-
公开(公告)号：US10227678B2
公开(公告)日：2019-03-12
申请号：US13156638
申请日：2011-06-09
申请人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, Jr. , Kathleen Blanche Morey , Pazhayannur Subramanian
发明人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, Jr. , Kathleen Blanche Morey , Pazhayannur Subramanian
摘要： A high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy is disclosed. The alloy includes, in weight percent: about 3.5 to about 4.9% of Al, about 12.2 to about 16.0% of W, about 24.5 to about 32.0% Ni, about 6.5% to about 10.0% Cr, about 5.9% to about 11.0% Ta, and the balance Co and incidental impurities. A method of making an article having high-temperature strength, cyclic oxidation resistance and corrosion resistance is disclosed. The method includes forming a high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy as described herein; forming an article from the alloy; solution-treating the alloy by a solution heat treatment; and aging the alloy by providing at least one aging heat treatment at an aging temperature that is less than the gamma-prime solvus temperature, wherein the alloy is configured to form a continuous, protective, adherent oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment.
-
2.发明授权Method for manufacturing a hot gas path component and hot gas path turbine component 有权热气路径部件和热气路径涡轮部件的制造方法公开(公告)号：US08870523B2
公开(公告)日：2014-10-28
申请号：US13042167
申请日：2011-03-07
申请人： Srikanth Chandrudu Kottilingam , David Vincent Bucci , Benjamin Paul Lacy , Kathleen Blanche Morey , Brian Lee Tollison , Patrick Thomas Walsh
发明人： Srikanth Chandrudu Kottilingam , David Vincent Bucci , Benjamin Paul Lacy , Kathleen Blanche Morey , Brian Lee Tollison , Patrick Thomas Walsh
CPC分类号： F02C7/00 , B23K31/02 , F01D9/04 , F05D2230/237 , F05D2240/11 , F05D2260/20 , Y10T29/49323
摘要： According to one aspect of the invention, a method for manufacturing a hot gas path component of a turbine is provided, the method including forming cooling channels in a surface of a member. The method also includes disposing a layer on the surface of the member to enclose the cooling channels, the layer being disposed on a portion of the member to be cooled and bonding the layer to the surface, wherein bonding comprises heating the member and the layer.
摘要翻译： 根据本发明的一个方面，提供了一种用于制造涡轮机的热气体通道部件的方法，所述方法包括在部件的表面中形成冷却通道。 该方法还包括在构件的表面上设置一层以封闭冷却通道，该层设置在要冷却的构件的一部分上，并将该层粘合到该表面上，其中，接合包括加热该构件和该层。
-
公开(公告)号：US20120312434A1
公开(公告)日：2012-12-13
申请号：US13156638
申请日：2011-06-09
申请人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, JR. , Kathleen Blanche Morey , Pazhayannur Subramanian
发明人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, JR. , Kathleen Blanche Morey , Pazhayannur Subramanian
CPC分类号： C22C19/07 , C22C19/057 , C22F1/10
摘要： A high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy is disclosed. The alloy includes, in weight percent: about 3.5 to about 4.9% of Al, about 12.2 to about 16.0% of W, about 24.5 to about 32.0% Ni, about 6.5% to about 10.0% Cr, about 5.9% to about 11.0% Ta, and the balance Co and incidental impurities. A method of making an article having high-temperature strength, cyclic oxidation resistance and corrosion resistance is disclosed. The method includes forming a high-temperature, high-strength, oxidation-resistant cobalt-nickel base alloy as described herein; forming an article from the alloy; solution-treating the alloy by a solution heat treatment; and aging the alloy by providing at least one aging heat treatment at an aging temperature that is less than the gamma-prime solvus temperature, wherein the alloy is configured to form a continuous, protective, adherent oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment.
摘要翻译： 公开了高温，高强度，耐氧化的钴镍基合金。 该合金包括重量百分比：约3.5至约4.9％的Al，约12.2至约16.0％的W，约24.5至约32.0％的Ni，约6.5％至约10.0％的Cr，约5.9％至约11.0％ Ta，余量Co和杂质。 公开了制造具有高温强度，耐环氧化和耐腐蚀性的制品的方法。 该方法包括形成如本文所述的高温，高强度，耐氧化的钴镍基合金; 从合金制成制品; 通过固溶热处理对合金进行溶解处理; 并且通过在低于γ'溶质温度的老化温度下提供至少一种时效热处理来老化合金，其中该合金构造成在暴露于合金表面时在合金表面上形成连续的，保护性的粘附氧化物层 高温氧化环境。
-
4.发明授权Alumina-forming cobalt-nickel base alloy and method of making an article therefrom 有权氧化铝形成钴镍基合金及其制品的制造方法公开(公告)号：US09034247B2
公开(公告)日：2015-05-19
申请号：US13156614
申请日：2011-06-09
申请人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, Jr. , Kathleen Blanche Morey , Jon Conrad Schaeffer , Pazhayannur Subramanian
发明人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, Jr. , Kathleen Blanche Morey , Jon Conrad Schaeffer , Pazhayannur Subramanian
CPC分类号： C22C19/07 , C22C19/056 , C22C19/057 , C22F1/10 , C23C8/10
摘要： A cobalt-nickel base alloy is disclosed. The alloy includes, in weight percent: greater than about 4 % of Al, about 10 to about 20 % of W, about 10 to about 40 % Ni, about 5 to 20 % Cr and the balance Co and incidental impurities. The alloy has a microstructure that is substantially free of a CoAl phase having a B2 crystal structure and configured to form a continuous, adherent aluminum oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment. A method of making an article of the alloy includes: selecting the alloy; forming an article from the alloy; solution-treating the alloy; and aging the alloy to form an alloy microstructure that is substantially free of a CoAl phase having a B2 crystal structure, wherein the alloy is configured to form a continuous, adherent aluminum oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment.
