TORCH IGNITER FOR A COMBUSTOR
    1.
    发明申请

    公开(公告)号:US20190032561A1

    公开(公告)日:2019-01-31

    申请号:US15664025

    申请日:2017-07-31

    IPC分类号: F02C7/266

    摘要: An igniter for a combustor of a turbomachine includes a fuel inlet in fluid communication with a mixing plenum. The mixing plenum is positioned upstream of a mixing channel. An air inlet is in fluid communication with the mixing plenum and an ignition source is in operative communication with the mixing channel. The igniter may include a mounting flange configured for coupling the igniter to the combustor. The ignition source may be positioned proximate to a downstream end of the mixing channel and upstream of the mounting flange. The mixing channel may define a venturi shape. The venturi shape includes a converging section between an upstream end of the mixing channel and a venturi throat.

    Torch igniter for a combustor
    2.
    发明授权

    公开(公告)号:US11519334B2

    公开(公告)日:2022-12-06

    申请号:US15664025

    申请日:2017-07-31

    摘要: An igniter for a combustor of a turbomachine includes a fuel inlet in fluid communication with a mixing plenum. The mixing plenum is positioned upstream of a mixing channel. An air inlet is in fluid communication with the mixing plenum and an ignition source is in operative communication with the mixing channel. The igniter may include a mounting flange configured for coupling the igniter to the combustor. The ignition source may be positioned proximate to a downstream end of the mixing channel and upstream of the mounting flange. The mixing channel may define a venturi shape. The venturi shape includes a converging section between an upstream end of the mixing channel and a venturi throat.

    TORCH IGNITER FOR A COMBUSTOR
    3.
    发明申请

    公开(公告)号:US20230045965A1

    公开(公告)日:2023-02-16

    申请号:US17975110

    申请日:2022-10-27

    摘要: An igniter for a combustor of a turbomachine includes a fuel inlet in fluid communication with a mixing plenum. The mixing plenum is positioned upstream of a mixing channel. An air inlet is in fluid communication with the mixing plenum and an ignition source is in operative communication with the mixing channel. The igniter may include a mounting flange configured for coupling the igniter to the combustor. The ignition source may be positioned proximate to a downstream end of the mixing channel and upstream of the mounting flange. The mixing channel may define a venturi shape. The venturi shape includes a converging section between an upstream end of the mixing channel and a venturi throat.