Hybrid Thermal Barrier Coating and Process of Making Same
    2.
    发明申请
    Hybrid Thermal Barrier Coating and Process of Making Same 审中-公开
    混合热障涂层及其制作方法

    公开(公告)号:US20160017475A1

    公开(公告)日:2016-01-21

    申请号:US14775031

    申请日:2013-12-30

    CPC classification number: C23C4/134 C23C4/11 C23C28/042

    Abstract: A thermal barrier coating is applied to a turbine engine component having a substrate. The thermal barrier coating has a first layer which has a strain tolerant columnar microstructure at an interface with the substrate for spallation resistance and a second layer which is porous conduction and radiation thermally resistant at an outer surface of the thermal barrier coating.

    Abstract translation: 将热障涂层施加到具有基底的涡轮发动机部件上。 热障涂层具有第一层,其在与基板的界面处具有耐应变的柱状微观结构,用于防剥离性,第二层是在热障涂层的外表面处是多孔传导和耐辐射的第二层。

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