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1. 发明授权

US08061965B2 Ring structure of metal construction having a run-in lining 失效
标题翻译：金属结构的环形结构具有磨合衬里
公开(公告)号：US08061965B2
公开(公告)日：2011-11-22
申请号：US11578862
申请日：2005-02-28
申请人： Manfred A. Daeubler , Horst Mueller-Wittek, legal representative , Renate Mendritzki, legal representative , Ulrike Hain , Werner Humhauser
发明人： Manfred A. Daeubler , Ulrike Hain , Werner Humhauser
IPC分类号： F01D11/08
CPC分类号： F01D11/122 , F01D11/127 , F05D2230/236 , F05D2230/237 , F05D2230/238 , F05D2250/283 , F05D2300/601
摘要： A ring structure with a metal design for a moving blade of axially flowed through compressor and turbine stages, particularly in gas turbine engines is provided. The ring structure includes a circular ring-shaped outer wall, a circular ring-shaped inner wall, which is located at a short radial distance from the moving blade tips, and includes a joining structure provided in the form of hollow chamber structure between the outer wall and the inner wall. The outer wall is provided in the form of a closed, mechanically stable housing wall of the compressor or turbine stage, and the joining structure provided in the form of hollow chamber structure is joined in a fixed manner to the outer wall and to the inner wall, for example, by soldering, diffusion welding or other joining techniques. The inner wall is provided in the form of a closed, mechanically stable structure, which serves as a run-in lining for the moving blade tips and which is made of a metal woven fabric and/or of a metal felt.
摘要翻译：提供了一种具有金属设计的环形结构，用于轴向流过压缩机和涡轮级的动叶片，特别是在燃气涡轮发动机中。环形结构包括圆形环形外壁，圆形环形内壁，其位于距活动叶片尖端短的径向距离处，并且包括以中空室结构的形式设置在外部的外部的接合结构墙壁和内壁。外壁以压缩机或涡轮机台的封闭的，机械稳定的壳体壁的形式提供，并且以中空室结构的形式提供的接合结构以固定的方式连接到外壁和内壁例如，通过焊接，扩散焊接或其它接合技术。内壁以闭合的，机械稳定的结构的形式提供，其用作活动叶片尖端的延伸衬里，其由金属织物和/或金属毡制成。

2. 发明授权

US08895134B2 Apparatus and method for coating a compressor housing 有权
标题翻译：用于涂覆压缩机壳体的装置和方法
公开(公告)号：US08895134B2
公开(公告)日：2014-11-25
申请号：US11631032
申请日：2005-04-29
申请人： Wilfried Smarsly , Renate Mendritzki , Horst Mueller-Wittek
发明人： Manfred Daeubler , Wilfried Smarsly
IPC分类号： B32B3/30 , F02K3/00 , F02C1/00 , F01D11/12
CPC分类号： F01D11/125 , F01D11/122 , F05D2300/614 , Y10T428/24355 , Y10T428/24521 , Y10T428/24537 , Y10T428/24612
摘要： A running-in coating for a compressor housing is disclosed. The running-in coating has at least two layers where a first layer is dimensionally stable and at least one additional layer has run-in capability.
摘要翻译：公开了一种用于压缩机壳体的流入式涂层。进入涂层具有至少两层，其中第一层是尺寸稳定的，并且至少一个附加层具有渗入能力。

3. 发明授权

US09303522B2 Method of repairing run-in coatings 有权
标题翻译：修补磨损涂层的方法
公开(公告)号：US09303522B2
公开(公告)日：2016-04-05
申请号：US12308523
申请日：2007-06-14
申请人： Manfred A. Daeubler , Horst Mueller-Wittek , Renate Mendritzki , André Werner , Heinrich Walter
发明人： Manfred A. Daeubler , André Werner , Heinrich Walter
IPC分类号： B05D3/00 , B32B43/00 , F01D11/12 , B23P6/00 , C23C10/16 , C23C10/18 , C23C26/00
CPC分类号： F01D11/12 , B23P6/007 , C23C10/16 , C23C10/18 , C23C26/00 , F05C2201/0463 , F05C2201/0466 , F05D2220/762 , F05D2230/10 , F05D2230/22 , F05D2230/30 , F05D2230/40 , F05D2230/80 , F05D2300/11 , F05D2300/224 , F05D2300/228
摘要： A method for repairing run-in coatings is provided. The method includes the steps of filling a damaged site of the run-in coating with a filling material having a material composition that corresponds to a material composition of the run-in coating or is comparable to the material composition of the run-in coating or having material properties that are comparable to material properties of the run-in coating; drying the filling material that has been filled into the damaged site; depositing a donor diffusion layer over an area of the damaged site and onto the dried filling material; and thermally treating the run-in coating at least in the area of the damaged site to locally diffuse at least one metallic element from the donor diffusion layer into the filling material.
摘要翻译：提供了修补磨损涂层的方法。该方法包括以下填充材料的填充材料的填充材料的填充损伤部位的步骤：材料组成与导入涂层的材料组成相对应，或者可以与渗入涂层的材料组成相当具有与外加涂层的材料性能相当的材料性质; 干燥已填充到损坏场所的填充材料; 在受损部位的区域上沉积供体扩散层，并将其施加到干燥的填充材料上; 以及至少在受损部位的区域热处理所述接合涂层，以将至少一种金属元素从所述供体扩散层局部扩散到所述填充材料中。

