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1.发明申请PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME 审中-公开气体涡轮发动机用保护涂层系统及其制造方法公开(公告)号：US20110305921A1
公开(公告)日：2011-12-15
申请号：US13173075
申请日：2011-06-30
CPC分类号： C23C30/00 , C23C18/1208 , C23C18/1216 , C23C18/1225 , C23C18/1229 , C23C18/1254 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/31 , F05D2300/611 , Y10T428/12611
摘要： Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary protective coating system comprises an aluminide-comprising bond coating disposed on a substrate, a thermal barrier coating overlying the aluminide-comprising bond coating, and a silicate layer interposed between the thermal barrier coating and the aluminide-comprising bond coating.
摘要翻译： 提供了用于燃气涡轮发动机应用的保护涂层系统以及用于制造这种保护涂层系统的方法。 示例性保护涂层系统包括设置在基底上的含铝化物粘合涂层，覆盖所述含铝化物粘合涂层的热障涂层以及置于所述热障涂层和所述含铝化物粘合涂层之间的硅酸盐层。
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2.发明授权Protective coating systems for gas turbine engine applications and methods for fabricating the same 失效用于燃气涡轮发动机应用的保护涂层系统及其制造方法公开(公告)号：US07993704B2
公开(公告)日：2011-08-09
申请号：US11950891
申请日：2007-12-05
CPC分类号： C23C30/00 , C23C18/1208 , C23C18/1216 , C23C18/1225 , C23C18/1229 , C23C18/1254 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/31 , F05D2300/611 , Y10T428/12611
摘要： Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary method of fabricating a protective coating system on a substrate comprises forming a bond coating on the substrate, forming a silicate layer on the bond coating, forming a thermal barrier coating overlying the silicate layer, and heating the thermal barrier coating.
摘要翻译： 提供了用于燃气涡轮发动机应用的保护涂层系统以及用于制造这种保护涂层系统的方法。 在衬底上制造保护涂层系统的示例性方法包括在衬底上形成粘合涂层，在粘结涂层上形成硅酸盐层，形成覆盖硅酸盐层的热障涂层，以及加热隔热涂层。
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3.发明申请公开(公告)号：US20090148628A1
公开(公告)日：2009-06-11
申请号：US11950891
申请日：2007-12-05
CPC分类号： C23C30/00 , C23C18/1208 , C23C18/1216 , C23C18/1225 , C23C18/1229 , C23C18/1254 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/31 , F05D2300/611 , Y10T428/12611
摘要： Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary method of fabricating a protective coating system on a substrate comprises forming a bond coating on the substrate, forming a silicate layer on the bond coating, forming a thermal barrier coating overlying the silicate layer, and heating the thermal barrier coating.
摘要翻译： 提供了用于燃气涡轮发动机应用的保护涂层系统以及用于制造这种保护涂层系统的方法。 在衬底上制造保护涂层系统的示例性方法包括在衬底上形成粘合涂层，在粘结涂层上形成硅酸盐层，形成覆盖硅酸盐层的热障涂层，以及加热隔热涂层。
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公开(公告)号：US09738533B2
公开(公告)日：2017-08-22
申请号：US12969390
申请日：2010-12-15
申请人： Derek Raybould , Christian Delacruz , Carl Kiser
发明人： Derek Raybould , Christian Delacruz , Carl Kiser
CPC分类号： C01B33/12 , C01B33/14 , C23C18/1216 , C23C18/1254 , C23C18/1283 , C23C18/1295
摘要： A coating for spark plugs and engine parts is resistant to fouling. The coating may be applied to the spark plug or engine part by dipping the part in a sol gel solution, ensuring it wets the part, and extracting it at a slow, controlled rate. As the part is allowed to dry, the sol gel reacts with moisture in the air to form a thin oxide film. Unlike conventional sol gel applications, which apply the oxide directly to the part, the present invention may form an oxide coating, in situ, while drying in place on the part.
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