of the driven device, a casing being connected to the elastic support, a casing cover being firmly fixed on the casing, a speed reducer and an electric motor being installed on the cover, an output shaft of the speed reducer extending into the casing under the casing cover, the output shaft having a pinion gear mounted thereon and meshed with a gear body of a bull gear positioned in the casing, the bull gear being connected to a shaft coupling through parallel keys via a key seat or an upright post, and the shaft coupling being fixed on a rotor of the driven device. The advantages of the invention is that the structure is more reasonable, the concentricity may be adjusted more conveniently, the elastic connection makes operation easy and vibration small, deformation caused by suspending arms is eliminated, and operation's accuracy and precision are improved because the gears may be meshed and operated smoothly.
    • 弹性联轴器装置(即弹性耦合转子转动齿轮)是用于调节垂直水力发电机组和其它旋转装置的轴系中心的弹性联轴器驱动转子的专用工具。 弹性耦合转子转动齿轮的特征在于,弹性支撑件安装在从动装置的框架上,壳体连接到弹性支撑件,壳体盖牢固地固定在壳体上,减速器和电动机 安装在盖上,减速器的输出轴延伸到壳体下方的壳体中,输出轴具有安装在其上的小齿轮并与定位在壳体中的大齿轮的齿轮体啮合,大齿轮连接 通过键座或立柱连接到通过平行键的轴,并且所述轴联接件固定在从动装置的转子上。 本发明的优点是结构更合理,可以更方便地调整同心度,弹性连接使操作容易,振动小,由悬挂臂引起的变形消除,操作精度和精度提高,因为齿轮可能 啮合平稳。
    • 6. 发明申请
    • Exit stay apparatus with intermediate flange
    • 具有中间法兰的出口支架
    • US20090087305A1
    • 2009-04-02
    • US11904579
    • 2007-09-28
    • Alexander Gokhman
    • Alexander Gokhman
    • F03B11/04
    • F03B11/04F03B3/02F03B3/18Y02E10/223Y02E10/226
    • The invention is an Exit Stay Apparatus with Intermediate Flange for Francis and propeller hydraulic turbines. The purpose of the invention is to improve the effectiveness of known Exit Stay Apparatus (U.S. Pat. No. 6,918,744, July 2005, for Hydraulic Turbine and Exit Stay Apparatus therefor) in eliminating the axial central vortex and, therefore, in increasing the efficiency and decreasing the flow pressure pulsations in draft tube cone at off optimum operating regimes. The new Exit Stay Apparatus has an intermediate flange between exit stay crown and periphery and two sets of exit stay vanes: crown exit stay vanes secured to the exit stay crown and the intermediate flange and peripheral exit stay vanes secured to the intermediate flange and following to the periphery. When installed in the turbine the peripheral exit stay vanes are secured at the periphery. There are more crown exit stay vanes than the peripheral exit stay vanes and their profiles are longer than the profiles of the peripheral exit stay vanes. The Exit Stay Apparatus with Intermediate Flange is expected to have the same peak efficiency as known Exit Stay Apparatus.
    • 本发明是用于弗朗西斯和螺旋桨水力涡轮机的中间法兰的出口保持装置。 本发明的目的是提高已知的出口保持装置(美国专利号6,918,744,2005年7月,用于其液压涡轮机和出口保持装置)的有效性,以消除轴向中心涡流,并因此提高效率和 在最佳操作状态下减小引流管锥体中的流量脉动。 新的出口保持装置在出口支撑冠和周边之间具有中间凸缘和两组出口支撑叶片:固定到出口支撑冠的顶盖出口支撑叶片和固定到中间凸缘的中间凸缘和外围出口支撑叶片, 周边。 当安装在涡轮机中时,周边出口支撑叶片固定在周边。 与外围出口支撑叶片相比,具有更多的冠出口支撑叶片,并且它们的轮廓比外围出口撑叶片的轮廓长。 具有中间法兰的出口保持装置预计具有与已知的退出装置相同的最高效率。
    • 7. 发明授权
    • Method and System for detecting and reducing draft tube pressure fluctuations
    • 用于检测和减少引流管压力波动的方法和系统
    • US07035718B2
    • 2006-04-25
    • US10707944
    • 2004-01-27
    • Raymond Verle JensenJames Robert Rasmussen
    • Raymond Verle JensenJames Robert Rasmussen
    • G05B13/00
    • F03B3/02F03B11/002F03B11/04G05D19/02Y02E10/223Y02E10/226
    • A method and system to reduce vibration in a turbine-generator including measuring a magnitude of radial vibration of a turbine shaft with at least one vibration sensor configured to generate a vibration signal indicative of vibration frequency; measuring a generator power output with a power output sensor configured to generate a generator power output signal; detecting vibration frequencies in a rough load zone range; engaging an air injection means when a magnitude of radial vibration detected in the rough load zone range is above a predetermined threshold; storing a generator power output level as a reference level when engaging the air injection means; and disengaging the air injection means when either the measured generator power output exceeds a predetermined level or the measured generator power output differs from the reference level by a predetermined amount.
