INLET FRAME FOR A GAS TURBINE ENGINE
    2.
    发明申请

    公开(公告)号:US20190048797A1

    公开(公告)日:2019-02-14

    申请号:US16028617

    申请日:2018-07-06

    IPC分类号: F02C7/04 F04D29/70 F04D29/063

    摘要: An inlet frame and a method of additively manufacturing the same are provided. The inlet frame includes a forward annular body spaced apart from a rear annular body to define an inlet passageway in fluid communication with a compressor inlet. The inlet frame may define integral wash manifolds and discharge ports for directing a flow of wash fluid directly through the compressor inlet. In addition, inlet frame may define one or more integral annular heating plenums in fluid communication with a hot air source for heating regions of the inlet frame that are prone to icing conditions.