摘要翻译： 公开了一种钴 - 镍基合金。 该合金包括以重量％计：大于约4％的Al，约10至约20％的W，约10至约40％的Ni，约5至20％的Cr以及余量为Co和杂质。 该合金具有基本上不含具有B2晶体结构的CoAl相的微结构，并且构造成在暴露于高温氧化环境时在合金表面上形成连续的附着氧化铝层。 制造合金制品的方法包括：选择合金; 从合金制成制品; 溶液处理合金; 并且老化该合金以形成基本上不含具有B2晶体结构的CoAl相的合金微结构，其中该合金构造成在暴露于高温氧化环境时在合金表面上形成连续的粘附氧化铝层 。
-
公开(公告)号：US08857055B2
公开(公告)日：2014-10-14
申请号：US12697005
申请日：2010-01-29
申请人： Bin Wei , Jon Conrad Schaeffer , Ronald Scott Bunker , Wenwu Zhang , Kathleen Blanche Morey , Jane Marie Lipkin , Benjamin Paul Lacy , Wilbur Douglas Scheidt
发明人： Bin Wei , Jon Conrad Schaeffer , Ronald Scott Bunker , Wenwu Zhang , Kathleen Blanche Morey , Jane Marie Lipkin , Benjamin Paul Lacy , Wilbur Douglas Scheidt
IPC分类号： B21D53/78 , B21K3/04 , B23P15/02 , F02C7/18 , F01D25/12 , B23K26/38 , B23K26/06 , B23K26/30 , B23K26/08
CPC分类号： F02C7/18 , B23K26/0624 , B23K26/082 , B23K26/384 , B23K26/389 , B23K26/60 , B23K26/702 , B23K2101/001 , B23K2101/34 , F01D25/12 , F05D2230/00 , F05D2230/13 , Y10T29/49316 , Y10T29/4932 , Y10T29/49336 , Y10T29/49339 , Y10T29/49341 , Y10T29/49348 , Y10T29/49799
摘要： A process is provided for forming shaped air holes, such as for use in turbine blades. Aspects of the disclosure relate to forming shaped portions of air holes using a short pulse laser, forming a metered hole corresponding to each shaped portion, and separately finishing the shaped portion using a short-pulse laser. In other embodiments, the order of these operations may be varied, such as to form the shaped portions and to finish the shaped portions using the short-pulse laser prior to forming the corresponding metered holes.
摘要翻译： 提供了一种用于形成成形气孔的方法，例如用于涡轮叶片。 本公开的方面涉及使用短脉冲激光器形成空气孔的成形部分，形成与每个成形部分相对应的计量孔，并且使用短脉冲激光单独精加工成形部分。 在其他实施例中，可以改变这些操作的顺序，诸如形成成形部分，并且在形成相应的计量孔之前使用短脉冲激光来完成成形部分。
-
6.发明申请METHOD FOR MANUFACTURING A HOT GAS PATH COMPONENT AND HOT GAS PATH TURBINE COMPONENT 有权燃气路径成分和热气路径涡轮组件的制造方法公开(公告)号：US20130139510A1
公开(公告)日：2013-06-06
申请号：US13042167
申请日：2011-03-07
申请人： Srikanth Chandrudu Kottilingam , David Vincent Bucci , Benjamin Paul Lacy , Kathleen Blanche Morey , Brian Lee Tollison , Patrick Thomas Walsh
发明人： Srikanth Chandrudu Kottilingam , David Vincent Bucci , Benjamin Paul Lacy , Kathleen Blanche Morey , Brian Lee Tollison , Patrick Thomas Walsh
CPC分类号： F02C7/00 , B23K31/02 , F01D9/04 , F05D2230/237 , F05D2240/11 , F05D2260/20 , Y10T29/49323
摘要： According to one aspect of the invention, a method for manufacturing a hot gas path component of a turbine is provided, the method including forming cooling channels in a surface of a member. The method also includes disposing a layer on the surface of the member to enclose the cooling channels, the layer being disposed on a portion of the member to be cooled and bonding the layer to the surface, wherein bonding comprises heating the member and the layer.
