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    Cooling Circuit for Enhancing Turbine Performance
    4.
    发明申请
    Cooling Circuit for Enhancing Turbine Performance 审中-公开
    用于提高涡轮机性能的冷却回路

    公开(公告)号：US20090074589A1

    公开(公告)日：2009-03-19

    申请号：US11856945

    申请日：2007-09-18

    申请人： Biao Fang ,  Christopher Edward Wolfe ,  Omprakash Samudrala ,  Matthew Scott Kight ,  Jeffrey John Butkiewicz ,  Tara McGovern

    发明人： Biao Fang ,  Christopher Edward Wolfe ,  Omprakash Samudrala ,  Matthew Scott Kight ,  Jeffrey John Butkiewicz ,  Tara McGovern

    IPC分类号： F01D5/08

    CPC分类号： F02C7/12 ,  F01D25/12

    摘要： In a gas turbine having a compressor discharge casing, a cooling circuit diverts compressor discharge air toward a high pressure packing (HPP) circuit. The cooling circuit includes an inlet pipe that receives compressor discharge air. One or several cooled cooling air pipes are in fluid communication with the inlet pipe via a pipe manifold, which distributes the discharge air across the cooled cooling air pipes. A seal is disposed upstream of an entrance to the HPP circuit to limit flow into the HPP circuit, and a second seal is disposed downstream of the HPP circuit at turbine wheelspace to limit ingestion and thus the purge flow air required. The circuit serves to reduce required purge flow in the HPP circuit so that an amount of compressor discharge air can be put back to the main flow path, thereby improving turbine performance.

    摘要翻译： 在具有压缩机排放壳体的燃气轮机中，冷却回路将压缩机排出的空气转向高压包装（HPP）回路。 冷却回路包括接收压缩机排出空气的入口管。 一个或几个冷却的冷却空气管通过管道歧管与入口管流体连通，管道歧管将排放空气分配在冷却的冷却空气管道上。 密封件设置在HPP回路入口的上游，以限制流入HPP回路的第二密封件，并且在涡轮机轮距处设置在HPP回路下游的第二密封件，以限制摄入量，从而限制吸入流量所需的空气流量。 该电路用于减少HPP电路中所需的清洗流量，使得压缩机排出空气的量可以放回到主流路，从而提高涡轮机性能。

    SEALS FOR REDUCING LEAKAGE IN ROTARY MACHINES
    5.
    发明申请
    SEALS FOR REDUCING LEAKAGE IN ROTARY MACHINES 审中-公开
    用于减少旋转机械中的泄漏的密封件

    公开(公告)号：US20130022459A1

    公开(公告)日：2013-01-24

    申请号：US13184592

    申请日：2011-07-18

    申请人： Omprakash Samudrala ,  Christopher Edward Wolfe ,  Raymond Edward Chupp

    发明人： Omprakash Samudrala ,  Christopher Edward Wolfe ,  Raymond Edward Chupp

    IPC分类号： F01D25/00 ,  F01D11/02 ,  F16J15/16 ,  F01D11/00 ,  F16J15/44 ,  F16J15/447

    CPC分类号： F01D11/12 ,  F01D11/001 ,  F01D11/003 ,  F05D2270/44

    摘要： A seal assembly for a rotary machine is provided. The seal assembly includes multiple sealing device segments disposed intermediate to a stationary housing and a rotor. Each of the segments includes at least one plate and a sealing element. The seal assembly also includes multiple inter-segment gaps formed between the multiple sealing device segments. Further, for each pair of adjacent sealing device segments, at least one pair of adjacent plates includes one plate overlapping another plate at an inter-segment gap.