4. 发明申请

US20090263239A1 Ring structure with a metal design having a run-in lining 失效
标题翻译：具有金属设计的环形结构具有磨合衬里
公开(公告)号：US20090263239A1
公开(公告)日：2009-10-22
申请号：US11578862
申请日：2005-02-28
申请人： Manfred A. Daeubler , Horst Mueller-Wittek , Renate Mendritzki , Ulrike Hain , Werner Humhauser
发明人： Manfred A. Daeubler , Horst Mueller-Wittek , Renate Mendritzki , Ulrike Hain , Werner Humhauser
IPC分类号： F04D29/52
CPC分类号： F01D11/122 , F01D11/127 , F05D2230/236 , F05D2230/237 , F05D2230/238 , F05D2250/283 , F05D2300/601
摘要： A ring structure with a metal design for a moving blade of axially flowed through compressor and turbine stages, particularly in gas turbine engines is provided. The ring structure includes a circular ring-shaped outer wall, a circular ring-shaped inner wall, which is located at a short radial distance from the moving blade tips, and includes a joining structure provided in the form of hollow chamber structure between the outer wall and the inner wall. The outer wall is provided in the form of a closed, mechanically stable housing wall of the compressor or turbine stage, and the joining structure provided in the form of hollow chamber structure is joined in a fixed manner to the outer wall and to the inner wall, for example, by soldering, diffusion welding or other joining techniques. The inner wall is provided in the form of a closed, mechanically stable structure, which serves as a run-in lining for the moving blade tips and which is made of a metal woven fabric and/or of a metal felt.
摘要翻译：提供了一种具有金属设计的环形结构，用于轴向流过压缩机和涡轮级的动叶片，特别是在燃气涡轮发动机中。环形结构包括圆形环形外壁，圆形环形内壁，其位于距活动叶片尖端短的径向距离处，并且包括以中空室结构的形式设置在外部的外部的接合结构墙壁和内壁。外壁以压缩机或涡轮机台的封闭的，机械稳定的壳体壁的形式提供，并且以中空室结构的形式提供的接合结构以固定的方式连接到外壁和内壁例如，通过焊接，扩散焊接或其它接合技术。内壁以闭合的，机械稳定的结构的形式提供，其用作活动叶片尖端的穿入衬里，并且由金属织物和/或金属毡制成。

5. 发明申请

US20110020560A1 Method for Manufacturing a Run-In Coating 审中-公开
标题翻译：润滑涂层的制造方法
公开(公告)号：US20110020560A1
公开(公告)日：2011-01-27
申请号：US12086110
申请日：2006-11-30
申请人： Manfred Daeubler , Horst Mueller-Wittek
发明人： Manfred Daeubler , Horst Mueller-Wittek
IPC分类号： C23C4/18 , B05D3/02 , B05D3/10
CPC分类号： C23C4/18 , C23C4/06 , F01D11/122 , F05D2230/30 , F05D2230/31 , F05D2230/40
摘要： A method for the production of a run-in coating is provided, whereby a metallic run-in coating material is provided on a component on the stator side of a turbomachine, especially a gas turbine. According to an embodiment of the invention, the provided run-in coating undergoes a heat treatment for purposes of improving its run-in characteristics.
摘要翻译：提供了一种用于生产磨损涂层的方法，由此在涡轮机，特别是燃气轮机的定子侧上的部件上设置有金属导入涂层材料。根据本发明的一个实施方案，为提高其渗入特性的目的，所提供的浸入式涂层经受热处理。

6. 发明申请

US20090214824A1 Apparatus and method for coating a compressor housing 有权
标题翻译：用于涂覆压缩机壳体的装置和方法
公开(公告)号：US20090214824A1
公开(公告)日：2009-08-27
申请号：US11631032
申请日：2005-04-29
申请人： Manfred Daeubler , Renate Mendritzki , Horst Mueller-Wittek , Wilfried Smarsly
发明人： Manfred Daeubler , Renate Mendritzki , Horst Mueller-Wittek , Wilfried Smarsly
IPC分类号： B32B5/00 , B32B5/02 , B05D1/36
CPC分类号： F01D11/125 , F01D11/122 , F05D2300/614 , Y10T428/24355 , Y10T428/24521 , Y10T428/24537 , Y10T428/24612
摘要： A running-in coating for a compressor housing is disclosed. The running-in coating has at least two layers where a first layer is dimensionally stable and at least one additional layer has run-in capability.
摘要翻译：公开了一种用于压缩机壳体的流入式涂层。进入涂层具有至少两层，其中第一层是尺寸稳定的，并且至少一个附加层具有渗入能力。

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