TURBINE ENGINE, ENGINE STRUCTURE, AND METHOD OF FORMING AN ENGINE STRUCTURE WITH THERMAL BARRIER COATING PROTECTION
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    发明申请
    TURBINE ENGINE, ENGINE STRUCTURE, AND METHOD OF FORMING AN ENGINE STRUCTURE WITH THERMAL BARRIER COATING PROTECTION 审中-公开
    涡轮发动机,发动机结构和形成发动机结构与热障涂层保护的方法

    公开(公告)号:US20150068188A1

    公开(公告)日:2015-03-12

    申请号:US14023084

    申请日:2013-09-10

    IPC分类号: F01D25/00 F01D5/28

    摘要: A turbine engine, an engine structure, and a method of forming an engine structure are provided herein. In an embodiment, an engine structure includes a metal substrate, a thermal barrier coating layer, and a metal silicate protective layer. The thermal barrier coating layer overlies the metal substrate, and the thermal barrier coating layer has columnar grains with gaps defined between the columnar grains. The metal silicate protective layer is formed over the thermal barrier coating layer, and the metal silicate protective layer covers the columnar grains and the gaps between the columnar grains.

    摘要翻译: 涡轮发动机,发动机结构以及形成发动机结构的方法。 在一个实施例中,发动机结构包括金属基底,热障涂层和金属硅酸盐保护层。 隔热涂层位于金属基板上,隔热涂层具有在柱状晶粒之间具有间隙的柱状晶粒。 金属硅酸盐保护层形成在隔热涂层之上,金属硅酸盐保护层覆盖柱状晶粒和柱状晶粒之间的间隙。