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公开(公告)号：EP2206568A3
公开(公告)日：2017-05-03
申请号：EP09180589.5
申请日：2009-12-23
发明人： Calla, Eklavya , Anand, Krishnamurthy , Subramanian, Prazhayannur Ramanathan , Sondhi, Sanjay Kumar , Oruganti, Ramkumar
摘要： A method (200) of coating a substrate with cryo-milled, nano-grained particles includes forming a face-centered-cubic gamma matrix (202) comprising nickel, cobalt, chromium, tungsten and molybdenum, adding a dispersion strengthening material (204) to the gamma matrix to form a first mixture, cryo-milling (206) the first mixture to form a second mixture to form a nano-grained structure, and cold spraying (212) the second mixture onto a substrate to form a coating having a nano-grained structure.
摘要翻译： 用低温研磨的纳米粒子颗粒涂覆基底的方法（200）包括形成包含镍，钴，铬，钨和钼的面心立方γ基质（202），添加分散强化材料（204） 加入γ基质以形成第一混合物，将第一混合物低温研磨（206）以形成第二混合物以形成纳米颗粒结构，以及将第二混合物冷喷涂（212）到基材上以形成具有 纳米晶粒结构。
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2.发明公开
公开(公告)号：EP2778147A2
公开(公告)日：2014-09-17
申请号：EP14158502.6
申请日：2014-03-10
发明人： Schaeffer, Jon Conrad , Pabla, Surinder Singh , Dimascio, Paul Stephen , Anand, Krishnamurthy , Margolies, Joshua Lee , Parakala, Padmaja
CPC分类号： F01D25/08 , C23C28/042 , F01D5/288 , F01D25/005
摘要： A process (101) of forming a calcium-magnesium-aluminosilicate (CMAS) penetration resistant coating, and a CMAS penetration resistant coating are disclosed. The process includes providing a thermal barrier coating (110) having a dopant (112), and exposing the thermal barrier coating (110) to calcium-magnesium-aluminosilicate (114) and gas turbine operating conditions. The exposing forming a calcium-magnesium-aluminosilicate penetration resistant layer (201). The coating includes a thermal barrier coating composition (110) comprising a dopant (112) selected from the group consisting of rare earth elements, non-rare earth element solutes, and combinations thereof. Additional or alternatively, the coating includes a thermal barrier coating (110) and an impermeable barrier layer or a washable sacrificial layer positioned on an outer surface of the thermal barrier coating.
摘要翻译： 形成钙 - 硅铝酸镁（CMAS）耐穿透性涂层的方法（101），和一个渗透CMAS性涂层是游离缺失盘。 该方法包括提供具有一个掺杂剂（112）和暴露所述热障涂层（110），以钙 - 硅铝酸镁（114）和燃气涡轮机工况下的热障涂层（110）。 曝光形成钙 - 硅铝酸镁耐穿透性层（201）。 该涂层包括含有选自稀土类元素，非稀土元素的溶质，以及它们的组合中选择的掺杂剂（112）的热障涂层组合物（110）。 额外或替代地，涂层包括热障涂层（110）和不可渗透的阻挡层上或设置在所述热障涂层的外表面的牺牲层洗。
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公开(公告)号：EP2455513A2
公开(公告)日：2012-05-23
申请号：EP11189989.4
申请日：2011-11-21
发明人： Pabla, Surinder Singh. , Pareek, Vinod Kumar , Sanyal, Suchismita , Bhattacharya, Prajina , Anand, Krishnamurthy
CPC分类号： C23C24/08 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , Y02T50/67 , Y10T428/12549 , Y10T428/12611
摘要： A vanadium resistant coating system resistant to high temperature vanadium attack. The system comprises a high temperature superalloy substrate (10). A bond coat (20) overlies the superalloy substrate (10). The bond coat (20) may be applied in multiple layers. A ceramic coating (40) overlies the bond coat. The ceramic coating (40) further comprises a zirconium oxide stabilized by at least one cation selected from the group consisting of Yb 3+ , Lu 3+ , Sc 3+ and Ce 4+ , in the amounts of about 5-10 weight percent. An overcoat may overlie the ceramic coating. The overcoat may be a sacrificial layer of YSZ infiltrated with cations having an atomic radius larger than Y 3+ . Alternatively, the overcoat may comprise zirconium oxide stabilized by Ce 4+ .
