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    CMC vane insulator and method of use
    3.
    发明授权
    CMC vane insulator and method of use 有权
    CMC叶片绝缘子及使用方法

    公开(公告)号：US07625170B2

    公开(公告)日：2009-12-01

    申请号：US11526501

    申请日：2006-09-25

    Applicant: John Greene ,  Ronald Ralph Cairo ,  Paul Steven Dimascio ,  Nitin Bhate ,  Jason Thurman Stewart

    Inventor： John Greene ,  Ronald Ralph Cairo ,  Paul Steven Dimascio ,  Nitin Bhate ,  Jason Thurman Stewart

    IPC: F01D11/00

    CPC classification number: F01D9/042 ,  F01D5/147 ,  F01D5/188 ,  F01D5/189 ,  F01D5/284 ,  F01D5/30 ,  F01D5/3084 ,  F05D2300/603 ,  F05D2300/6033 ,  Y10T29/49321

    Abstract: A method for assembling a gas or steam turbine is provided. The method includes providing an insulator and positioning the insulator between a vane support and a vane such that the insulator facilitates preventing hot gas migration into the vane, and such that during operation, hot gas is channeled from a high pressure side of the vane to a low pressure side of the vane. A vane assembly for a turbine rotor assembly is also provided. The vane assembly includes a vane support and an insulator including a projecting portion. The assembly also includes a vane. The insulator is coupled to the vane support such that the projecting portion is between the vane and a nozzle support strut to facilitate hot gas flow from a pressure side of the projecting portion to a suction side of the projecting portion.

    Abstract translation: 提供了一种用于组装气体或汽轮机的方法。 该方法包括提供绝缘体并将绝缘体定位在叶片支撑件和叶片之间，使得绝缘体有助于防止热气体迁移到叶片中，并且使得在操作期间，热气体从叶片的高压侧引导至 叶片的低压侧。 还提供了一种用于涡轮转子组件的叶片组件。 叶片组件包括叶片支撑件和包括突出部分的绝缘体。 组件还包括叶片。 绝缘体联接到叶片支撑件，使得突出部分在叶片和喷嘴支撑支柱之间，以便于热气体从突出部分的压力侧流到突出部分的吸入侧。

    Seal-less CMC vane to platform interfaces
    4.
    发明授权
    Seal-less CMC vane to platform interfaces 有权
    无密封CMC叶片到平台接口

    公开(公告)号：US07329087B2

    公开(公告)日：2008-02-12

    申请号：US11228251

    申请日：2005-09-19

    Applicant: Ronald Ralph Cairo ,  Nitin Bhate

    Inventor： Ronald Ralph Cairo ,  Nitin Bhate

    IPC: F01D9/04

    CPC classification number: F01D9/042 ,  F01D5/147 ,  F01D5/284 ,  F01D11/005 ,  F05D2230/642 ,  F05D2300/6033

    Abstract: A stator vane assembly for a gas turbine includes a ceramic matrix composite airfoil held between radially inner and outer metal platforms wherein an interface between the airfoil and at least one of the radially inner and outer platforms is shaped to create a circuitous leakage path for gas from the gas turbine hot gas path.

    Abstract translation: 用于燃气轮机的定子叶片组件包括保持在径向内部和外部金属平台之间的陶瓷基体复合翼型件，其中翼型件与径向内部和外部平台中的至少一个之间的界面成形为产生迂回的气体泄漏路径 燃气轮机热气路径。

    Sealing device and method for turbomachinery
    6.
    发明申请
    Sealing device and method for turbomachinery 有权
    涡轮机械密封装置及方法

    公开(公告)号：US20050220610A1

    公开(公告)日：2005-10-06

    申请号：US10813102

    申请日：2004-03-30

    Applicant: Farshad Ghasripoor ,  Murtuza Lokhandwalla ,  Raymond Chupp ,  Nitin Bhate

    Inventor： Farshad Ghasripoor ,  Murtuza Lokhandwalla ,  Raymond Chupp ,  Nitin Bhate

    IPC: F01D11/08 ,  F01D5/28 ,  F01D11/12 ,  F01D11/14 ,  F02C7/28 ,  F01D5/20

    CPC classification number: F01D11/14 ,  F01D5/225 ,  Y02T50/673

    Abstract: A compliant seal for use between rotating blades and a static shroud surrounding the rotating blades in a steam or gas turbine is disclosed. The seal includes a tip surface, substantially resistant to wear due to rubbing by the tip of the rotating blades, and an elastic biasing member, comprising a biasing element. The wear-resistant surface is thus biased against the tips of the rotating blades to seal a gas path between the rotating blades and the static shroud.

