Fiberoptic clearance detection system and method
    71.
    发明授权
    Fiberoptic clearance detection system and method 有权
    光纤清除检测系统及方法

    公开(公告)号:US08009939B2

    公开(公告)日:2011-08-30

    申请号:US12241527

    申请日:2008-09-30

    CPC分类号: G01B11/14

    摘要: A fiberoptic system for clearance detection between rotating and stationary turbomachinery components is presented. The system comprises an optical fiber probe comprising a plurality of optical fibers, at least one of the optical fibers comprising a transmission fiber and at least one of the optical fibers comprising a signal fiber; a light source for providing light through the transmission fiber towards a target; filters for receiving light from the signal fibers, at least two of the filters for filtering different wavelengths; and at least one photodetector for receiving filtered light from the filters.

    摘要翻译: 提出了一种用于旋转和固定涡轮机组件之间的间隙检测的光纤系统。 该系统包括包括多个光纤的光纤探针,至少一个光纤包括传输光纤,并且至少一个光纤包括信号光纤; 用于通过传输光纤向目标提供光的光源; 用于从信号光纤接收光的滤波器,用于滤除不同波长的滤波器中的至少两个; 以及至少一个用于从滤光器接收滤光的光电检测器。

    ACTIVE RETRACTABLE SEAL FOR TURBOMACHINERY AND RELATED METHOD
    73.
    发明申请
    ACTIVE RETRACTABLE SEAL FOR TURBOMACHINERY AND RELATED METHOD 审中-公开
    用于涡轮机的主动回缩密封件及相关方法

    公开(公告)号:US20100078893A1

    公开(公告)日:2010-04-01

    申请号:US12241407

    申请日:2008-09-30

    IPC分类号: F16J15/447

    摘要: An active retractable seal assembly is configured for use between a rotating component and a stationary component of turbo machinery is disclosed. The seal assembly includes a seal mounted to the stationary component. The seal is movable towards and away from the rotating component between a respective closed position and an open position as a function of pressure drop across the seal. The seal includes an active seal segment, a non-active seal segment, and a fluid by-pass circuit. The fluid by-pass circuit is configured for directing fluid around the active seal segment to reduce pressure drop across the active seal segment thereby resulting in the active seal segment moving towards an open position under the action of one or more biasing devices while maintaining the non-active seal segment in a closed position.

    摘要翻译: 公开了一种主动的可缩回密封组件,用于在涡轮机械的旋转部件和固定部件之间使用。 密封组件包括安装到固定部件的密封件。 密封件可以在相应的关闭位置和打开位置之间朝向和远离旋转部件移动,作为穿过密封件的压降的函数。 密封件包括主动密封段,非活动密封段和流体旁路电路。 流体旁路电路被配置成用于引导流体围绕主动密封段,以减小跨过主动密封段的压降,从而导致主动密封段在一个或多个偏置装置的作用下朝向打开位置移动,同时保持非 - - 活动密封段处于关闭位置。

    Turbomachinery system fiberoptic multi-parameter sensing system and method
    74.
    发明申请
    Turbomachinery system fiberoptic multi-parameter sensing system and method 有权
    涡轮机械系统光纤多参数传感系统及方法

    公开(公告)号:US20090320609A1

    公开(公告)日:2009-12-31

    申请号:US12215094

    申请日:2008-06-25

    IPC分类号: G01L1/24 G01H9/00 G01B11/00

    摘要: A fiberoptic multi-parameter sensing system for monitoring turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status includes a multi-furcated fiber bundle based optical splitter configured to transmit light to a surface of at least one turbomachinery system shaft through a plurality of optical fiber bundles disposed at a plurality of locations in proximity to the surface of the at least one shaft, in which the plurality of locations together are arranged in a substantially axial direction between the ends of the at least one shaft. The system further includes an array of high-temperature bifurcated fiber bundle based reflectance probes to receive reflectance signals from the shaft surface and send to an array of photosensitive detectors, configured to detect dynamic light reflected from the at least one turbomachinery system shaft surface in response to the transmitted light during rotation of at least one turbomachinery system shaft and generate dynamic reflected light signals there from. A sensing mechanism is configured to determine a torque or vibration on at least one turbomachinery system shaft in response to the dynamic reflected light signal signatures based on time-domain and frequency-domain signal processes.

    摘要翻译: 用于监测涡轮机械系统轴静态和动态扭矩,振动模式和相关操作状态的光纤多参数感测系统包括多分叉光纤束分光镜,其被配置为通过多个透镜将光透射到至少一个涡轮机械系统轴的表面 设置在所述至少一个轴的表面附近的多个位置的光纤束,其中所述多个位置一起在所述至少一个轴的端部之间沿大致轴向布置。 该系统还包括一组高温分叉纤维束的反射探测器,用于接收来自轴表面的反射信号并发送到一组光敏检测器,该阵列被配置为响应于检测从至少一个涡轮机械系统轴表面反射的动态光 在至少一个涡轮机械系统轴的旋转期间的透射光,并且从那里产生动态反射光信号。 感测机构被配置为响应于基于时域和频域信号处理的动态反射光信号特征来确定至少一个涡轮机械系统轴上的扭矩或振动。

    FLUIDIC SEALING FOR TURBOMACHINERY
    75.
    发明申请
    FLUIDIC SEALING FOR TURBOMACHINERY 失效
    流体密封用于涡轮机

    公开(公告)号:US20090297341A1

    公开(公告)日:2009-12-03

    申请号:US12131193

    申请日:2008-06-02

    IPC分类号: F01D5/20

    摘要: Disclosed is a seal for turbomachinery including a seal face locatable between a first turbomachinery component and a second turbomachinery component. At least one fluid channel extends through the seal. The at least one fluid channel is capable of injecting fluid flow between the first turbomachinery component and the second turbomachinery component at the seal face thereby disrupting a leakage flow between the first turbomachinery component and the second turbomachinery component. Further disclosed is a turbomachine utilizing the seal.

