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    • 1. 发明授权
    • Field repairable high temperature smooth wear coating
    • 现场可修高温平滑磨损涂层
    • US07588797B2
    • 2009-09-15
    • US10819856
    • 2004-04-07
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • B05D1/26B05D1/40B05D1/42B05D7/14
    • C23C28/3215C23C24/08C23C28/321C23C28/325C23C28/345C23C28/3455C23C28/347Y02T50/67
    • A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has suffered localized damage to the thermal barrier coating. After cleaning the surface area of the component exposed by the localized spallation, a paste-like mixture of a ceramic composition comprising ceramic powders and nano-sized ceramic materials in a binder is applied to the surface area of the component, and is optionally smoothed using mechanical means. The composition is then allowed to dry and cure to form a dried coating having polymeric characteristics. Upon subsequent heating, the dried coating reacts to produce a glassy ceramic repair coating. Due to the thixotropic properties of the coating composition upon application to a component, the repair method can be performed in-situ while the component remains installed in its operating environment.
    • 用于修复设计用于恶劣热环境的部件上的热障涂层的化学组成和方法,例如燃气涡轮发动机的涡轮机,燃烧器和增压器部件。 该方法修复已经对热障涂层局部损坏的部件上的热障涂层。 在清洁通过局部剥离暴露的部件的表面积之后,将包含陶瓷粉末和纳米尺寸陶瓷材料的陶瓷组合物的粘合剂的糊状混合物施加到部件的表面区域,并且可选地使用 机械手段。 然后将组合物干燥并固化以形成具有聚合特性的干燥涂层。 随后加热,干燥的涂层反应生成玻璃状陶瓷修补涂层。 由于涂料组合物在施用于组分时的触变性能,可以在组分保持安装在其操作环境中时原位进行修复方法。
    • 2. 发明授权
    • Field repairable high temperature smooth wear coating
    • 现场可修高温平滑磨损涂层
    • US07842335B2
    • 2010-11-30
    • US11170471
    • 2005-06-29
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • B05D1/26B05D1/40B05D1/42B05D7/14
    • C23C24/08C09D1/00F01D5/288F05D2230/80F05D2230/90F23R2900/00019Y02T50/67Y02T50/671
    • A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has suffered localized damage to the thermal barrier coating. After cleaning the surface area of the component exposed by the localized spallation, a paste-like mixture of a ceramic composition comprising ceramic powders and nano-sized ceramic materials in a binder, further including an accelerant, is applied to the surface area of the component, and is optionally smoothed using mechanical means. The composition is then allowed to dry and cure to form a dried coating having polymeric characteristics. Upon subsequent heating, the dried coating reacts to produce a glassy ceramic repair coating. Due to the thixotropic properties of the coating composition upon application to a component, the repair method can be performed in-situ while the component remains installed in its operating environment.
    • 用于修复设计用于恶劣热环境的部件上的热障涂层的化学组成和方法,例如燃气涡轮发动机的涡轮机,燃烧器和增压器部件。 该方法修复已经对热障涂层局部损坏的部件上的热障涂层。 在清洁通过局部剥落暴露的部件的表面积之后,将包含陶瓷粉末和纳米尺寸陶瓷材料的陶瓷组合物的粘合剂中的还含有促进剂的糊状混合物施加到部件的表面区域 ,并且使用机械装置任选地平滑。 然后将组合物干燥并固化以形成具有聚合特性的干燥涂层。 随后加热,干燥的涂层反应生成玻璃状陶瓷修补涂层。 由于涂料组合物在施用于组分时的触变性能,可以在组分保持安装在其操作环境中时原位进行修复方法。
    • 3. 发明申请
    • Field repairable high temperature smooth wear coating
    • 现场可修高温平滑磨损涂层
    • US20070134408A1
    • 2007-06-14
    • US11170471
    • 2005-06-29
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellDavid E. Caldwell
    • B05D3/00B05D5/00B05D3/12B05D3/02
    • C23C24/08C09D1/00F01D5/288F05D2230/80F05D2230/90F23R2900/00019Y02T50/67Y02T50/671
    • A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has suffered localized damage to the thermal barrier coating. After cleaning the surface area of the component exposed by the localized spallation, a paste-like mixture of a ceramic composition comprising ceramic powders and nano-sized ceramic materials in a binder, further including an accelerant, is applied to the surface area of the component, and is optionally smoothed using mechanical means. The composition is then allowed to dry and cure to form a dried coating having polymeric characteristics. Upon subsequent heating, the dried coating reacts to produce a glassy ceramic repair coating. Due to the thixotropic properties of the coating composition upon application to a component, the repair method can be performed in-situ while the component remains installed in its operating environment.
