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1. 发明申请

US20100327213A1 TURBINE ENGINE COMPONENTS 有权
标题翻译：涡轮发动机组件
公开(公告)号：US20100327213A1
公开(公告)日：2010-12-30
申请号：US12495208
申请日：2009-06-30
申请人： Vladimir K. Tolpygo
发明人： Vladimir K. Tolpygo
IPC分类号： E04B1/76
CPC分类号： C04B35/495 , C04B35/488 , C04B35/4885 , C04B35/49 , C04B2235/3217 , C04B2235/3222 , C04B2235/3224 , C04B2235/3225 , C04B2235/3232 , C04B2235/3244 , C04B2235/3246 , C04B2235/3249 , C04B2235/3251 , C04B2235/3255 , C04B2235/76 , C04B2235/762 , C04B2235/764 , C04B2235/765 , C04B2235/80 , C04B2235/85 , C23C14/083 , C23C14/30 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C30/00 , F01D5/288 , F05D2230/90 , Y02T50/67
摘要： A thermal barrier coating is formed over the substrate. A majority of the thermal barrier coating comprises a multi-phase material comprising a polycrystalline material including two or more phases. Each phase forms an individual grain, adjacent individual grains are separated by grain boundaries, each phase comprises an oxide compound, the multi-phase material is formed from three or more constituents, the three or more constituents consist of different materials that are not completely soluble in each other, and the two or more phases are not completely soluble in each other and do not form only one compound.
摘要翻译：在衬底上形成热障涂层。大多数热障涂层包括多相材料，其包括包括两个或多个相的多晶材料。每相形成单个晶粒，相邻的单个晶粒由晶界分离，每相包含氧化物化合物，多相材料由三种或更多种组分形成，三种或更多种组分由不完全溶解的不同材料组成彼此之间，两相以上的相不完全相溶，不能仅形成一种化合物。

2. 发明授权

US08124246B2 Coated components and methods of fabricating coated components and coated turbine disks 有权
标题翻译：涂覆部件和制造涂层部件和涂覆涡轮盘的方法
公开(公告)号：US08124246B2
公开(公告)日：2012-02-28
申请号：US12273843
申请日：2008-11-19
申请人： Vladimir K. Tolpygo
发明人： Vladimir K. Tolpygo
IPC分类号： B32B15/04
CPC分类号： C23C10/38 , C23C10/02 , C23C10/28 , C23C10/60 , C25D3/50 , C25D5/34 , C25D5/50 , Y10T428/12458 , Y10T428/12493 , Y10T428/12931
摘要： Coated components and methods of fabricating coated components and coated turbine disks are provided. In an embodiment, by way of example only, a coated component includes a substrate comprising a superalloy in an unmodified form and a coating disposed over the substrate, where the coating comprises the superalloy in a modified form. The modified form of the superalloy includes, by weight, at least 10% more chromium and at least 10% more of one or more noble metals than the unmodified form of the superalloy, and the modified form of the superalloy is substantially free of aluminum.
摘要翻译：提供涂覆部件和制造涂覆部件和涂覆涡轮盘的方法。在一个实施例中，仅作为示例，涂覆部件包括包含未改性形式的超级合金的基体和设置在基底上的涂层，其中涂层包含改性形式的超级合金。超合金的改性形式包括比超合金的未改性形式重量更多的铬和至少10％以上的一种或多种贵金属，并且超合金的改性形式基本上不含铝。