    摘要翻译: 公开了一种用于涡轮机械的密封件,包括可定位在第一涡轮机械部件和第二涡轮机械部件之间的密封面。 至少一个流体通道延伸穿过密封件。 所述至少一个流体通道能够在密封面处在第一涡轮机械部件和第二涡轮机械部件之间注入流体流动,从而破坏第一涡轮机械部件和第二涡轮机械部件之间的泄漏流。 另外公开了利用密封件的涡轮机。

    Compliant plate seals for turbomachinery
    76.
    发明授权
    Compliant plate seals for turbomachinery 有权
    符合涡轮机械的板式密封件

    公开(公告)号:US07419164B2

    公开(公告)日:2008-09-02

    申请号:US11504061

    申请日:2006-08-15

    IPC分类号: F16J15/447

    摘要: A shaft seal serves to reduce leakage between a rotating shaft and a static shell. The shaft seal includes a plurality of compliant plate members, each having a root and a tip. The compliant plate members are secured to the static shell at their root in facing relation. The tips of the compliant plate members define a sealing ring between the static shell and the rotating shaft. An axial flow resistance member is disposed within the compliant plate members and serves as a barrier to axial leakage flow between the compliant plate members.

    摘要翻译: 轴密封件用于减少旋转轴和静态外壳之间的泄漏。 轴封包括多个柔性板构件,每个具有根部和尖端。 柔性板构件在其根部处以面对关系固定到静态壳体上。 柔性板构件的尖端在静态壳和旋转轴之间限定密封环。 轴向阻力构件设置在柔性板构件内并用作在柔性板构件之间的轴向泄漏流动的障碍。

    Rotary machine sealing assembly
    78.
    发明授权
    Rotary machine sealing assembly 有权
    旋转机密封组件

    公开(公告)号:US06969231B2

    公开(公告)日:2005-11-29

    申请号:US10248259

    申请日:2002-12-31

    摘要: A sealing assembly for disposition in a rotary machine is disposed between a rotary component and a stationary component of the rotary machine. The sealing assembly includes at least one sealing strip affixed by caulking to one of the rotary and stationary components. An abradable portion is disposed on another of the rotary and stationary components and is positioned radially opposite to the at least one sealing strip. The abradable portion includes a thermal spray coated material, and the thermal spray coated material includes Cobalt, Nickel, Chromium, Aluminum, Yttrium (CoNiCrAlY) and further includes a material selected from the group consisting of hexagonal boron nitride, a thermoset polymer, and combinations thereof.

    摘要翻译: 用于设置在旋转机器中的密封组件设置在旋转机器的旋转部件和固定部件之间。 密封组件包括至少一个通过铆接固定到旋转部件和固定部件之一的密封条。 可磨损部分设置在另一个旋转和静止部件上,并且被定位成与至少一个密封条的径向相对。 可磨损部分包括热喷涂材料,热喷涂材料包括钴,镍,铬,铝,钇(CoNiCrAlY),并且还包括选自六方氮化硼,热固性聚合物和组合的材料 其中。

    Turbine brush seal protection device and method
    80.
    发明授权
    Turbine brush seal protection device and method 失效
    涡轮刷密封保护装置及方法

    公开(公告)号:US06206629B1

    公开(公告)日:2001-03-27

    申请号:US09376835

    申请日:1999-08-18

    IPC分类号: F01D4907

    CPC分类号: F16J15/3288 F16J15/3268

    摘要: A turbine brush seal protection device includes an annular substrate having an outer periphery and defining a slot open at the outer periphery. The slot is for receiving a portion of an annular brush seal of a gas turbine subassembly during installation of a gas turbine and such that the annular substrate at least partially covers the annular brush seal of the gas turbine subassembly. The annular substrate at the outer periphery and within the slot thereof is removably mounted to a stationary portion of the gas turbine subassembly. A turbine brush seal protection method includes the steps of providing the annular substrate, placing the annular substrate over a portion of an annular brush seal of a gas turbine subassembly such that the seal portion is inside the slot of the annular substrate during installation of a gas turbine and the annular substrate at least partially covers the annular brush seal of the gas turbine subassembly, mounting the annular substrate at the outer periphery and within the slot thereof to a stationary portion of the gas turbine subassembly, and removing the annular substrate from the stationary portion of the gas turbine subassembly before completion of installation of the gas turbine subassembly.

    摘要翻译: 涡轮刷密封保护装置包括具有外周边并限定在外周边开口的狭槽的环形基板。 所述槽用于在燃气轮机的安装期间接收燃气轮机子组件的环形刷密封件的一部分,并且使得环形衬底至少部分地覆盖燃气轮机子组件的环形刷密封。 在外周和其槽口内的环形基板可拆卸地安装到燃气轮机组件的固定部分。 涡轮刷密封保护方法包括以下步骤:提供环形基板,将环形基板放置在燃气轮机子组件的环形刷密封件的一部分上,使得密封部分在安装气体期间在环形基板的槽内 涡轮机和环形基板至少部分地覆盖燃气轮机子组件的环形刷密封件,将环形基板安装在外周边并且在其槽内,到燃气轮机子组件的固定部分,并将环形基板从固定件 在完成燃气轮机组件的安装之前,燃气轮机组件的一部分。