    • 一种用于减少涡轮发电机中的振动的方法和系统,包括:用至少一个振动传感器测量涡轮轴的径向振动的大小,所述至少一个振动传感器被配置成产生表示振动频率的振动信号; 用配置成产生发电机功率输出信号的功率输出传感器来测量发电机功率输出; 检测粗加载区范围内的振动频率; 当在粗加载区域范围内检测到的径向振动的大小高于预定阈值时,接合空气喷射装置; 当接合空气喷射装置时,将发电机功率输出电平存储为参考电平; 以及当所测量的发电机功率输出超过预定水平或所测量的发电机功率输出与参考水平不同预定量时,分离空气喷射装置。
    • 8. 发明申请
    • METHOD AND SYSTEM FOR DETECTING AND REDUCING DRAFT TUBE PRESSURE FLUCTUATIONS
    • 用于检测和减少管道压力波动的方法和系统
    • US20050165510A1
    • 2005-07-28
    • US10707944
    • 2004-01-27
    • Raymond JensenJames Rasmussen
    • Raymond JensenJames Rasmussen
    • F03B11/00F03B11/04G05D19/02G01M1/38G05B13/00G05B15/00G05B21/00G05D23/00
    • F03B3/02F03B11/002F03B11/04G05D19/02Y02E10/223Y02E10/226
    • A method and system to reduce vibration in a turbine-generator including measuring a magnitude of radial vibration of a turbine shaft with at least one vibration sensor configured to generate a vibration signal indicative of vibration frequency; measuring a generator power output with a power output sensor configured to generate a generator power output signal; detecting vibration frequencies in a rough load zone range; engaging an air injection means when a magnitude of radial vibration detected in the rough load zone range is above a predetermined threshold; storing a generator power output level as a reference level when engaging the air injection means; and disengaging the air injection means when either the measured generator power output exceeds a predetermined level or the measured generator power output differs from the reference level by a predetermined amount.
    • 一种用于减少涡轮发电机中的振动的方法和系统,包括:用至少一个振动传感器测量涡轮轴的径向振动的大小,所述至少一个振动传感器被配置成产生表示振动频率的振动信号; 用配置成产生发电机功率输出信号的功率输出传感器来测量发电机功率输出; 检测粗加载区范围内的振动频率; 当在粗加载区域范围内检测到的径向振动的大小高于预定阈值时,接合空气喷射装置; 当接合空气喷射装置时,将发电机功率输出电平存储为参考电平; 以及当所测量的发电机功率输出超过预定水平或所测量的发电机功率输出与参考水平不同预定量时,分离空气喷射装置。
    • 9. 发明授权
    • Hydraulic turbine and exit stay apparatus therefor
    • 液压涡轮机和出口支架
    • US06918744B2
    • 2005-07-19
    • US10224442
    • 2002-08-21
    • Alexander Gokhman
    • Alexander Gokhman
    • F03B3/18F03B11/04F03B3/16
    • F03B3/02F03B3/18F03B11/04Y02E10/223Y02E10/226Y10S415/914
    • The invention is an Exit Stay Apparatus for Francis and propeller hydraulic turbines. The purpose of the invention is to eliminate the loss of turbine efficiency and strong pulsations in draft tube caused by the axial circular vortex in all turbine operating regimes other than optimum without a noticeable decrease in maximum efficiency. It can be incorporated not only into newly fabricated hydraulic turbines, but also retrofitted into existing turbines. The Exit Stay Apparatus has a crown and exit stay vanes secured to the the crown. When installed in the turbine, the exit stay crown is located immediately after the runner crown, which is truncated at the bottom by a plane perpendicular to the central axis of the turbine. The exit stay crown together with the truncated runner crown forms water passages after the runner blade crown profile exit. The exit stay vanes are arranged in a circular array around the turbine axis, located after the runner blades, and attached at the periphery either to the draft tube cone or to an exit stay flange secured to the turbine discharge ring and to the draft tube cone.
