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1.发明授权Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade 有权制备用于喷涂和安装涡轮叶片的涡轮叶片的方法公开(公告)号：US07717058B2
公开(公告)日：2010-05-18
申请号：US11518554
申请日：2006-09-08
IPC分类号： B05C21/00
摘要： The invention relates to a method of preparing turbine blades for spray coating their blade region that is subjected to the medium flowing through during operation in a spray coating apparatus, in which the turbine blade is inserted with its blade root into a cavity of a mounting in such a way that it protrudes with the blade region that adjoins the blade root from an opening of the cavity to form a gap between the rim of the opening and the turbine blade, and in which the gap is bridged by a shielding fixed on the mounting, which is characterized in that a shielding layer of a plastic which is resistant during the spray coating is used for the shielding, the shielding layer being arranged in such a way that it reaches up to the boundary between the blade root and the blade region.
摘要翻译： 本发明涉及一种制备涡轮机叶片的方法，用于在喷涂装置中在其操作期间经受介质流动的叶片区域喷涂其中，其中涡轮机叶片以其叶片根部插入安装的空腔中 这样一种方式使得其与从腔的开口邻接叶片根部的叶片区域突出，以在开口的边缘和涡轮叶片之间形成间隙，并且其中间隙由固定在安装件上的屏蔽物桥接 其特征在于，在喷涂期间耐用的塑料的屏蔽层用于屏蔽，屏蔽层以使其到达叶片根部和叶片区域之间的边界的方式布置。
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公开(公告)号：US20100086757A1
公开(公告)日：2010-04-08
申请号：US12518912
申请日：2007-09-21
CPC分类号： C23C4/12 , C23C4/134 , C23C28/042 , C23C28/048 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , F23M2900/05003 , F23M2900/05004 , F23R2900/00018 , Y02T50/67 , Y10T428/24975 , Y10T428/252
摘要： A method is provided for coating a component with a multilayer ceramic coating in which the individual layers of the ceramic coating are applied covering one another on the component, and in which ceramic particles are supplied to a coating burner, melted partly or completely by the coating burner, and deposited on the component. The ceramic particles have a particle size, which increases from layer to layer, and are supplied to the coating burner. Furthermore, a multilayer ceramic coating and a component which has with a multilayer ceramic coating are provided.
摘要翻译： 提供了一种用多层陶瓷涂层涂覆组分的方法，其中涂覆陶瓷涂层的各层彼此覆盖在组分上，并且其中将陶瓷颗粒供应到涂层燃烧器，部分或完全由涂层熔化 燃烧器，并沉积在组件上。 陶瓷颗粒具有从一层到另一层增加的粒度，并且被供应到涂料燃烧器。 此外，提供了多层陶瓷涂层和具有多层陶瓷涂层的部件。
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公开(公告)号：US20100255200A1
公开(公告)日：2010-10-07
申请号：US11653721
申请日：2007-01-12
IPC分类号： B05D1/32
CPC分类号： F01D5/288 , C23C4/01 , C23C4/11 , C23C4/129 , C23C4/134 , F05D2230/31 , F05D2230/90 , F05D2300/611 , Y02T50/67
摘要： The invention relates to a method for production of turbine components having at least one flow body, which has cooling air outlet openings arranged in the area of its trailing edge with the flow body, for example a blade section, being provided with an in particular ceramic coating by spraying coating. According to the invention, before the coating is applied, the cooling air outlet openings are completely covered by a covering strip which is composed of a material which is resistant to the coating process.
摘要翻译： 本发明涉及一种用于生产具有至少一个流动体的涡轮机部件的方法，所述流动体具有布置在其后缘区域中的冷却空气出口开口，流体主体（例如叶片部分）设置有特别是陶瓷 涂层喷涂。 根据本发明，在施加涂层之前，冷却空气出口开口完全被覆盖带覆盖，该覆盖条由耐涂层过程的材料组成。
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4.发明申请Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade 有权制备用于喷涂和安装涡轮叶片的涡轮叶片的方法公开(公告)号：US20070110910A1
公开(公告)日：2007-05-17
申请号：US11518554
申请日：2006-09-08
摘要： The invention relates to a method of preparing turbine blades for spray coating their blade region that is subjected to the medium flowing through during operation in a spray coating apparatus, in which the turbine blade is inserted with its blade root into a cavity of a mounting in such a way that it protrudes with the blade region that adjoins the blade root from an opening of the cavity to form a gap between the rim of the opening and the turbine blade, and in which the gap is bridged by a shielding fixed on the mounting, which is characterized in that a shielding layer of a plastic which is resistant during the spray coating is used for the shielding, the shielding layer being arranged in such a way that it reaches up to the boundary between the blade root and the blade region.
摘要翻译： 本发明涉及一种制备涡轮机叶片的方法，用于在喷涂装置中在其操作期间经受介质流动的叶片区域喷涂其中，其中涡轮机叶片以其叶片根部插入安装的空腔中 这样一种方式使得其与从腔的开口邻接叶片根部的叶片区域突出，以在开口的边缘和涡轮叶片之间形成间隙，并且其中间隙由固定在安装件上的屏蔽物桥接 其特征在于，在喷涂期间耐用的塑料的屏蔽层用于屏蔽，屏蔽层以使其到达叶片根部和叶片区域之间的边界的方式布置。
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