Gas turbine diffuser with flow separator
    1.
    发明授权
    Gas turbine diffuser with flow separator 有权
    带流量分离器的燃气轮机扩散器

    公开(公告)号:US09239166B2

    公开(公告)日:2016-01-19

    申请号:US13663133

    申请日:2012-10-29

    CPC classification number: F23R3/26 F23R3/04 F23R2900/00016 Y10T29/49323

    Abstract: A diffuser for use in a gas turbine engine, the diffuser having a first wall, a second wall, and a flow separator. The first and second wall define an annular cavity, with the annular cavity having an inlet. The first and second wall also forming a prediffuser that is proximate the inlet, and a dump region distal the inlet. The flow separator extends from the first wall into the annular cavity.

    Abstract translation: 一种用于燃气涡轮发动机的扩散器,扩散器具有第一壁,第二壁和流动分离器。 第一和第二壁限定环形空腔,环形空腔具有入口。 第一和第二壁还形成靠近入口的预扩散器,以及远离入口的倾倒区域。 流动分离器从第一壁延伸到环形空腔中。

    GAS TURBINE DIFFUSER WITH FLOW SEPARATOR
    2.
    发明申请
    GAS TURBINE DIFFUSER WITH FLOW SEPARATOR 有权
    具有流量分离器的气体涡轮增压器

    公开(公告)号:US20140116056A1

    公开(公告)日:2014-05-01

    申请号:US13663133

    申请日:2012-10-29

    CPC classification number: F23R3/26 F23R3/04 F23R2900/00016 Y10T29/49323

    Abstract: A diffuser for use in a gas turbine engine, the diffuser having a first wall, a second wall, and a flow separator. The first and second wall define an annular cavity, with the annular cavity having an inlet. The first and second wall also forming a prediffuser that is proximate the inlet, and a dump region distal the inlet. The flow separator extends from the first wall into the annular cavity.

    Abstract translation: 一种用于燃气涡轮发动机的扩散器,扩散器具有第一壁,第二壁和流动分离器。 第一和第二壁限定环形空腔,环形空腔具有入口。 第一和第二壁还形成靠近入口的预扩散器,以及远离入口的倾倒区域。 流动分离器从第一壁延伸到环形空腔中。

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