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公开(公告)号:WO2014065928A3
公开(公告)日:2014-07-17
申请号:PCT/US2013054088
申请日:2013-08-08
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHROCK CHRISTOPHER W , MALONEY MICHAEL , LITTON DAVID A , ZIMMERMAN BENJAMIN JOSEPH , HAZEL BRIAN T
CPC classification number: C23C4/02 , C23C4/11 , C23C4/134 , C23C28/321 , C23C28/3215 , C23C28/3455 , C23C28/347 , F01D5/288 , F05D2300/13 , F05D2300/514 , Y10T428/249981 , Y10T428/31678
Abstract: A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.
Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板,沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料,所述环境污染物与外层接触以改变外层的微观结构。
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公开(公告)号:EP2893148A4
公开(公告)日:2015-11-04
申请号:EP13849810
申请日:2013-08-08
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHROCK CHRISTOPHER W , MALONEY MICHAEL , LITTON DAVID A , ZIMMERMAN BENJAMIN JOSEPH , HAZEL BRIAN T
CPC classification number: C23C4/02 , C23C4/11 , C23C4/134 , C23C28/321 , C23C28/3215 , C23C28/3455 , C23C28/347 , F01D5/288 , F05D2300/13 , F05D2300/514 , Y10T428/249981 , Y10T428/31678
Abstract: A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.
Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板,沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料,其与外层接触以改变外层的微观结构。
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