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1.发明申请公开(公告)号：US20070141298A1
公开(公告)日：2007-06-21
申请号：US10575695
申请日：2004-09-30
IPC分类号： B32B3/02
CPC分类号： C22C47/025 , C22C47/00 , C22C47/20 , Y10T428/12444 , Y10T428/21 , Y10T428/211 , Y10T428/218
摘要： The invention relates to a composite material which is formed of several assembled discs of matrix material, wherein preferably in each disc at least one groove is formed in which at least one fiber (14) is inserted. According to the invention a composite of matrix material and fiber (14) is present in an inner section (16), whereas the matrix material is exclusively present in an outer section (17), wherein the fibers (14) reach to different extents into the outer section (17), in which the matrix material is exclusively present, for a strength optimizing intermeshing of the inner section (16) with the outer section (17).
摘要翻译： 本发明涉及一种复合材料，其由多个基体材料的组装盘形成，其中优选在每个盘中形成有至少一个纤维（14）插入至少一个槽。 根据本发明，基体材料和纤维（14）的复合物存在于内部部分（16）中，而基质材料仅存在于外部部分（17）中，其中纤维（14）达到不同的程度 其中仅存在基质材料的外部部分（17）用于内部部分（16）与外部部分（17）的强度优化相互啮合。
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2.发明授权公开(公告)号：US07524566B2
公开(公告)日：2009-04-28
申请号：US10575695
申请日：2004-09-30
IPC分类号： B32B15/14
CPC分类号： C22C47/025 , C22C47/00 , C22C47/20 , Y10T428/12444 , Y10T428/21 , Y10T428/211 , Y10T428/218
摘要： A composite material is formed of several assembled discs of matrix material, wherein each disc preferably has at least one groove therein, and at least one fiber (14) is inserted in each groove. A composite of matrix material and fibers (14) is present in an inner section (16), whereas exclusively the matrix material is present in an outer section (17). The inner section with the fibers (14) reaches to different radial extents toward the outer section (17), to achieve a strength-optimizing intermeshing of the inner section (16) with the outer section (17).
摘要翻译： 复合材料由几个组合的基质材料盘形成，其中每个盘优选地具有至少一个凹槽，并且至少一个纤维（14）插入每个凹槽中。 基体材料和纤维（14）的复合物存在于内部部分（16）中，而专门的基质材料存在于外部部分（17）中。 具有纤维（14）的内部部分朝着外部部分（17）到达不同的径向范围，以实现内部部分（16）与外部部分（17）的强度优化相互啮合。
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公开(公告)号：US20140202601A1
公开(公告)日：2014-07-24
申请号：US14237929
申请日：2012-08-09
申请人： Dietmar Helm , Falko Heutling , Ulrike Habel , Wilfried Smarsly
发明人： Dietmar Helm , Falko Heutling , Ulrike Habel , Wilfried Smarsly
CPC分类号： C22F1/183 , C22C14/00 , F01D5/28 , F05D2300/174
摘要： The present invention relates to a method for producing forged components of a TiAl alloy, in particular turbine blades, wherein the components are forged and undergo a two-stage heat treatment after the forging process, the first stage of the heat treatment comprising a recrystallization annealing process for 50 to 100 minutes at a temperature below the γ/α transition temperature, and the second stage of the heat treatment comprising a stabilization annealing process in the temperature range of from 800° C. to 950° C. for 5 to 7 hrs, and the cooling rate during the first heat treatment stage being greater than or equal to 3° C./sec, in the temperature range between 1300° C. to 900° C.
摘要翻译： 本发明涉及一种用于生产TiAl合金，特别是涡轮叶片的锻造部件的方法，其中锻件在锻造之后被锻造并进行两级热处理，第一阶段的热处理包括再结晶退火 在低于γ/α转变温度的温度下处理50至100分钟，第二阶段的热处理包括在800℃至950℃的温度范围内的稳定退火工艺5至7小时 在1300℃〜900℃的温度范围内，第一热处理阶段的冷却速度大于或等于3℃/秒。
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公开(公告)号：US20100226782A1
公开(公告)日：2010-09-09
申请号：US11472626
申请日：2006-06-21
IPC分类号： F01D5/14
CPC分类号： F01D5/28 , F01D5/284 , F01D5/286 , F05D2300/21 , F05D2300/611 , Y02T50/672 , Y02T50/673 , Y10T428/12458 , Y10T428/12549 , Y10T428/12576 , Y10T428/12806 , Y10T428/12847 , Y10T428/12875
摘要： A blade of a turbomachine such as a gas turbine includes a blade vane with a blade tip and a blade base. A blade tip armor cladding is applied on the blade tip. A coating covers at least the armor cladding and includes at least one multilayer coating system, and preferably plural such coating systems stacked repetitively on one another. Each coating system includes at least two different layers stacked successively on one another, with one layer of a metal material closer to the blade tip and one layer of a ceramic material farther from the blade tip.