    • 本发明是用于弗朗西斯和推进器水力涡轮机的出口装置。 本发明的目的是消除除最佳效率以外的所有涡轮机操作方案中由轴向圆形涡流引起的涡轮机效率和强脉动的损失,而不会出现明显的降低。 它不仅可以纳入新制造的水轮机,而且还可以加装到现有的涡轮机中。 退出装置具有固定在冠上的冠和出口支撑叶片。 当安装在涡轮机中时,出口支撑冠位于紧靠在垂直于涡轮机的中心轴线的平面的底部截尾的转轮冠之后。 出口保持冠与截顶的流道冠冠在流道叶片冠轮廓出口之后形成水通道。 出口支撑叶片围绕涡轮机轴线布置在涡轮机轴线上,位于流道叶片之后,并且在外围附接到引流管锥体或固定到涡轮机排出环的出口支撑凸缘和引流管​​锥体 。
    • 10. 发明授权
    • Adjustable blade turbines
    • 可调叶片涡轮机
    • US6164907A
    • 2000-12-26
    • US314225
    • 1999-05-18
    • Joseph M. CybularzRichard K. DonelsonRichard K. Fisher, Jr.Robert G. GrubbRandy V. SeifarthSiegbert EtterDonald E. Zehner
    • Joseph M. CybularzRichard K. DonelsonRichard K. Fisher, Jr.Robert G. GrubbRandy V. SeifarthSiegbert EtterDonald E. Zehner
    • F03B3/06F03B3/14F03B11/00F03B11/04F03B3/18F03B15/10F03B15/14
    • F03B11/006F03B3/06F03B3/14F03B11/04Y02E10/223Y02E10/226
    • A turbine installation having reduced inner and outer gaps comprises a water passageway and a turbine runner disposed in the passageway downstream of a discharge ring. The turbine runner includes a hollow hub having spaced apart inner and outer surfaces and a longitudinal axis and a plurality of runner blades. Each blade comprises a hydrofoil having an inner edge and a distal outer edge, a leading edge and a trailing edge separated by a water directing surface. Each blade is pivotally connected to the hub about a rotational axis extending in a direction generally perpendicular to the longitudinal axis so that its inner edge is proximate the hub. Each blade is rotatable between a maximum pitch position and a minimum pitch position. The discharge ring has a spherical configuration cooperable with the outer edge of each of the blades to reduce an outer gap formed between the outer edge of each of the blades and the passageway. The hub may be configured as a sphere downstream of the blade rotational axes to reduce an inner gap formed between the inner edge of each of the blades and the hub. The hub may also include a plurality of pockets or raised areas formed on the outer surface of the hub to reduce the inner gap formed between the inner edge of each of the blades and the hub.
    • 具有减小的内部和外部间隙的涡轮机装置包括设置在排出环下游的通道中的水通道和涡轮流道。 涡轮流道包括具有间隔开的内表面和外表面以及纵向轴线和多个流道叶片的中空轮毂。 每个叶片包括具有内边缘和远端外边缘的水翼,前缘和由水引导表面分开的后缘。 每个叶片围绕围绕纵向轴线的方向延伸的旋转轴线枢转地连接到轮毂,使得其内边缘靠近轮毂。 每个叶片可在最大俯仰位置和最小俯仰位置之间旋转。 排出环具有与每个叶片的外边缘配合的球形构造,以减少形成在每个叶片的外边缘和通道之间的外部间隙。 毂可以被配置为在叶片旋转轴线的下游的球体,以减小形成在每个叶片的内边缘和轮毂之间的内部间隙。 轮毂还可以包括形成在轮毂的外表面上的多个凹穴或凸起区域,以减小形成在每个叶片的内边缘和轮毂之间的内部间隙。