GAS TURBINE ENGINE MAINTENANCE METHOD
    28.
    发明申请

    公开(公告)号:US20180156062A1

    公开(公告)日:2018-06-07

    申请号:US15370360

    申请日:2016-12-06

    摘要: A method for inspecting a gas turbine engine using a maintenance tool includes assembling a plurality of rail segments of a rail system of the maintenance tool within a core air flowpath of the gas turbine engine. The gas turbine engine includes a compressor section, a combustion section, and a turbine section together defining at least in part the core air flowpath. The method also includes moving a maintenance head of the maintenance tool along the plurality of rail segments of the rail system to perform maintenance operations within the core air flowpath of the gas turbine engine.