摘要翻译： 诸如燃气轮机的涡轮机的叶片包括具有叶片尖端和叶片基座的叶片叶片。 叶片尖端装甲包层被施加在叶片尖端上。 涂层至少覆盖铠装包层，并且包括至少一个多层涂层系统，并且优选地多个相互重复堆叠的多个这样的涂层系统。 每个涂层系统包括至少两个彼此层叠的不同层，其中一层金属材料更靠近叶片尖端，一层陶瓷材料与叶片尖端更远。
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5.发明授权Process for producing a fiber-reinforced semifinished product in the form of metal strips, metal sheets or the like and apparatus for carrying out the process 失效用于制造金属条，金属片等形式的纤维增强半成品的方法和用于执行该方法的装置公开(公告)号：US07005598B2
公开(公告)日：2006-02-28
申请号：US10412053
申请日：2003-04-11
CPC分类号： C22C47/20 , B22F2998/00 , B22F2998/10 , B22F2999/00 , B23K15/0046 , B23K26/123 , B23K26/22 , B23K26/244 , B23K26/26 , B23K2101/16 , B23K2101/32 , B23K2101/34 , B23K2103/14 , C22C47/025 , C22C47/064 , C22C47/068 , C22C47/08 , C22C47/04 , B22F2202/11
摘要： A process for is producing a fiber-reinforced semifinished product in the form of metal strips, metal sheets etc., from at least one layer of fibers which includes a number of long to endless reinforcing fibers spaced apart from one another and arranged in parallel and a metal. A metal jacket applied to the reinforcing fiber by a PVD process (physical vapor deposition) may act for example as the metal. At least certain regions of the metal and the reinforcing fibers run through a welding process in which a bonding takes place by planar melting of the metal to form a matrix surrounding the reinforcing fibers.
摘要翻译： 一种用于从至少一层纤维制成金属条，金属片等形式的纤维增强半成品的方法，所述纤维层包括彼此间隔开并且平行设置的多个长到环形增强纤维， 金属。 通过PVD工艺（物理气相沉积）施加到增强纤维上的金属夹套可以例如作为金属起作用。 金属和增强纤维的至少某些区域穿过焊接工艺，其中通过金属的平面熔化进行接合以形成围绕增强纤维的基体。
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公开(公告)号：US08663814B2
公开(公告)日：2014-03-04
申请号：US12664372
申请日：2008-05-17
IPC分类号： B32B15/04
CPC分类号： C23C28/321 , C23C28/322 , C23C28/34 , C23C28/347 , C23C28/36 , C23C28/42 , F01D5/288 , Y10T428/12535 , Y10T428/12549 , Y10T428/31678
摘要： An anti-wear coating, in particular an anti-erosion coating, which is applied to a surface of a component that is stressed under fluid technology and is to be protected, in particular a gas turbine part, is disclosed. The anti-wear coating includes one or more multilayer systems applied in a repeating order to the surface to be coated, and the/each multilayer system includes at least one relatively soft metallic layer and at least one relatively hard ceramic layer. All the layers of the/each multilayer system are based on chromium, and a diffusion barrier layer is applied between the surface to be protected and the multilayer system(s).
