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    • 81. 发明授权
    • Shaft seal assembly and method
    • 轴封装配及方法
    • US07249768B2
    • 2007-07-31
    • US10841652
    • 2004-05-07
    • John E. Keba
    • John E. Keba
    • F16J15/34F16J15/46
    • F16J15/3448F16J15/004F16J15/164F16J15/3404
    • A pressure-actuated shaft seal assembly and associated method for controlling the flow of fluid adjacent a rotatable shaft are provided. The seal assembly includes one or more seal members that can be adjusted between open and closed positions, for example, according to the rotational speed of the shaft. For example, the seal member can be configured to be adjusted according to a radial pressure differential in a fluid that varies with the rotational speed of the shaft. In addition, in the closed position, each seal member can contact a rotatable member connected to the shaft to form a seal with the rotatable member and prevent fluid from flowing through the assembly. Thus, the seal can be closed at low speeds of operation and opened at high speeds of operation, thereby reducing the heat and wear in the seal assembly while maintaining a sufficient seal during all speeds of operation.
    • 提供了一种用于控制邻近可旋转轴的流体流动的压力驱动轴密封组件和相关联的方法。 密封组件包括一个或多个可以在打开和关闭位置之间调节的密封件,例如根据轴的转速。 例如,密封构件可以被配置为根据随轴的旋转速度而变化的流体中的径向压力差进行调节。 此外,在关闭位置,每个密封构件可以接触连接到轴的可旋转构件,以与可旋转构件形成密封并防止流体流过组件。 因此,密封件可以在低速操作下关闭并在高速运转时打开,由此在所有操作速度期间保持足够的密封,从而减少密封组件中的热量和磨损。
    • 85. 发明授权
    • Method and apparatus for controlling fluid leakage through gas turbine engines
    • 用于控制通过燃气涡轮发动机的流体泄漏的方法和装置
    • US06932567B2
    • 2005-08-23
    • US10326028
    • 2002-12-19
    • Robert Joseph AlbersMarcia Jean BoyleRafael Ruiz
    • Robert Joseph AlbersMarcia Jean BoyleRafael Ruiz
    • F01D11/00F01D11/02F16J15/34
    • F16J15/3448F01D11/003F01D11/02
    • A method for controlling fluid leakage between a first pressure region and a second pressure region within a gas turbine engine using a first sealing member and a second sealing member. The first sealing member is movably coupled to a portion of the gas turbine engine, and a space defined generally between a portion of the first sealing member and a portion of the second sealing member fluidly couples the first pressure region to the second pressure region. The method includes moving the first sealing member towards the second sealing member using fluid pressure within a portion of the engine, and, using the first and second sealing members, substantially controlling fluid leakage between the first pressure area and the second pressure area through the space generally without contacting the first sealing member with the second sealing member.
    • 一种使用第一密封构件和第二密封构件来控制燃气涡轮发动机内的第一压力区域和第二压力区域之间的流体泄漏的方法。 第一密封构件可移动地联接到燃气涡轮发动机的一部分,并且通常在第一密封构件的一部分和第二密封构件的一部分之间限定的空间将第一压力区域流体耦合到第二压力区域。 该方法包括使用发动机的一部分内的流体压力将第一密封构件朝向第二密封构件移动,并且使用第一和第二密封构件,通过空间基本上控制第一压力区域和第二压力区域之间的流体泄漏 通常不使第一密封构件与第二密封构件接触。
    • 87. 发明申请
    • Method and apparatus for controlling fluid leakage through gas turbine engines
    • 用于控制通过燃气涡轮发动机的流体泄漏的方法和装置
    • US20040120807A1
    • 2004-06-24
    • US10326028
    • 2002-12-19
    • Robert Joseph AlbersMarcia Jean BoyleRafael Ruiz
    • F01D005/00
    • F16J15/3448F01D11/003F01D11/02
    • A method for controlling fluid leakage between a first pressure region and a second pressure region within a gas turbine engine using a first sealing member and a second sealing member. The first sealing member is movably coupled to a portion of the gas turbine engine, and a space defined generally between a portion of the first sealing member and a portion of the second sealing member fluidly couples the first pressure region to the second pressure region. The method includes moving the first sealing member towards the second sealing member using fluid pressure within a portion of the engine, and, using the first and second sealing members, substantially controlling fluid leakage between the first pressure area and the second pressure area through the space generally without contacting the first sealing member with the second sealing member.
    • 一种使用第一密封构件和第二密封构件来控制燃气涡轮发动机内的第一压力区域和第二压力区域之间的流体泄漏的方法。 第一密封构件可移动地联接到燃气涡轮发动机的一部分,并且通常在第一密封构件的一部分和第二密封构件的一部分之间限定的空间将第一压力区域流体耦合到第二压力区域。 该方法包括使用发动机的一部分内的流体压力将第一密封构件朝向第二密封构件移动,并且使用第一和第二密封构件,通过空间基本上控制第一压力区域和第二压力区域之间的流体泄漏 通常不使第一密封构件与第二密封构件接触。
    • 90. 发明授权
    • Temperature and pressure resistant rotating seal construction for a pump
    • 泵的耐压耐旋转密封结构
    • US5642888A
    • 1997-07-01
    • US570001
    • 1995-12-08
    • Robert E. Rockwood
    • Robert E. Rockwood
    • F16J15/34
    • F16J15/3448F16J15/3404Y10S277/93Y10T137/85954
    • A seal construction is provided for sealing a rotating pump shaft against passage of a fluid along its central axis. The seal construction includes front and rear sealing flanges mounted coaxially to and rotatable with the pump shaft. Stationary engaging members are provided adjacent the rear surface of the front sealing flange and the front surface of the rear sealing flange for sealing engagement therewith. A temperature stabilized chamber is provided adjacent each sealing flange including means for recirculating and cooling fluid disposed therein so as to maintain the fluid between adjacent engaging members at a substantially constant temperature thereby maintaining a flatness of the sealing engagement between the sealing flange surfaces and the engaging members. The recirculating/cooling system includes a gland having first, second, third, and fourth fluid passages defined therein.
    • 提供密封结构用于密封旋转的泵轴以防止流体沿其中心轴线流过。 密封结构包括与泵轴同轴并与泵轴一起旋转安装的前后密封凸缘。 固定接合构件邻近前密封凸缘的后表面和后密封凸缘的前表面设置,用于与其密封接合。 在每个密封凸缘附近设置有温度稳定室,包括用于再循环和冷却设置在其中的流体的装置,以便使相邻接合构件之间的流体保持在基本恒定的温度,从而保持密封凸缘表面和接合部之间的密封接合的平坦度 会员 循环/冷却系统包括其中限定有第一,第二,第三和第四流体通道的压盖。