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1.发明申请Device for a coating process, a retort, and a process for internal coating 审中-公开用于涂布工艺，蒸馏器和内部涂覆的方法的装置公开(公告)号：US20070089675A1
公开(公告)日：2007-04-26
申请号：US11543516
申请日：2006-10-05
IPC分类号： C23C16/00
CPC分类号： C23C8/04 , C23C10/04 , C23C14/046 , C23C16/045 , Y02T50/67
摘要： In internal coating processes there is often the problem that an outer surface of the component to be coated is also coated. The device according to the invention consists in the fact that the outer surface is protected by a robust outer envelope and a filling material between the component to be coated and the outer envelope.
摘要翻译： 在内部涂覆方法中，常常存在待涂覆的组分的外表面也被涂覆的问题。 根据本发明的装置在于外表面由坚固的外封套和待涂覆的部件与外封套之间的填充材料保护的事实。
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2.发明申请Filler for the Drilling of Through-Holes in Hollow Components, a Process and Apparatus Therefor 审中-公开用于在空心部件中钻孔的填料，其工艺和设备公开(公告)号：US20110132882A1
公开(公告)日：2011-06-09
申请号：US12958657
申请日：2010-12-02
CPC分类号： F01D5/005 , B23K26/389 , B23K26/40 , B23K2101/001 , B23K2103/172 , Y02T50/67 , Y10T428/2982
摘要： A filler made of glass beads is provided. The glass improves the absorption and the distribution of the energy of the beam such that an internal wall of the hollow component is not damaged. A process for producing a through-hole in a hollow component is provided. Also, an apparatus for laser drilling is provided.
摘要翻译： 提供由玻璃珠制成的填料。 该玻璃改善了梁的能量的吸收和分布，使得中空部件的内壁不被损坏。 提供了一种用于在中空部件中制造通孔的方法。 另外，提供了一种用于激光钻孔的装置。
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公开(公告)号：US20070186848A1
公开(公告)日：2007-08-16
申请号：US11653202
申请日：2007-01-12
摘要： The invention relates to a coating system, especially a low pressure plasma coating system, with at least one treatment chamber and a coating tool, especially a plasma spraying device, wherein at least one pump is provided for evacuation of the treatment chamber, which treatment chamber is formed to be temperature controllable. In addition there is a coating method for low pressure plasma coating with a temperature controlled and evacuated treatment chamber, in which a workpiece is coated by means of at least one coating tool. For acceleration of the coating process, especially the evacuating of the treatment chamber, it is proposed that at least the walls of the treatment chamber and/or the inside of the treatment chamber are temperature controlled at a temperature between 45° C. and 75° C.
摘要翻译： 本发明涉及一种具有至少一个处理室和涂覆工具，特别是等离子体喷涂装置的涂覆系统，特别是低压等离子体涂覆系统，其中提供至少一个用于抽出处理室的泵，该处理室 形成为温度可控的。 此外，还有一种用于低温等离子体涂层的涂覆方法，其具有温度控制和抽真空的处理室，其中通过至少一个涂覆工具涂覆工件。 为了加速涂覆过程，特别是处理室的抽空，建议至少将处理室的壁和/或处理室的内部温度控制在45℃和75℃之间的温度 C。
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4.发明申请Masking Material, Masking Layer, Process for Masking a Substrate and Process for Coating a Substrate 审中-公开掩模材料，掩蔽层，掩模基板的工艺和涂覆基板的工艺公开(公告)号：US20110135947A1
公开(公告)日：2011-06-09
申请号：US12958521
申请日：2010-12-02
IPC分类号： B32B15/04 , B05D1/12 , B05D1/18 , B05D1/28 , B05D1/36 , B05D5/00 , B32B18/00 , C04B35/00 , C04B35/46 , C04B35/443 , C04B35/465 , C04B35/10
CPC分类号： C23C28/00 , C23C4/02 , C23C16/042 , Y02T50/67 , Y02T50/6765
摘要： A two-layer system made of ceramic powder and metallic powder is provided. The ceramic powder may include zirconium oxide, aluminum oxide, titanium oxide, a perovskite, a spindle, a pyrochore and/or boron nitride and mixtures thereof. The metallic powder may include nickel, aluminum, cobalt and/or chromium, and mixtures or alloys thereof. A masking layer and a process for masking a substrate are also provided.