摘要翻译： 公开了一种抗磨损涂层，特别是抗侵蚀涂层，其被应用于在流体技术下应力并被保护的部件的表面，特别是燃气轮机部件。 抗磨损涂层包括以重复顺序施加到待涂覆表面的一个或多个多层系统，并且/每个多层系统包括至少一个相对软的金属层和至少一个相对硬的陶瓷层。 每个多层系统的所有层都基于铬，并且在被保护表面和多层体系之间施加扩散阻挡层。
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公开(公告)号：US20120141822A1
公开(公告)日：2012-06-07
申请号：US12664372
申请日：2008-05-17
IPC分类号： B32B15/04
CPC分类号： C23C28/321 , C23C28/322 , C23C28/34 , C23C28/347 , C23C28/36 , C23C28/42 , F01D5/288 , Y10T428/12535 , Y10T428/12549 , Y10T428/31678
摘要： An anti-wear coating, in particular an anti-erosion coating, which is applied to a surface of a component that is stressed under fluid technology and is to be protected, in particular a gas turbine part, is disclosed. The anti-wear coating includes one or more multilayer systems applied in a repeating order to the surface to be coated, and the/each multilayer system includes at least one relatively soft metallic layer and at least one relatively hard ceramic layer. All the layers of the/each multilayer system are based on chromium, and a diffusion barrier layer is applied between the surface to be protected and the multilayer system(s).
摘要翻译： 公开了一种抗磨损涂层，特别是抗侵蚀涂层，其被应用于在流体技术下应力并被保护的部件的表面，特别是燃气轮机部件。 抗磨损涂层包括以重复顺序施加到待涂覆表面的一个或多个多层系统，并且/每个多层系统包括至少一个相对软的金属层和至少一个相对硬的陶瓷层。 每个多层系统的所有层都基于铬，并且在被保护表面和多层体系之间施加扩散阻挡层。
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公开(公告)号：US20100239429A1
公开(公告)日：2010-09-23
申请号：US12738829
申请日：2008-10-10
CPC分类号： C23C28/00 , C23C28/322 , C23C28/34 , C23C28/345 , C23C28/347 , Y10T428/24364
摘要： The English-language Abstract from the international application is to be retained and is therefore not duplicated in the specification.
摘要翻译： 国际申请中的英文摘要将被保留，因此在规范中不再重复。
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公开(公告)号：US20080317998A1
公开(公告)日：2008-12-25
申请号：US12163677
申请日：2008-06-27
CPC分类号： C23C14/226 , C23C28/322 , C23C28/34 , C23C28/3455 , C23C28/347 , C23C28/36 , C23C28/42 , F01D5/288 , F05D2230/313 , F05D2300/614 , Y10T428/12542 , Y10T428/12549 , Y10T428/12576 , Y10T428/12611 , Y10T428/12618 , Y10T428/12632 , Y10T428/12875 , Y10T428/24058 , Y10T428/24174 , Y10T428/24355 , Y10T428/24413
摘要： The present technology generally relates to a wear-resistant coating, especially for gas turbine components, comprising a horizontally segmented or multilayered structure, i.e. at least one relatively hard, ceramic layer and at least one relatively soft, metallic layer. The ceramic layer and the metallic layer are alternately arranged on top of each other in such a way that an external layer forming an external surface of the wear-resistant coating is embodied as a ceramic layer. According to the invention, at least the external, ceramic layer is segmented in a column-type manner in a vertical direction.
摘要翻译： 本技术通常涉及耐磨涂层，特别是对于燃气轮机部件，包括水平分段或多层结构，即至少一个相对硬的陶瓷层和至少一个相对柔软的金属层。 陶瓷层和金属层交替地布置在彼此的顶部上，使得形成耐磨涂层的外表面的外层被实施为陶瓷层。 根据本发明，至少外部陶瓷层在垂直方向上以列式方式分段。
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公开(公告)号：US09951411B2
公开(公告)日：2018-04-24
申请号：US12988045
申请日：2009-04-18
CPC分类号： C23C14/0641 , C23C14/027 , C23C28/044 , C23C28/048 , C23C28/42 , F01D5/284 , F01D5/288 , F05D2300/506 , Y10T428/24975 , Y10T428/24983
摘要： The invention relates to an erosion protection coating (11), in particular, for gas turbine components, having a horizontally segmented and/or multi-layered construction. i.e., having at least one relatively hard layer (12) and having at least one relatively soft layer (13), wherein the relatively hard layer or each relatively hard layer as well as the relatively soft layer or each relatively soft layer are disposed on top of one another in an alternating manner, in such a way that an outer-lying layer, which forms an outer surface of the erosion protection coating, is formed as a relatively hard layer (12). According to the invention, the relatively hard layer or each relatively hard layer (12) as well as the relatively soft layer or each relatively soft layer (13) are formed as a ceramic layer in each case.
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