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1.发明授权Coating system and method for vibrational damping of gas turbine engine airfoils 有权燃气涡轮发动机翼型振动阻尼的涂层系统和方法公开(公告)号：US07250224B2
公开(公告)日：2007-07-31
申请号：US10711888
申请日：2004-10-12
申请人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
发明人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
CPC分类号： F01D5/26 , C23C14/027 , C23C14/0688 , F01D5/288 , F05D2230/31 , F05D2230/90 , F05D2300/141 , F05D2300/21 , Y10T428/12611 , Y10T428/12722 , Y10T428/12847 , Y10T428/12896 , Y10T428/12944
摘要： A coating system and coating method for damping vibration in an airfoil of a rotating component of a turbomachine. The coating system includes a metallic coating on a surface of the airfoil, and a ceramic coating overlying the metallic coating. The metallic coating contains metallic particles dispersed in a matrix having a metallic and/or intermetallic composition. The metallic particles are more ductile than the matrix, and have a composition containing silver and optionally tin. The method involves ion plasma cleaning the surface of the airfoil before depositing the metallic coating and then the ceramic coating.
摘要翻译： 一种用于阻尼涡轮机的旋转部件的翼型中的振动的涂布系统和涂布方法。 涂层系统包括在翼型件的表面上的金属涂层和覆盖金属涂层的陶瓷涂层。 金属涂层含有分散在具有金属和/或金属间组合物的基体中的金属颗粒。 金属颗粒比基体更具韧性，并且具有包含银和任选的锡的组合物。 该方法包括在沉积金属涂层然后陶瓷涂层之前离子等离子体清洁翼型件的表面。
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公开(公告)号：US08017195B2
公开(公告)日：2011-09-13
申请号：US11748625
申请日：2007-05-15
申请人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
发明人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
CPC分类号： F01D5/26 , C23C14/027 , C23C14/0688 , F01D5/288 , F05D2230/31 , F05D2230/90 , F05D2300/141 , F05D2300/21 , Y10T428/12611 , Y10T428/12722 , Y10T428/12847 , Y10T428/12896 , Y10T428/12944
摘要： A coating system and coating method for damping vibration in an airfoil of a rotating component of a turbomachine. The coating system includes a metallic coating on a surface of the airfoil, and a ceramic coating overlying the metallic coating. The metallic coating contains metallic particles dispersed in a matrix having a metallic and/or intermetallic composition. The metallic particles are more ductile than the matrix, and have a composition containing silver and optionally tin. The method involves ion plasma cleaning the surface of the airfoil before depositing the metallic coating and then the ceramic coating.
摘要翻译： 一种用于阻尼涡轮机的旋转部件的翼型中的振动的涂布系统和涂布方法。 涂层系统包括在翼型件的表面上的金属涂层和覆盖金属涂层的陶瓷涂层。 金属涂层含有分散在具有金属和/或金属间组合物的基体中的金属颗粒。 金属颗粒比基体更具韧性，并且具有包含银和任选的锡的组合物。 该方法包括在沉积金属涂层然后陶瓷涂层之前离子等离子体清洁翼型件的表面。
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3.发明申请COATING SYSTEM AND METHOD FOR VIBRATIONAL DAMPING OF GAS TURBINE ENGINE AIRFOILS 有权燃气轮机发动机振动阻尼涂层系统及方法公开(公告)号：US20100136254A1
公开(公告)日：2010-06-03
申请号：US11748625
申请日：2007-05-15
申请人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
发明人： Ramgopal Darolia , Matthew Mark Weaver , Dennis Martin Corbly , Boris Alexeevich Movchan , Anatolii Ivanovich Ustinov
IPC分类号： B05D3/10
CPC分类号： F01D5/26 , C23C14/027 , C23C14/0688 , F01D5/288 , F05D2230/31 , F05D2230/90 , F05D2300/141 , F05D2300/21 , Y10T428/12611 , Y10T428/12722 , Y10T428/12847 , Y10T428/12896 , Y10T428/12944
摘要： A coating system and coating method for damping vibration in an airfoil of a rotating component of a turbomachine. The coating system includes a metallic coating on a surface of the airfoil, and a ceramic coating overlying the metallic coating. The metallic coating contains metallic particles dispersed in a matrix having a metallic and/or intermetallic composition. The metallic particles are more ductile than the matrix, and have a composition containing silver and optionally tin. The method involves ion plasma cleaning the surface of the airfoil before depositing the metallic coating and then the ceramic coating.
摘要翻译： 一种用于阻尼涡轮机的旋转部件的翼型中的振动的涂布系统和涂布方法。 涂层系统包括在翼型件的表面上的金属涂层和覆盖金属涂层的陶瓷涂层。 金属涂层含有分散在具有金属和/或金属间组合物的基体中的金属颗粒。 金属颗粒比基体更具韧性，并且具有包含银和任选的锡的组合物。 该方法包括在沉积金属涂层然后陶瓷涂层之前离子等离子体清洁翼型件的表面。
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