ASYMMETRIC GAS TURBINE EXHAUST DIFFUSER
    1.
    发明申请

    公开(公告)号:US20180216495A1

    公开(公告)日:2018-08-02

    申请号:US15438996

    申请日:2017-02-22

    IPC分类号: F01D25/30 F02C3/04

    摘要: A gas turbine exhaust diffuser is configured to be at least partially disposed within an exhaust collector. The diffuser also includes an inner wall configured to extend to a back wall of the exhaust collector, an outer wall circumferentially disposed about the inner wall along a portion of the collector, and an inlet between the upstream end of the inner and outer walls. The inlet is configured to receive an exhaust flow from a gas turbine engine. An outlet for the exhaust is located between the inner wall and a downstream end of the outer wall. The outer wall is asymmetrically shaped so that an opening between the outlet and the back wall of the exhaust collector is larger on a first lateral side of the diffuser adjacent an exhaust exit of the collector than an opposite lateral side of the diffuser.

    Asymmetric gas turbine exhaust diffuser

    公开(公告)号:US10550729B2

    公开(公告)日:2020-02-04

    申请号:US15438996

    申请日:2017-02-22

    IPC分类号: F01D25/30 F02C3/04

    摘要: A gas turbine exhaust diffuser is configured to be at least partially disposed within an exhaust collector. The diffuser also includes an inner wall configured to extend to a back wall of the exhaust collector, an outer wall circumferentially disposed about the inner wall along a portion of the collector, and an inlet between the upstream end of the inner and outer walls. The inlet is configured to receive an exhaust flow from a gas turbine engine. An outlet for the exhaust is located between the inner wall and a downstream end of the outer wall. The outer wall is asymmetrically shaped so that an opening between the outlet and the back wall of the exhaust collector is larger on a first lateral side of the diffuser adjacent an exhaust exit of the collector than an opposite lateral side of the diffuser.