Erosion and corrosion resistant coatings for exhaust gas recirculation based gas turbines
    1.
    发明授权
    Erosion and corrosion resistant coatings for exhaust gas recirculation based gas turbines 有权
    基于排气再循环的燃气轮机的侵蚀和耐腐蚀涂层

    公开(公告)号:US09365932B2

    公开(公告)日:2016-06-14

    申请号:US13528149

    申请日:2012-06-20

    IPC分类号: C23C30/00 F01D5/28

    摘要: A compressor blade for use in a compressor section of a gas turbine engine, comprising: a martensitic stainless steel compressor blade and an abrasive coating having an anodic component. The compressor blade has a blade portion, a dovetail portion and a platform portion intermediate the blade portion and the dovetail portion, the blade portion terminating in a tip opposite the dovetail portion. A cobalt-based coating overlies at least the blade portion of the compressor blade. The cobalt-based coating comprises a cobalt based material that includes precipitates of tungsten carbide that provide erosion resistance and particles of a sacrificial metal-based material distributed through the cobalt-based coating that provide galvanic corrosion resistance to the system.

    摘要翻译: 一种用于燃气涡轮发动机的压缩机部分的压缩机叶片,包括:马氏体不锈钢压缩机叶片和具有阳极组分的磨料涂层。 压缩机叶片具有叶片部分,燕尾部分和在叶片部分和燕尾部分之间的平台部分,叶片部分终止于与燕尾部分相对的尖端。 钴基涂层至少覆盖压缩机叶片的叶片部分。 钴基涂层包括钴基材料,其包括提供耐腐蚀性的碳化钨的沉淀物和分布在钴基涂层上的牺牲金属基材料的颗粒,其为系统提供电镀腐蚀性。

    Vanadium resistant coating system
    4.
    发明授权
    Vanadium resistant coating system 有权
    耐钒涂层系统

    公开(公告)号:US08337996B2

    公开(公告)日:2012-12-25

    申请号:US12951350

    申请日:2010-11-22

    IPC分类号: B21D39/00

    摘要: A vanadium resistant coating system resistant to high temperature vanadium attack. The system comprises a high temperature superalloy substrate. A bond coat overlies the superalloy substrate. The bond coat may be applied in multiple layers. A ceramic coating overlies the bond coat. The ceramic coating further comprises a zirconium oxide stabilized by at least one cation selected from the group consisting of Yb3+, Lu3+, Sc3+ and Ce4+, in the amounts of about 5-10 weight percent. An overcoat may overlie the ceramic coating. The overcoat may be a sacrificial layer of YSZ infiltrated with cations having an atomic radius larger than Y3+. Alternatively, the overcoat may comprise zirconium oxide stabilized by Ce4+.

    摘要翻译: 耐高温钒攻击的耐钒涂层体系。 该系统包括高温超合金基底。 粘合涂层覆盖在超合金基板上。 粘合涂层可以多层施用。 陶瓷涂层覆盖在粘结层上。 所述陶瓷涂层还包含以约5-10重量%的量由至少一种选自Yb3 +,Lu3 +,Sc3 +和Ce4 +的阳离子稳定的氧化锆。 外涂层可能覆盖陶瓷涂层。 外涂层可以是原子半径大于Y 3 +的阳离子渗透的YSZ的牺牲层。 或者,外涂层可以包括由Ce 4+稳定的氧化锆。

    Self-lubricating brush seal assembly and method of reducing leakage
    9.
    发明授权
    Self-lubricating brush seal assembly and method of reducing leakage 有权
    自润滑刷密封组件及减少泄漏的方法

    公开(公告)号:US09074487B2

    公开(公告)日:2015-07-07

    申请号:US13211473

    申请日:2011-08-17

    IPC分类号: F01D11/00 F16J15/32

    摘要: A self-lubricating brush seal assembly, for a power generation system and method of reducing air leakage in a power generation system including a plurality of self-lubricating members is provided. The plurality of self-lubricating members include a plurality of self-lubricating bristles, a plurality of cores sheathed in a self-lubricating braid, a plurality of cores having an outer diameter coated with self-lubricating material and a solid lubricating pack. The lubricating material is selected from graphite, hexagonal-boron nitrite (hBN), molybdenum disulfide (MoS2), tungsten disulfide (WS2), titanium nitride (TiN), titanium aluminum nitride (TiAlN), titanium carbonitride (TiCN), and combinations thereof.

    摘要翻译: 本发明提供一种自润滑刷密封组件,用于发电系统和减少包括多个自润滑构件的发电系统中的空气泄漏的方法。 多个自润滑构件包括多个自润滑刷毛,包覆在自润滑编织物中的多个芯,具有涂覆有自润滑材料的外径的多个芯和固体润滑包。 润滑材料选自石墨,六亚硼酸亚铁(hBN),二硫化钼(MoS2),二硫化钨(WS2),氮化钛(TiN),氮化钛(TiAlN),碳氮化钛(TiCN)及其组合 。

    EROSION AND CORROSION RESISTANT COATINGS FOR EXHAUST GAS RECIRCULATION BASED GAS TURBINES
    10.
    发明申请
    EROSION AND CORROSION RESISTANT COATINGS FOR EXHAUST GAS RECIRCULATION BASED GAS TURBINES 有权
    基于气体回收的气体涡轮机的耐腐蚀和耐腐蚀涂层

    公开(公告)号:US20130340403A1

    公开(公告)日:2013-12-26

    申请号:US13528149

    申请日:2012-06-20

    IPC分类号: B32B15/18 F02C3/34

    摘要: A compressor blade for use in a compressor section of a gas turbine engine, comprising: a martensitic stainless steel compressor blade and an abrasive coating having an anodic component. The compressor blade has a blade portion, a dovetail portion and a platform portion intermediate the blade portion and the dovetail portion, the blade portion terminating in a tip opposite the dovetail portion. A cobalt-based coating overlies at least the blade portion of the compressor blade. The cobalt-based coating comprises a cobalt based material that includes precipitates of tungsten carbide that provide erosion resistance and particles of a sacrificial metal-based material distributed through the cobalt-based coating that provide galvanic corrosion resistance to the system.

    摘要翻译: 一种用于燃气涡轮发动机的压缩机部分的压缩机叶片,包括:马氏体不锈钢压缩机叶片和具有阳极组分的磨料涂层。 压缩机叶片具有叶片部分,燕尾部分和在叶片部分和燕尾部分之间的平台部分,叶片部分终止于与燕尾部分相对的尖端。 钴基涂层至少覆盖压缩机叶片的叶片部分。 钴基涂层包括钴基材料,其包括提供耐腐蚀性的碳化钨的沉淀物和分布在钴基涂层上的牺牲金属基材料的颗粒,其为系统提供电镀腐蚀性。