3. 发明授权

US08605858B2 Methods and systems for inspecting structures for crystallographic imperfections 有权
标题翻译：检查晶体缺陷结构的方法和系统
公开(公告)号：US08605858B2
公开(公告)日：2013-12-10
申请号：US13169902
申请日：2011-06-27
申请人： Surendra Singh , Andy Szuromi , Vladimir K. Tolpygo , Andy Kinney
发明人： Surendra Singh , Andy Szuromi , Vladimir K. Tolpygo , Andy Kinney
IPC分类号： G01N23/207
CPC分类号： G01N23/207
摘要： Embodiments of methods and systems for inspecting a structure for a crystallographic imperfection are provided. In the method, an X-ray wavelength that is particularly susceptible to diffraction by the crystallographic imperfection is identified. Then an X-ray source is provided to emit X-rays in the identified X-ray wavelength. While placing the structure at a sequence of positions relative to the X-ray source, X-rays are directed at the structure in multiple, non-parallel arrays to create sequential patterns of diffracted X-rays. The patterns of diffracted X-rays are digitally captured and communicated to a computer that compares them to locate the crystallographic imperfection. For a surface imperfection, the imperfection may be marked with a target to allow for physical removal.
摘要翻译：提供了用于检查晶体缺陷的结构的方法和系统的实施例。在该方法中，识别出通过晶体缺陷特别容易衍射的X射线波长。然后提供X射线源以在所识别的X射线波长中发射X射线。当将结构放置在相对于X射线源的位置序列时，X射线被引导到多个非平行阵列中的结构以产生衍射X射线的顺序图案。衍射X射线的图案被数字捕获并传送到计算机，以比较它们以定位晶体学缺陷。对于表面缺陷，缺陷可以用目标标记以允许物理去除。

4. 发明授权

US08206117B2 Turbine components and methods of manufacturing turbine components 有权
标题翻译：涡轮机部件和制造涡轮机部件的方法
公开(公告)号：US08206117B2
公开(公告)日：2012-06-26
申请号：US11960099
申请日：2007-12-19
申请人： Thomas E. Strangman , Vladimir K. Tolpygo
发明人： Thomas E. Strangman , Vladimir K. Tolpygo
IPC分类号： F01D5/34
CPC分类号： F01D5/3007 , B23P15/006 , F05D2300/607 , Y10T29/49316 , Y10T29/49321
摘要： Turbine components are provided. In an embodiment, by way of example, a hub and a ring are included. The hub comprises a first material. The ring is bonded to the hub. The ring comprises a plurality of arc segments forming a ring, each arc segment comprising a second material comprising a single crystal superalloy material having a predetermined primary orientation and a predetermined secondary orientation, each predetermined primary orientation of each arc segment being substantially equal, and each predetermined secondary orientation of each arc segment being substantially equal, each arc segment adjacent another arc segment, and the adjacent arc segments having a predetermined crystallographic mismatch therebetween. Methods of manufacturing are also provided.
摘要翻译：提供涡轮机组件。在一个实施例中，作为示例，包括轮毂和环。轮毂包括第一材料。环结合到轮毂上。所述环包括形成环的多个弧段，每个弧段包括第二材料，所述第二材料包括具有预定主取向和预定二次取向的单晶超合金材料，每个弧段的每个预定主取向基本相等，每个弧段的预定次级取向基本相等，每个弧段相邻另一个弧段，并且相邻的弧段在它们之间具有预定的晶体失配。还提供了制造方法。

5. 发明授权

US08449994B2 Turbine engine components 有权
标题翻译：涡轮发动机部件
公开(公告)号：US08449994B2
公开(公告)日：2013-05-28
申请号：US12495208
申请日：2009-06-30
申请人： Vladimir K. Tolpygo
发明人： Vladimir K. Tolpygo
IPC分类号： F03D11/02 , F04D29/38 , B64C11/16 , F01D5/14 , B32B27/32 , B32B9/00 , B32B15/04 , B32B19/00
CPC分类号： C04B35/495 , C04B35/488 , C04B35/4885 , C04B35/49 , C04B2235/3217 , C04B2235/3222 , C04B2235/3224 , C04B2235/3225 , C04B2235/3232 , C04B2235/3244 , C04B2235/3246 , C04B2235/3249 , C04B2235/3251 , C04B2235/3255 , C04B2235/76 , C04B2235/762 , C04B2235/764 , C04B2235/765 , C04B2235/80 , C04B2235/85 , C23C14/083 , C23C14/30 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C30/00 , F01D5/288 , F05D2230/90 , Y02T50/67
摘要： A thermal barrier coating is formed over the substrate. A majority of the thermal barrier coating comprises a multi-phase material comprising a polycrystalline material including two or more phases. Each phase forms an individual grain, adjacent individual grains are separated by grain boundaries, each phase comprises an oxide compound, the multi-phase material is formed from three or more constituents, the three or more constituents consist of different materials that are not completely soluble in each other, and the two or more phases are not completely soluble in each other and do not form only one compound.
摘要翻译：在衬底上形成热障涂层。大多数热障涂层包括多相材料，其包括包括两个或多个相的多晶材料。每相形成单个晶粒，相邻的单个晶粒由晶界分离，每相包含氧化物化合物，多相材料由三种或更多种组分形成，三种或更多种组分由不完全溶解的不同材料组成彼此之间，两相以上的相不完全相溶，不能仅形成一种化合物。

