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公开(公告)号：US20110177250A1
公开(公告)日：2011-07-21
申请号：US13119801
申请日：2009-08-11
摘要： An apparatus and a method for masking a component zone which is to be omitted by the spray jet during the thermal spraying of a component is disclosed. The apparatus can be elastically deformed at least partially at room temperature for attachment to the component. During the thermal spraying operation the apparatus has at least one inelastic region such that the impinging spray particles adhere to the surface thereof. After the thermal spraying operation, the apparatus can be removed from the covered component zone without leaving any residue. In this way, a simple, reusable solution is created, which avoids the disadvantages of the prior art.
摘要翻译： 公开了一种用于掩蔽组件区域的装置和方法，所述组件区域在组件的热喷涂期间将被喷射射线所省略。 该装置可以至少部分地在室温下弹性变形以附接到部件。 在热喷涂操作期间，该装置具有至少一个非弹性区域，使得冲击喷雾颗粒附着在其表面上。 在热喷涂操作之后，可以将设备从被覆盖的部件区域移除而不留下任何残留物。 以这种方式，创建了简单的可再利用的解决方案，这避免了现有技术的缺点。
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公开(公告)号：US20110014055A1
公开(公告)日：2011-01-20
申请号：US12834346
申请日：2010-07-12
摘要： The present invention relates to a method for producing a coating on a gas turbine component, in which particles at least of parts of a material to be applied as coating are accelerated by means of kinetic gas dynamic cold spraying in a spray jet onto the surface (2) of the component (1) to be coated, wherein a reactive gas is fed into the spray jet (6), so that the reactive gas reacts at least partially with the particles of the coating material when the particles impinge on the surface (2) to be coated and/or wherein the deposited layer (9) is heated locally and/or over a large area and impacted with a reactive gas, as well as a gas turbine component produced in this way.
摘要翻译： 本发明涉及一种在燃气轮机部件上制造涂层的方法，其中至少部分待涂覆的材料的颗粒通过喷雾喷射到表面上的动态气体动态冷喷涂而被加速（ 2），其中反应性气体被供给到喷射射流（6）中，使得当颗粒撞击在表面上时，反应气体至少部分地与涂层材料的颗粒反应（ 2）被涂覆和/或其中沉积层（9）被局部加热和/或大面积加热并与反应气体冲击，以及以这种方式制造的燃气轮机部件。
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公开(公告)号：US09040116B2
公开(公告)日：2015-05-26
申请号：US13509578
申请日：2010-11-11
CPC分类号： C23C24/04 , B05B7/205 , B05B15/50 , B05B15/55 , C04B41/009
摘要： A method for spraying a coating and a cold gas spray nozzle is disclosed. The method includes spraying a coating by the cold gas spray nozzle. A rinsing gas is fed to the cold gas spray nozzle during an interruption of the spraying or at an end of the spraying. Deposits in the cold gas spray nozzle are cooled and detached by the rinsing gas.
摘要翻译： 公开了喷涂涂层和冷气喷嘴的方法。 该方法包括通过冷气喷嘴喷涂涂层。 在喷雾中断期间或在喷雾结束时，冲洗气体被供给到冷气喷嘴。 冷气喷嘴中的沉积物被冲洗气体冷却和分离。
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公开(公告)号：US20120225213A1
公开(公告)日：2012-09-06
申请号：US13509578
申请日：2010-11-11
CPC分类号： C23C24/04 , B05B7/205 , B05B15/50 , B05B15/55 , C04B41/009
摘要： A method for spraying a coating and a cold gas spray nozzle is disclosed. The method includes spraying a coating by the cold gas spray nozzle. A rinsing gas is fed to the cold gas spray nozzle during an interruption of the spraying or at an end of the spraying. Deposits in the cold gas spray nozzle are cooled and detached by the rinsing gas.
摘要翻译： 公开了喷涂涂层和冷气喷嘴的方法。 该方法包括通过冷气喷嘴喷涂涂层。 在喷雾中断期间或在喷雾结束时，冲洗气体被供给到冷气喷嘴。 冷气喷嘴中的沉积物被冲洗气体冷却和分离。
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5.发明申请METHOD FOR PRODUCING A PLATING OF A VANE TIP AND CORRESPONDINGLY PRODUCED VANES AND GAS TURBINES 有权用于生产瓦楞和相应生产的瓦和气体涡轮机的方法公开(公告)号：US20120034092A1
公开(公告)日：2012-02-09
申请号：US13265606
申请日：2010-04-21
CPC分类号： F01D5/288 , C23C4/08 , C23C4/18 , C23C24/04 , F05D2230/30 , F05D2230/90 , Y10T29/49318 , Y10T29/49734
摘要： The invention relates to a method for producing a plating (5) of a vane tip. Said method consists of the following steps: a) a vane having a vane tip which is arranged opposite the base of the vane (2) and which comprises a surface which points radially outwards is provided, and b) a porous layer (7) is applied to at least the surface (4) of the vane tip and/or c) a bulge (8) which increases the surface of the vane tip is applied to at least one part of the flanks of the vane tip, said flanks surrounding the surface of the vane tip, and d) the plating (5) is applied to the porous layer and/or the bulge. The invention also relates to corresponding vanes or gas turbines with corresponding vanes.
