ELECTROLYTE SEPARATOR AND METHOD OF MAKING THE ELECTROLYTE SEPARATOR
    11.
    发明申请
    ELECTROLYTE SEPARATOR AND METHOD OF MAKING THE ELECTROLYTE SEPARATOR 有权
    电解质分离器和制造电解质分离器的方法

    公开(公告)号:US20110236743A1

    公开(公告)日:2011-09-29

    申请号:US12730496

    申请日:2010-03-24

    CPC classification number: H01M2/1646 H01M10/39

    Abstract: An electrolyte separator structure is provided. The electrolyte separator structure comprises a graded integral structure, wherein the structure comprises an ion-conducting first ceramic at a first end and an electrically insulating second ceramic at a second end, wherein the difference in the coefficient of thermal expansion of the ion-conducting first ceramic and the electrically insulating second ceramic is less than or equal to about 5 parts per million per degrees Centigrade, and wherein at least one of the first ceramic or the second ceramic comprises a strengthening agent. Method of making the ion-separator structure is provided. Electrochemical cells comprising the ion-separator structure and method of making the electrochemical cell using the ion-separator structure are also provided.

    Abstract translation: 提供电解质分离器结构。 电解质分离器结构包括梯度整体结构,其中该结构包括在第一端处的离子传导第一陶瓷和在第二端处的电绝缘的第二陶瓷,其中离子导电的第一陶瓷的热膨胀系数的差异 陶瓷和电绝缘的第二陶瓷的含量小于或等于约百万分之一摄氏度,其中第一陶瓷或第二陶瓷中的至少一种包含增强剂。 提供了制备离子分离器结构的方法。 还提供了包括离子分离器结构的电化学电池和使用离子分离器结构制造电化学电池的方法。

    Erosion and corrosion resistant coatings for exhaust gas recirculation based gas turbines
    12.
    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

    Abstract: 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.

    Abstract translation: 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。

    Gas sensor and method of making
    15.
    发明授权
    Gas sensor and method of making 有权
    气体传感器及制作方法

    公开(公告)号:US07827852B2

    公开(公告)日:2010-11-09

    申请号:US11961092

    申请日:2007-12-20

    CPC classification number: G01N27/125 F02D41/146 F02D41/1476

    Abstract: A gas sensor is disclosed. The gas sensor includes a gas sensing layer including doped oxygen deficient tungsten oxide and a dopant selected from the group consisting of Re, Ni, Cr, V, W, and a combination thereof, at least one electrode positioned within a layer of titanium, and a response modification layer. The at least one electrode is in communication with the gas sensing layer and the gas sensing layer is capable of detecting at least one gas selected from the group consisting of NO, NO2, SOx O2, H2O, and NH3. A method of fabricating the gas sensor is also disclosed.

    Abstract translation: 公开了一种气体传感器。 气体传感器包括气体感测层,其包括掺杂的氧缺乏氧化钨和选自Re,Ni,Cr,V,W及其组合的掺杂剂,位于钛层内的至少一个电极,以及 响应修改层。 所述至少一个电极与所述气体感测层连通,并且所述气体感测层能够检测至少一种选自NO,NO 2,SO x O 2,H 2 O和NH 3的气体。 还公开了一种制造气体传感器的方法。

    EROSION AND CORROSION RESISTANT COATINGS FOR EXHAUST GAS RECIRCULATION BASED GAS TURBINES
    19.
    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

    Abstract: 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.

    Abstract translation: 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。

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