ENHANCED ADHESION THERMAL BARRIER COATING
    146.
    发明申请

    公开(公告)号:US20170159460A1

    公开(公告)日:2017-06-08

    申请号:US14959057

    申请日:2015-12-04

    Abstract: A gas turbine engine including a compressor section, a combustor section fluidly connected to the compressor section, a turbine section fluidly connected to the combustor section, and a plurality of gas path components exposed to a primary fluid flowpath through the compressor section, the combustor section and the turbine section. At least one of the gas path components includes an exterior facing surface, a lattice structure extending outward from the exterior facing surface, the lattice structure being integral to the exterior facing surface, and a thermal barrier coating adhered to at least a portion of the exterior facing surface and the lattice structure.

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