    摘要翻译： 提供了一种用于旋转机器的密封组件。 密封组件包括设置在固定壳体和转子中间的多个密封装置段。 每个段包括至少一个板和密封元件。 密封组件还包括在多个密封装置段之间形成的多个跨段间隙。 此外，对于每对相邻的密封装置段，至少一对相邻的板包括在片段间隙处与另一个板重叠的一个板。

    Enhanced cloth seal
    8.
    发明授权
    Enhanced cloth seal 有权

    公开(公告)号：US10161523B2

    公开(公告)日：2018-12-25

    申请号：US13336750

    申请日：2011-12-23

    申请人： Neelesh Nandkumar Sarawate ,  David Wayne Weber ,  Omprakash Samudrala ,  Victor John Morgan

    发明人： Neelesh Nandkumar Sarawate ,  David Wayne Weber ,  Omprakash Samudrala ,  Victor John Morgan

    IPC分类号： F16J15/02 ,  F16J15/08 ,  F01D11/00

    摘要： The embodiments described herein provide a cloth seal for use with turbine components. The cloth seal includes first and second cloth layers. One or more central shims are positioned between the first and second cloth layers so as to block a leakage flow path. Another shim is positioned on and seals the opposite side of the first cloth layer from the one or more central shims positioned between the first and second cloth layers so as to block another leakage flow path. Yet another sealing shim may be positioned on the opposite side of the second cloth layer from the one or more central shims positioned between the first and second cloth layers to as to seal the opposite side of the second cloth layer and block another leakage flow path.

    ENHANCED CLOTH SEAL
    9.
    发明申请
    ENHANCED CLOTH SEAL 审中-公开
    增强衣服密封

    公开(公告)号：US20130161914A1

    公开(公告)日：2013-06-27

    申请号：US13336750

    申请日：2011-12-23

    申请人： Neelesh Nandkumar Sarawate ,  David Wayne Weber ,  Omprakash Samudrala ,  Victor John Morgan

    发明人： Neelesh Nandkumar Sarawate ,  David Wayne Weber ,  Omprakash Samudrala ,  Victor John Morgan

    IPC分类号： F16J15/02

    CPC分类号： F16J15/0812 ,  F01D11/006 ,  F05D2240/57 ,  F05D2300/6012

    摘要： The embodiments described herein provide a cloth seal for use with turbine components. The cloth seal includes first and second cloth layers. One or more central shims are positioned between the first and second cloth layers so as to block a leakage flow path. Another shim is positioned on and seals the opposite side of the first cloth layer from the one or more central shims positioned between the first and second cloth layers so as to block another leakage flow path. Yet another sealing shim may be positioned on the opposite side of the second cloth layer from the one or more central shims positioned between the first and second cloth layers to as to seal the opposite side of the second cloth layer and block another leakage flow path.

    摘要翻译： 本文所述的实施例提供了一种用于涡轮机部件的布密封件。 布密封件包括第一和第二布层。 一个或多个中心垫片位于第一和第二布层之间，以便阻止泄漏流动路径。 另一个垫片定位在第一布层的相对侧上并与第一和第二布层之间的一个或多个中心垫片密封，以便阻挡另一泄漏流动路径。 另一个密封垫片可以位于第二布层的与位于第一和第二布层之间的一个或多个中心垫片的相对侧上，以便密封第二布层的相对侧并阻挡另一泄漏流动路径。

    RETRACTABLE SEAL SYSTEM
    10.
    发明申请
    RETRACTABLE SEAL SYSTEM 有权
    可重复密封系统

    公开(公告)号：US20120286476A1

    公开(公告)日：2012-11-15

    申请号：US13104069

    申请日：2011-05-10

    申请人： Omprakash Samudrala ,  Siddarth Kumar ,  Gregory Crum ,  Karimulla Shaik Sha

    发明人： Omprakash Samudrala ,  Siddarth Kumar ,  Gregory Crum ,  Karimulla Shaik Sha

    IPC分类号： F16J15/44

    CPC分类号： F01D11/025 ,  F01D11/001 ,  F05D2240/56

    摘要： The present application thus provides a retractable seal system for use between a high pressure side and a low pressure side of a turbine engine. The retractable seal system may include a seal positioned in a slot of a stationary component, a pressure balance pocket positioned about the seal, and a conduit in communication with the pressure balance pocket and the high pressure side.

    摘要翻译： 因此，本申请提供了一种在涡轮发动机的高压侧和低压侧之间使用的可缩回的密封系统。 可伸缩密封系统可以包括定位在固定部件的槽中的密封件，围绕密封件定位的压力平衡袋以及与压力平衡袋和高压侧连通的导管。