摘要翻译： 耐高温钒攻击的耐钒涂层系统。 该系统包括高温超合金基底（10）。 粘合涂层（20）覆盖超合金基板（10）。 粘合涂层（20）可以以多层施加。 陶瓷涂层（40）覆盖在粘结涂层上。 所述陶瓷涂层（40）还包含以约5-10重量％的量由至少一种选自Yb 3+，Lu 3+，Sc 3+和Ce 4+的阳离子稳定的氧化锆。 外涂层可能覆盖陶瓷涂层。 外涂层可以是具有原子半径大于Y 3+的阳离子渗透的YSZ的牺牲层。 或者，外涂层可以包括由Ce 4+稳定的氧化锆。
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4.发明公开
公开(公告)号：EP2778147A3
公开(公告)日：2017-02-22
申请号：EP14158502.6
申请日：2014-03-10
发明人： Schaeffer, Jon Conrad , Pabla, Surinder Singh , Dimascio, Paul Stephen , Anand, Krishnamurthy , Margolies, Joshua Lee , Parakala, Padmaja
CPC分类号： F01D25/08 , C23C28/042 , F01D5/288 , F01D25/005
摘要： A process (101) of forming a calcium-magnesium-aluminosilicate (CMAS) penetration resistant coating, and a CMAS penetration resistant coating are disclosed. The process includes providing a thermal barrier coating (110) having a dopant (112), and exposing the thermal barrier coating (110) to calcium-magnesium-aluminosilicate (114) and gas turbine operating conditions. The exposing forming a calcium-magnesium-aluminosilicate penetration resistant layer (201). The coating includes a thermal barrier coating composition (110) comprising a dopant (112) selected from the group consisting of rare earth elements, non-rare earth element solutes, and combinations thereof. Additional or alternatively, the coating includes a thermal barrier coating (110) and an impermeable barrier layer or a washable sacrificial layer positioned on an outer surface of the thermal barrier coating.
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公开(公告)号：EP2206568A2
公开(公告)日：2010-07-14
申请号：EP09180589.5
申请日：2009-12-23
发明人： Calla, Eklavya , Anand, Krishnamurthy , Subramanian, Prazhayannur Ramanathan , Sondhi, Sanjay Kumar , Oruganti, Ramkumar
摘要： A method (200) of coating a substrate with cryo-milled, nano-grained particles includes forming a face-centered-cubic gamma matrix (202) comprising nickel, cobalt, chromium, tungsten and molybdenum, adding a dispersion strengthening material (204) to the gamma matrix to form a first mixture, cryo-milling (206) the first mixture to form a second mixture to form a nano-grained structure, and cold spraying (212) the second mixture onto a substrate to form a coating having a nano-grained structure.
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6.发明公开
公开(公告)号：EP2056004A1
公开(公告)日：2009-05-06
申请号：EP07119529.1
申请日：2007-10-29
发明人： Anand, Krishnamurthy , Salehi, Mohsen , Brisson, Bruce William , Ghasripoor, Farshad , Mathew, Paul , Gray, Dennis Michael , Srinivasan, Dheepa
IPC分类号： F16J15/34
CPC分类号： F16J15/3412 , C10M103/00 , C10M2201/0413 , C10N2230/06 , C10N2250/121 , C10N2280/00 , C23C28/00 , C23C28/021 , C23C28/022 , C23C28/027 , C23C28/028 , C23C28/042 , C23C28/044 , C23C28/046 , C23C28/048 , C23C28/42 , F16J15/3496
摘要： A mechanical seal includes a pair of opposing seal faces (10), wherein at least one of the pair of seal faces (10) includes a multilayer coating (14) disposed on a substrate (12), wherein the multilayer coating (14) has a periodic repetition of distinct layers, a plurality of layers of a composite wherein no two adjacent layers of the composite comprise an identical ratio of composite constituents, or both. A method of making the seal includes disposing a multilayer coating (14) on a substrate (12) to form at least one of a pair of opposing seal faces (10) of a mechanical seal.
摘要翻译： 机械密封件包括一对相对的密封面（10），其中所述一对密封面（10）中的至少一个包括设置在基底（12）上的多层涂层（14），其中所述多层涂层（14）具有 不同层的周期性重复，多层复合材料，其中复合材料的两个相邻层不包含相同比例的复合材料成分，或两者。 制造密封件的方法包括在基底（12）上设置多层涂层（14）以形成机械密封件的一对相对密封面（10）中的至少一个。
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7.发明公开Metallic alloy nanocomposite for high-temperature structural components and methods of making 审中-公开用于金属纳米复合物在合金高温部件以及制造方法的
公开(公告)号：EP1548134A3
公开(公告)日：2007-06-13
申请号：EP04257883.1
申请日：2004-12-16
发明人： Subramanian, Pazhayannur Ramanathan , Corderman, Reed Roeder , Marte, Judson Sloan , Angeliu, Thomas Martin , Huang, Shyh-Chin , Gray, Dennis Michael , Anand, Krishnamurthy , Oruganti, Ramkumar Kashyap , Srinivasan, Dheepa , Amancherla, Sundar
IPC分类号： C22C1/05
CPC分类号： C22C1/05 , B22F3/162 , B22F2009/041 , B22F2998/00 , B22F2998/10 , B22F2999/00 , B22F9/04 , B22F3/16 , B22F1/0018
摘要： A nanocomposite comprising a plurality of nanoparticles dispersed in a metallic alloy matrix, and a structural component formed from such a nanocomposite. The metallic matrix comprises at least one of a nickel-based alloy and an iron-based alloy. The nanocomposite contains a higher volume fraction of nanoparticle dispersoids than those presently available. The structural component include those used in hot gas path assemblies, such as steam turbines, gas turbines, and aircraft turbine. A method of making such nanocomposites is also disclosed.