    • 用于修复设计用于恶劣热环境的部件上的热障涂层的化学组成和方法,例如燃气涡轮发动机的涡轮机,燃烧器和增压器部件。 该方法修复已经对热障涂层局部损坏的部件上的热障涂层。 在清洁通过局部剥落暴露的部件的表面积之后,将包含陶瓷粉末和纳米尺寸陶瓷材料的陶瓷组合物的糊状混合物在粘合剂中,还包括促进剂,被施加到部件的表面区域 ,并且使用机械装置任选地平滑。 然后将组合物干燥并固化以形成具有聚合特性的干燥涂层。 随后加热,干燥的涂层反应生成玻璃状陶瓷修补涂层。 由于涂料组合物在施用于组分时的触变性能,可以在组分保持安装在其操作环境中时原位进行修复方法。
    • 6. 发明授权
    • Field repairable high temperature smooth wear coating
    • 现场可修高温平滑磨损涂层
    • US06827969B1
    • 2004-12-07
    • US10735359
    • 2003-12-12
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellTimothy Ray Lattire
    • Andrew Jay SkoogJane Ann MurphyWilliam Randolph StowellTimothy Ray Lattire
    • B05D102
    • C23C18/1208C23C18/04C23C18/06C23C18/127Y02T50/67
    • A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has suffered localized damage to the thermal barrier coating. After cleaning the surface area of the component exposed by the localized spallation, a mixture of a ceramic composition comprising a ceramic powder in a binder is applied, preferably by spraying, to the surface area of the component. The binder is then allowed to dry to form a dried coating. Upon subsequent heating, the dried coating reacts to produce a ceramic-containing repair coating, wherein the coating comprises the ceramic powder in a matrix of a material formed when the binder was reacted. The binder is preferably a ceramic precursor material that can be converted immediately to a ceramic or allowed to thermally decompose over time to form a ceramic. The repair method can be performed while the component remains installed, e.g., in a gas turbine engine. The chemical composition is a liquid mixture that comprises ceramic material in at least two particle size ranges, as well as a nano-sized ceramic material and a binder that imparts thixotropic properties to the coating composition upon application to a component.
    • 用于修复设计用于恶劣热环境的部件上的热障涂层的化学组成和方法,例如燃气涡轮发动机的涡轮机,燃烧器和增压器部件。 该方法修复已经对热障涂层局部损坏的部件上的热障涂层。 在清洁通过局部剥离暴露的部件的表面积之后,将包含粘合剂中的陶瓷粉末的陶瓷组合物的混合物优选地通过喷雾施加到部件的表面区域。 然后将粘合剂干燥以形成干燥的涂层。 随后加热,干燥的涂层反应生成含陶瓷的修复涂层,其中涂层包含陶瓷粉末,其为当粘合剂反应时形成的材料的基质。 粘合剂优选是陶瓷前体材料,其可以立即转化成陶瓷或随时间被热分解以形成陶瓷。 当部件保持安装时,例如在燃气涡轮发动机中,可以执行修理方法。 化学组成是包含至少两个粒度范围的陶瓷材料的液体混合物,以及纳米尺寸陶瓷材料和粘合剂,其在施用于组分时赋予涂料组合物触变性能。
    • 9. 发明申请
    • COMPOSITION AND METHOD FOR A THERMAL COATING SYSTEM
    • 热涂层系统的组成和方法
    • US20120148834A1
    • 2012-06-14
    • US13402565
    • 2012-02-22
    • Andrew Jay SkoogJane Ann Murphy
    • Andrew Jay SkoogJane Ann Murphy
    • B32B18/00B32B33/00B32B15/04
    • C23C24/00B05B5/043C23C4/12C23C4/18Y02T50/67Y02T50/6765Y10T428/26Y10T428/263Y10T428/264Y10T428/265
    • A thermal coating includes a substrate, a first coating layer, and a second coating layer. The substrate is selected from the group consisting of superalloys and ceramic matrix composites. The first coating layer comprises an alumina powder, a silica binder, and at least one additive selected from either a first group or a second group. The second coating layer comprises at least one of zinc titanate or cerium oxide. A method for applying a thermal coating system includes spraying a bond coat mixture onto a substrate using a liquid electrostatic sprayer. The bond coat mixture comprises an alumina powder, a silica binder, and at least one additive selected from either a first group or a second group. The method further includes applying a top coat mixture onto the bond coat mixture, wherein the top coat mixture comprises at least one of zinc titanate or cerium oxide.
    • 热涂层包括基底,第一涂层和第二涂层。 基材选自超级合金和陶瓷基复合材料。 第一涂层包含氧化铝粉末,二氧化硅粘合剂和至少一种选自第一组或第二组的添加剂。 第二涂层包含钛酸锌或氧化铈中的至少一种。 施加热涂覆系统的方法包括使用液体静电喷涂器将粘合涂层混合物喷涂到基底上。 粘合涂层混合物包含氧化铝粉末,二氧化硅粘合剂和至少一种选自第一组或第二组的添加剂。 该方法还包括将面漆混合物施加到粘合涂层混合物上,其中顶涂层混合物包含钛酸锌或氧化铈中的至少一种。