摘要翻译： 本发明涉及一种用于生产叶片尖端的电镀（5）的方法。 所述方法包括以下步骤：a）具有与叶片（2）的底部相对设置并且包括径向向外指向的表面的叶片尖端的叶片，以及b）多孔层（7）是 至少施加到叶片尖端的表面（4）和/或c）将叶片尖端的表面增加的凸起（8）施加到叶片尖端的侧面的至少一部分，所述侧面围绕 叶片尖端的表面，以及d）将电镀（5）施加到多孔层和/或凸起。 本发明还涉及具有相应叶片的相应叶片或燃气轮机。
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公开(公告)号：US20110143039A1
公开(公告)日：2011-06-16
申请号：US13002313
申请日：2009-06-26
CPC分类号： C23C24/04
摘要： The invention relates to a process for cold spraying, wherein particles of at least one coating material, together with a carrier gas, are directed onto a surface of a workpiece to be coated by means of a spray gun. According to the invention, the particles of at least one coating material are preheated.
摘要翻译： 本发明涉及一种冷喷涂方法，其中至少一种涂料与载气一起的颗粒通过喷枪被引导到待涂覆的工件的表面上。 根据本发明，预热至少一种涂料的颗粒。
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7.发明授权Method for producing a plating of a vane tip and correspondingly produced vanes and gas turbines 有权用于制造叶片尖端和相应产生的叶片和燃气轮机的电镀的方法公开(公告)号：US09021696B2
公开(公告)日：2015-05-05
申请号：US13265606
申请日：2010-04-21
CPC分类号： F01D5/288 , C23C4/08 , C23C4/18 , C23C24/04 , F05D2230/30 , F05D2230/90 , Y10T29/49318 , Y10T29/49734
摘要： The invention relates to a method for producing a plating (5) of a vane tip. Said method consists of the following steps: a) a vane having a vane tip which is arranged opposite the base of the vane (2) and which comprises a surface which points radially outwards is provided, and b) a porous layer (7) is applied to at least the surface (4) of the vane tip and/or c) a bulge (8) which increases the surface of the vane tip is applied to at least one part of the flanks of the vane tip, said flanks surrounding the surface of the vane tip, and d) the plating (5) is applied to the porous layer and/or the bulge. The invention also relates to corresponding vanes or gas turbines with corresponding vanes.
摘要翻译： 本发明涉及一种用于生产叶片尖端的电镀（5）的方法。 所述方法包括以下步骤：a）具有与叶片（2）的底部相对设置并且包括径向向外指向的表面的叶片尖端的叶片，以及b）多孔层（7）是 至少施加到叶片尖端的表面（4）和/或c）将叶片尖端的表面增加的凸起（8）施加到叶片尖端的侧面的至少一部分，所述侧面围绕 叶片尖端的表面，以及d）将电镀（5）施加到多孔层和/或凸起。 本发明还涉及具有相应叶片的相应叶片或燃气轮机。
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公开(公告)号：US20130034661A1
公开(公告)日：2013-02-07
申请号：US13640677
申请日：2011-04-06
摘要： A method for processing a surface of a component, in particular in the aviation sector, including the following steps: spraying the component with a first powder and coating the component with a second powder, the first powder having the same chemical composition as the second powder.
摘要翻译： 一种用于处理特别是航空部门的部件的表面的方法，包括以下步骤：用第一粉末喷涂部件并用第二粉末涂覆部件，第一粉末具有与第二粉末相同的化学组成 。
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公开(公告)号：US20110223325A1
公开(公告)日：2011-09-15
申请号：US13128383
申请日：2009-11-07
CPC分类号： B05B15/045 , B05B12/20 , C23C24/04
摘要： A mask and method for kinetic cold gas compacting is disclosed. The mask includes a body for covering a not-to-be-coated region of a substrate to be coated having a work side exposed to a coating substance. The work side has a hardness such that the work side is not plastic deformable by a striking coating particle.
摘要翻译： 公开了用于动态冷气压实的掩模和方法。 掩模包括用于覆盖待涂覆的基底的未被涂覆区域的主体，其具有暴露于涂层物质的工作侧。 工作侧具有这样的硬度，使得工作侧不会被打击的涂层颗粒塑性变形。
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公开(公告)号：US08153274B2
公开(公告)日：2012-04-10
申请号：US12304978
申请日：2007-06-12
CPC分类号： C23C28/3215 , C23C28/322 , C23C28/325 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/90 , F05D2300/21 , F05D2300/2112 , F16L59/029 , Y02T50/67 , Y02T50/672 , Y10T428/12549 , Y10T428/12611 , Y10T428/12618 , Y10T428/26
摘要： A thermal barrier layer for metallic components, in particular for gas turbine components which are subject to high temperatures or hot gas, is disclosed. The thermal barrier layer includes an inner contact layer and an outer top layer, where the inner contact layer is applied to a surface of the component via an adhesion-promoting layer that is disposed therebetween, and between the outer top layer and the inner contact layer an intermediate layer is formed.
摘要翻译： 公开了用于金属部件的热障层，特别是用于经受高温或热气体的燃气轮机部件。 隔热层包括内接触层和外顶层，其中内接触层经由设置在其间的粘合促进层，以及在外顶层和内接触层之间施加到部件的表面 形成中间层。
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