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8.发明公开Erosion and wear resistant protective structures for turbine engine components 有权侵蚀与防腐工程SchutzstrukturefürBauteile eines Turbinentriebwerks
公开(公告)号：EP1577422A1
公开(公告)日：2005-09-21
申请号：EP05251407.2
申请日：2005-03-08
发明人： Gigliotti, Michael Francis Xavier, Jr. , Hardwicke, Canan Uslu , Jiang, Liang , Short, John William , Lipkin, Don Mark , Blank, Jonathan Paul , Anand, Krishnamurthy
CPC分类号： B23K20/08 , F01D5/28 , F01D5/288 , F05C2201/0463 , F05C2201/0466 , F05D2220/31 , F05D2230/311 , F05D2230/312 , F05D2230/313 , F05D2230/80 , F05D2230/90 , F05D2300/501 , F05D2300/505 , F05D2300/611 , Y10S420/902 , Y10T428/12493 , Y10T428/12611 , Y10T428/12806 , Y10T428/12944
摘要： An erosion resistant protective structure for a turbine engine component comprises a shape memory alloy. The shape memory alloy includes nickel-titanium based alloys, indium-titanium based alloys, nickel-aluminum based alloys, nickel-gallium based alloys, copper based alloys, gold-cadmium based alloys, iron -platinum based alloys, iron-palladium based alloys, silver-cadmium based alloys, indium-cadmium based alloys, manganese-copper based alloys, ruthenium-niobium based alloys, ruthenium-tantalum based alloys, titanium based alloys, iron-based alloys, or combinations comprising at least one of the foregoing alloys. Also, disclosed herein are methods for forming the shape memory alloy onto turbine component.
摘要翻译： 用于涡轮发动机部件的耐侵蚀保护结构包括形状记忆合金。 形状记忆合金包括镍 - 钛基合金，铟 - 钛基合金，镍 - 铝基合金，镍 - 镓基合金，铜基合金，金 - 镉基合金，铁 - 铂基合金，铁 - 钯基合金 银镉基合金，铟镉基合金，锰 - 铜基合金，钌 - 铌基合金，钌 - 钽基合金，钛基合金，铁基合金或包含至少一种上述合金的组合 。 此外，本文公开的是将形状记忆合金形成到涡轮部件上的方法。
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9.发明公开Architectures for high temperature TBCs with ultra low thermal conductivity and abradability and method of making 审中-公开用于高温热障涂层具有超低导热性和易碎性体系结构以及用于制备方法
公开(公告)号：EP2799588A3
公开(公告)日：2015-04-29
申请号：EP14163745.4
申请日：2014-04-07
发明人： Parakala, Padmaja , Pabla, Surinder S. , Margolies, Joshua Lee , Ruud, James Anthony , Anand, Krishnamurthy , Schaeffer, Jon Conrad
IPC分类号： C23C4/12 , C23C28/00 , C23C28/04 , C04B35/486 , F01D5/28
CPC分类号： F01D25/005 , C04B35/486 , C04B35/50 , C04B2235/3224 , C04B2235/3225 , C04B2235/3227 , C04B2235/3244 , C04B2235/96 , C04B2235/9607 , C23C4/02 , C23C4/11 , C23C4/134 , C23C28/3215 , C23C28/3455 , F01D5/288 , Y10T428/24471 , Y10T428/24942 , Y10T428/31678
摘要： A method for fabricating thermal barrier coatings. The thermal barrier coatings are produced with a fine grain size by reverse co-precipitation of fine powders. The powders are then sprayed by a solution plasma spray that partially melts the fine powders while producing a fine grain size with dense vertical cracking. The coatings comprise at least one of 45% -65% Yb 2 O 3 the balance Zr, Yb/Y/Hf/Ta the balance Zr and 2.3-7.8% La, 1.4-5.1% Y and the balance Zr and are characterized by a thermal conductivity that is about 25-50% lower than that of thermal barrier coatings comprising YSZ. The thermal barrier coatings also are characterized by at least one of excellent erosion resistance, fracture toughness and abrasion resistance.
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10.发明公开Multilayered coatings with diamond like carbon 审中-公开Mehrschichtige Beschichtungen mitdiamantähnlichemKohlenstoff
公开(公告)号：EP2821525A1
公开(公告)日：2015-01-07
申请号：EP14173879.9
申请日：2014-06-25
CPC分类号： C23C28/42 , C23C28/046 , F01D5/288 , F05D2250/62 , F05D2300/224 , F05D2300/506 , Y10T428/24355
摘要： Multilayered coatings 10 include an adhesion base layer 12 that can adhere to a metal substrate 20, and a top surface layer 16 that has a surface roughness of less than or equal to about Ra 0.0254 µm, wherein at least one of the layers 12, 16 comprises a diamond-like carbon.
摘要翻译： 多层涂层10包括可粘附到金属基底20上的粘合基底层12和具有小于或等于约Ra0.0254μm的表面粗糙度的顶表面层16，其中层12,16中的至少一个 包括类金刚石碳。
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