APPARATUS AND METHOD FOR SEALING TURBINE ASSEMBLY

    公开(公告)号:US20170114654A1

    公开(公告)日:2017-04-27

    申请号:US15301659

    申请日:2014-04-02

    Abstract: A turbine or turbine system includes a compressor, a combustor, a turbine section, a diffuser with a parting line between two components, and a seal along the parting line. The seal includes a protrusion, a recess, and a flexible portion between the protrusion and the recess. The flexible portion has a bent cross-section perpendicular to the parting line. An outer surface of the bent cross-section contacts an inner surface of the recess. An inner surface of the bent cross-section contacts an outer surface of the protrusion. Sealing a parting line between two parts of a diffuser in a gas turbine system includes disposing a flexible portion between a protrusion and a recess of the two parts, contacting an outer surface of the bent cross-section with an inner surface of the recess, contacting an inner surface of the bent cross-section with an outer surface of the protrusion, and pressurizing the diffuser.

    EXHAUST FRAME STRUT WITH COOLING FINS
    2.
    发明申请
    EXHAUST FRAME STRUT WITH COOLING FINS 审中-公开
    带有冷却活塞的排气框架

    公开(公告)号:US20170067365A1

    公开(公告)日:2017-03-09

    申请号:US14849112

    申请日:2015-09-09

    Abstract: A system is provided including a turbine exhaust section. The turbine exhaust section includes an exhaust flow path. The turbine exhaust section also includes an outer structure having an outer casing and an outer exhaust wall disposed along the exhaust flow path. An inner structure of the turbine exhaust section includes an inner exhaust wall disposed along the exhaust flow path. A strut extends between the outer structure and the inner structure, and the strut is configured to convey a flow of fluid from the inner structure toward the outer structure. The strut includes a plurality of cooling fins to facilitate heat transfer from the strut to the flow of fluid.

    Abstract translation: 提供了一种包括涡轮机排气部分的系统。 涡轮排气部包括排气流路。 涡轮机排气部还包括外部结构,其具有沿着排气流路设置的外壳和外排气壁。 涡轮排气部的内部结构包括沿排气流路设置的内排气壁。 支柱在外部结构和内部结构之间延伸,并且支柱构造成将流体流从内部结构传送到外部结构。 支柱包括多个冷却翅片,以便于从支柱到流体流的热传递。

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