摘要翻译： 提供由陶瓷粉末和金属粉末制成的两层系统。 陶瓷粉末可以包括氧化锆，氧化铝，氧化钛，钙钛矿，锭子，煅烧炉和/或氮化硼及其混合物。 金属粉末可以包括镍，铝，钴和/或铬及其混合物或合金。 还提供掩蔽层和用于掩蔽衬底的工艺。
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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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6.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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7.发明申请Process for preparing turbine blades or vanes for a subsequent treatment, and associated turbine blade or vane 有权用于制备用于后续处理的涡轮机叶片或叶片以及相关联的涡轮叶片或叶片的方法公开(公告)号：US20100254818A1
公开(公告)日：2010-10-07
申请号：US11651706
申请日：2007-01-10
CPC分类号： F01D25/285 , C23C4/123 , C23C4/134 , C23C4/185 , Y02T50/67 , Y10T29/49336
摘要： Process for preparing turbine blades or vanes for a subsequent treatment, for example the application of a coating and/or a material-removing operation, wherein the turbine blade or vane has an airfoil, which is delimited at at least one end by an endplate with peripheral surfaces, wherein at least one of the peripheral surfaces is at least partially covered prior to the treatment of the turbine blade or vane. In the process a covering strip is fitted onto at least one peripheral surface to form a plug connection.
摘要翻译： 制备用于后续处理的涡轮机叶片或叶片的方法，例如施加涂层和/或材料去除操作，其中涡轮机叶片或叶片具有翼型件，该翼型件在至少一端处被端板限定， 周边表面，其中至少一个周边表面在处理涡轮叶片或叶片之前至少部分被覆盖。 在该过程中，将覆盖条安装在至少一个外围表面上以形成插头连接。
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8.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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9.发明申请Setting the quantity of cooling air for a turbine blade or vane by controlled overspray 有权通过受控的喷涂设置涡轮叶片或叶片的冷却空气量公开(公告)号：US20120094029A1
公开(公告)日：2012-04-19
申请号：US13274689
申请日：2011-10-17
CPC分类号： F01D5/288 , C23C4/01 , C23C4/12 , F01D5/005 , F05D2230/312 , F05D2230/90 , F05D2300/132 , F05D2300/2118 , F05D2300/611 , Y02T50/67
摘要： A process for coating an edge within a hole in a coated component is provided. The hole is a cooling-air hole operable conduct a coolant therethrough. According to the processes, an outer coating is provided on the outer surface of the component. An inner coating is provided on an inner surface within the hole, wherein the inner coating within the hole takes place using a coating nozzle at a different angle to the coating of the outer surface around the hole, if the spray angles for the outer coating and inner coating relate to the outer surface.
摘要翻译： 提供了一种在涂覆部件的孔内涂覆边缘的方法。 该孔是可冷却空气的冷却空气孔。 根据该方法，在组件的外表面上设置外涂层。 内部涂层设置在孔内的内表面上，其中如果外涂层的喷射角度和外涂层的喷射角度，则孔内的内涂层使用涂覆喷嘴以与外孔周围的外表面不同的角度发生， 内涂层涉及外表面。
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公开(公告)号：US20120027931A1
公开(公告)日：2012-02-02
申请号：US13146737
申请日：2010-01-08
IPC分类号： B05D1/02
摘要： A method for coating a substrate of a component is provided. Using the previous coating method, localized coating that can occur unexpectedly at one spot is often more difficult because the coating sequence must be reprogrammed here. This irregularity is resolved in a short period of time by a simple, manual coating.
摘要翻译： 提供一种涂覆部件的基板的方法。 使用以前的涂布方法，在一个点可能意外发生的局部涂层通常更困难，因为涂层顺序必须在这里重新编程。 这种不规则性在短时间内通过简单的手动涂层来解决。
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