6. 发明申请

US20120328079A1 METHODS AND SYSTEMS FOR INSPECTING STRUCTURES FOR CRYSTALLOGRAPHIC IMPERFECTIONS 有权
标题翻译：用于检查晶体显示结构的方法和系统
公开(公告)号：US20120328079A1
公开(公告)日：2012-12-27
申请号：US13169902
申请日：2011-06-27
申请人： Surendra Singh , Andy Szuromi , Vladimir K. Tolpygo , Andy Kinney
发明人： Surendra Singh , Andy Szuromi , Vladimir K. Tolpygo , Andy Kinney
IPC分类号： G01N23/207
CPC分类号： G01N23/207
摘要： Embodiments of methods and systems for inspecting a structure for a crystallographic imperfection are provided. In the method, an X-ray wavelength that is particularly susceptible to diffraction by the crystallographic imperfection is identified. Then an X-ray source is provided to emit X-rays in the identified X-ray wavelength. While placing the structure at a sequence of positions relative to the X-ray source, X-rays are directed at the structure in multiple, non-parallel arrays to create sequential patterns of diffracted X-rays. The patterns of diffracted X-rays are digitally captured and communicated to a computer that compares them to locate the crystallographic imperfection. For a surface imperfection, the imperfection may be marked with a target to allow for physical removal.
摘要翻译：提供了用于检查晶体缺陷的结构的方法和系统的实施例。在该方法中，识别出通过晶体缺陷特别容易衍射的X射线波长。然后提供X射线源以在所识别的X射线波长中发射X射线。当将结构放置在相对于X射线源的位置序列时，X射线被引导到多个非平行阵列中的结构以产生衍射X射线的顺序图案。衍射X射线的图案被数字捕获并传送到计算机，以比较它们以定位晶体学缺陷。对于表面缺陷，缺陷可以用目标标记以允许物理去除。

7. 发明申请

US20120090736A1 COATED COMPONENTS AND METHODS OF FABRICATING COATED COMPONENTS AND COATED TURBINE DISKS 审中-公开
标题翻译：涂层组件和涂覆组件和涂层涡轮盘的方法
公开(公告)号：US20120090736A1
公开(公告)日：2012-04-19
申请号：US13341259
申请日：2011-12-30
申请人： Vladimir K. Tolpygo
发明人： Vladimir K. Tolpygo
IPC分类号： C23C10/00 , C23C10/60 , C23C28/02
CPC分类号： C23C10/38 , C23C10/02 , C23C10/28 , C23C10/60 , C25D3/50 , C25D5/34 , C25D5/50 , Y10T428/12458 , Y10T428/12493 , Y10T428/12931
摘要： Coated components and methods of fabricating coated components and coated turbine disks are provided. In an embodiment, by way of example only, a coated component includes a substrate comprising a superalloy in an unmodified form and a coating disposed over the substrate, where the coating comprises the superalloy in a modified form. The modified form of the superalloy includes, by weight, at least 10% more chromium and at least 10% more of one or more noble metals than the unmodified form of the superalloy, and the modified form of the superalloy is substantially free of aluminum
摘要翻译：提供涂覆部件和制造涂覆部件和涂覆涡轮盘的方法。在一个实施例中，仅作为示例，涂覆部件包括包含未改性形式的超级合金的基体和设置在基底上的涂层，其中涂层包含改性形式的超级合金。超合金的改性形式包括比超合金的未改性形式多至少10％的铬和至少10％的一种或多种贵金属，并且该超级合金的改性形式基本上不含铝