    Abstract translation: 公开了一种在旋转叶片和围绕蒸汽或燃气轮机中的旋转叶片的静态护罩之间使用的柔性密封件。 密封件包括基本上抵抗由旋转刀片的尖端摩擦而导致的磨损的尖端表面，以及包括偏置元件的弹性偏置构件。 因此耐磨表面被偏压抵靠旋转叶片的尖端以密封旋转叶片和静态护罩之间的气体路径。

    FIXTURE AND INSPECTION METHOD FOR AN ANNULAR SEAL
    8.
    发明申请
    FIXTURE AND INSPECTION METHOD FOR AN ANNULAR SEAL 有权
    固定密封件的检测方法

    公开(公告)号：US20100236066A1

    公开(公告)日：2010-09-23

    申请号：US12792078

    申请日：2010-06-02

    Applicant: Anthony Constantine Thermos ,  Ronald Ralph Cairo ,  Mehmet Demiroglu ,  Nitin Bhate

    Inventor： Anthony Constantine Thermos ,  Ronald Ralph Cairo ,  Mehmet Demiroglu ,  Nitin Bhate

    IPC: B21D53/84

    CPC classification number: F16J15/3296 ,  F16J15/3288 ,  G01B5/12 ,  G01B5/252 ,  Y10T29/49297 ,  Y10T29/49895 ,  Y10T29/49998 ,  Y10T29/53961 ,  Y10T29/53978

    Abstract: A fixture assembly and inspection method by which the internal diameter and/or concentricity of a segmented annular seal can be readily inspected and optionally measured prior to final installation. The fixture assembly has at least two fixture segments supported on a base, by which an annular fixture housing is defined having an outer rim and a groove with a cross-sectional shape corresponding to a cross-sectional shape of the annular seal. The fixture assembly further includes a device or apparatus for assessing at least one dimensional characteristic of the annular seal when installed in the groove of the fixture housing and as the assessing device/apparatus travels along the interior circumference of the fixture housing.

    Abstract translation: 一种夹具组件和检查方法，通过该固定装置和检查方法可以在最终安装之前容易地检查和任选地测量分段环形密封件的内径和/或同心度。 夹具组件具有至少两个支撑在基座上的固定部分，环形夹具壳体被限定为具有外缘和具有对应于环形密封件的横截面形状的横截面形状的凹槽。 固定装置还包括一种装置或装置，用于当安装在固定件壳体的凹槽中时评估环形密封件的至少一维尺寸特征，并且当评估装置/装置沿固定件壳体的内周行进时。

    BARRIER SEALING SYSTEM
    9.
    发明申请
    BARRIER SEALING SYSTEM 审中-公开
    障碍密封系统

    公开(公告)号：US20090066033A1

    公开(公告)日：2009-03-12

    申请号：US11853404

    申请日：2007-09-11

    Applicant: Roderick Mark Lusted ,  Nitin Bhate ,  Eric John Ruggiero ,  Kripa Kiran Varanasi ,  Gabriele Mariotti ,  Paolo Susini

    Inventor： Roderick Mark Lusted ,  Nitin Bhate ,  Eric John Ruggiero ,  Kripa Kiran Varanasi ,  Gabriele Mariotti ,  Paolo Susini

    IPC: F01D11/02

    CPC classification number: F01D11/001 ,  F01D11/02 ,  F01D11/04 ,  F05D2240/56 ,  F16J15/002 ,  F16J15/406

    Abstract: A barrier seal system comprises a rotatable shaft disposed within an outer housing. The rotatable shaft axially extends from a high-pressure region to a low-pressure region within the outer housing. At least a portion of the rotatable shaft, typically the portion disposed adjacent to the low-pressure region, comprises an oleophobic surface. The system further comprises a barrier seal that radially extends from the outer housing to the rotatable shaft and defines a gap between the barrier seal and the rotatable shaft. A barrier gas injector is provided for injecting a barrier gas into the gap to flow from the high-pressure region to the low-pressure region.

    Abstract translation: 隔离物密封系统包括设置在外壳内的可旋转轴。 可旋转轴从外部壳体内的高压区域轴向延伸到低压区域。 可旋转轴的至少一部分，通常是邻近低压区设置的部分，包括疏油表面。 所述系统还包括从所述外壳径向延伸到所述可旋转轴并且限定所述阻挡密封件和所述可旋转轴之间的间隙的隔离密封件。 提供阻挡气体注入器，用于将阻挡气体注入间隙以从高压区域流到低压区域。

    Sealing device and method for turbomachinery
    10.
    发明授权
    Sealing device and method for turbomachinery 有权
    涡轮机械密封装置及方法

    公开(公告)号：US07435049B2

    公开(公告)日：2008-10-14

    申请号：US10813102

    申请日：2004-03-30

    Applicant: Farshad Ghasripoor ,  Murtuza Lokhandwalla ,  Raymond Edward Chupp ,  Nitin Bhate

    Inventor： Farshad Ghasripoor ,  Murtuza Lokhandwalla ,  Raymond Edward Chupp ,  Nitin Bhate

    IPC: F01D11/06

    CPC classification number: F01D11/14 ,  F01D5/225 ,  Y02T50/673

    Abstract: A compliant seal for use between rotating blades and a static shroud surrounding the rotating blades in a steam or gas turbine is disclosed. The seal includes a tip surface, substantially resistant to wear due to rubbing by the tip of the rotating blades, and an elastic biasing member, comprising a biasing element. The wear-resistant surface is thus biased against the tips of the rotating blades to seal a gas path between the rotating blades and the static shroud.

    Abstract translation: 公开了一种在旋转叶片和围绕蒸汽或燃气轮机中的旋转叶片的静态护罩之间使用的柔性密封件。 密封件包括基本上抵抗由旋转刀片的尖端摩擦而导致的磨损的尖端表面，以及包括偏置元件的弹性偏置构件。 因此耐磨表面被偏压抵靠旋转叶片的尖端以密封旋转叶片和静态护罩之间的气体路径。

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