8. 发明申请

US20100124670A1 COATED COMPONENTS AND METHODS OF FABRICATING COATED COMPONENTS AND COATED TURBINE DISKS 有权
标题翻译：涂层组件和涂覆组件和涂层涡轮盘的方法
公开(公告)号：US20100124670A1
公开(公告)日：2010-05-20
申请号：US12273843
申请日：2008-11-19
申请人： Vladimir K. Tolpygo
发明人： Vladimir K. Tolpygo
IPC分类号： H01B12/00 , C23C10/28 , C23C28/00
CPC分类号： C23C10/38 , C23C10/02 , C23C10/28 , C23C10/60 , C25D3/50 , C25D5/34 , C25D5/50 , Y10T428/12458 , Y10T428/12493 , Y10T428/12931
摘要： Coated components and methods of fabricating coated components and coated turbine disks are provided. In an embodiment, by way of example only, a coated component includes a substrate comprising a superalloy in an unmodified form and a coating disposed over the substrate, where the coating comprises the superalloy in a modified form. The modified form of the superalloy includes at least 10% more chromium and at least 10% more of one or more noble metals than the unmodified form of the superalloy, and the modified form of the superalloy is substantially free of aluminum.
摘要翻译：提供涂覆部件和制造涂覆部件和涂覆涡轮盘的方法。在一个实施例中，仅作为示例，涂覆部件包括包含未改性形式的超级合金的基体和设置在基底上的涂层，其中涂层包含改性形式的超级合金。超合金的改性形式包括比超合金的未改性形式多至少10％的铬和至少10％的一种或多种贵金属，并且超合金的改性形式基本上不含铝。

9. 发明申请

US20090162205A1 TURBINE COMPONENTS AND METHODS OF MANUFACTURING TURBINE COMPONENTS 有权
标题翻译：涡轮机组件及制造涡轮机组件的方法
公开(公告)号：US20090162205A1
公开(公告)日：2009-06-25
申请号：US11960099
申请日：2007-12-19
申请人： Thomas E. Strangman , Vladimir K. Tolpygo
发明人： Thomas E. Strangman , Vladimir K. Tolpygo
IPC分类号： F01D5/30 , B23P15/04 , F01D5/14
CPC分类号： F01D5/3007 , B23P15/006 , F05D2300/607 , Y10T29/49316 , Y10T29/49321
摘要： Turbine components are provided. In an embodiment, by way of example, a hub and a ring are included. The hub comprises a first material. The ring is bonded to the hub. The ring comprises a plurality of arc segments forming a ring, each arc segment comprising a second material comprising a single crystal superalloy material having a predetermined primary orientation and a predetermined secondary orientation, each predetermined primary orientation of each arc segment being substantially equal, and each predetermined secondary orientation of each arc segment being substantially equal, each arc segment adjacent another arc segment, and the adjacent arc segments having a predetermined crystallographic mismatch therebetween. Methods of manufacturing are also provided.
摘要翻译：提供涡轮机组件。在一个实施例中，作为示例，包括轮毂和环。轮毂包括第一材料。环结合到轮毂上。环包括形成环的多个弧段，每个弧段包括第二材料，第二材料包括具有预定主要取向和预定次要取向的单晶超合金材料，每个弧段的每个预定主要取向基本相等，每个弧段的预定次级取向基本相等，每个弧段相邻另一个弧段，并且相邻的弧段在它们之间具有预定的晶体失配。还提供了制造方法。

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