摘要翻译： 根据本发明的一个方面，提供了一种用于制造涡轮机的热气体通道部件的方法，所述方法包括在部件的表面中形成冷却通道。 该方法还包括在构件的表面上设置一层以封闭冷却通道，该层设置在要冷却的构件的一部分上，并将该层粘合到该表面上，其中，接合包括加热该构件和该层。
-
7.发明申请Alumina-Forming Cobalt-Nickel Base Alloy and Method of Making an Article Therefrom 有权氧化铝形成钴 - 镍基合金及其制造方法公开(公告)号：US20120312426A1
公开(公告)日：2012-12-13
申请号：US13156614
申请日：2011-06-09
申请人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, JR. , Kathleen Blanche Morey , Jon Conrad Schaeffer , Pazhayannur Subramanian
发明人： Akane Suzuki , Andrew John Elliott , Michael Francis Xavier Gigliotti, JR. , Kathleen Blanche Morey , Jon Conrad Schaeffer , Pazhayannur Subramanian
CPC分类号： C22C19/07 , C22C19/056 , C22C19/057 , C22F1/10 , C23C8/10
摘要： A cobalt-nickel base alloy is disclosed. The alloy includes, in weight percent: greater than about 4% of Al, about 10 to about 20% of W, about 10 to about 40% Ni, about 5 to 20% Cr and the balance Co and incidental impurities. The alloy has a microstructure that is substantially free of a CoAl phase having a B2 crystal structure and configured to form a continuous, adherent aluminum oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment. A method of making an article of the alloy includes: selecting the alloy; forming an article from the alloy; solution-treating the alloy; and aging the alloy to form an alloy microstructure that is substantially free of a CoAl phase having a B2 crystal structure, wherein the alloy is configured to form a continuous, adherent aluminum oxide layer on an alloy surface upon exposure to a high-temperature oxidizing environment.
摘要翻译： 公开了一种钴 - 镍基合金。 该合金包括以重量％计：大于约4％的Al，约10至约20％的W，约10至约40％的Ni，约5至20％的Cr以及余量为Co和杂质。 该合金具有基本上不含具有B2晶体结构的CoAl相的微结构，并且构造成在暴露于高温氧化环境时在合金表面上形成连续的附着氧化铝层。 制造合金制品的方法包括：选择合金; 从合金制成制品; 溶液处理合金; 并且老化该合金以形成基本上不含具有B2晶体结构的CoAl相的合金微结构，其中该合金构造成在暴露于高温氧化环境时在合金表面上形成连续的粘附氧化铝层 。
-
8.发明申请TURBULATED ARRANGEMENT OF THERMOELECTRIC ELEMENTS FOR UTILIZING WASTE HEAT GENERATED FROM TURBINE ENGINE 失效用于利用涡轮发动机产生的废热的热电元件的涡轮机布置公开(公告)号：US20120031067A1
公开(公告)日：2012-02-09
申请号：US12849517
申请日：2010-08-03
CPC分类号： F02C6/18 , F01D25/30 , F02C3/00 , F05D2220/60 , F05D2240/127 , H01L35/30
摘要： Disclosed is a turbulated arrangement of thermoelectric elements for utilizing waste heat generated from a turbine engine. The turbulated arrangement of thermoelectric elements is located within the turbine casing at a heat exhaust end of the turbine engine. The turbulated arrangement of thermoelectric elements convert heat exhaust generated from the turbine engine into electrical energy. In one embodiment, the electrical energy generated from the turbulated arrangement of thermoelectric elements can be used to power electrical components located about the turbine engine.
摘要翻译： 公开了一种用于利用从涡轮发动机产生的废热的热电元件的混合布置。 热电元件的混浊布置位于涡轮机外壳内，在涡轮发动机的排热端。 热电元件的混合布置将从涡轮发动机产生的热排放转换为电能。 在一个实施例中，从热电元件的混沌布置产生的电能可用于为位于涡轮发动机周围的电气部件供电。
-
公开(公告)号：US20110185572A1
公开(公告)日：2011-08-04
申请号：US12697005
申请日：2010-01-29
申请人： Bin Wei , Jon Conrad Schaeffer , Ronald Scott Bunker , Wenwu Zhang , Kathleen Blanche Morey , Jane Marie Lipkin , Benjamin Paul Lacy , Wilbur Douglas Scheidt
发明人： Bin Wei , Jon Conrad Schaeffer , Ronald Scott Bunker , Wenwu Zhang , Kathleen Blanche Morey , Jane Marie Lipkin , Benjamin Paul Lacy , Wilbur Douglas Scheidt
CPC分类号： F02C7/18 , B23K26/0624 , B23K26/082 , B23K26/384 , B23K26/389 , B23K26/60 , B23K26/702 , B23K2101/001 , B23K2101/34 , F01D25/12 , F05D2230/00 , F05D2230/13 , Y10T29/49316 , Y10T29/4932 , Y10T29/49336 , Y10T29/49339 , Y10T29/49341 , Y10T29/49348 , Y10T29/49799
摘要： A process and system are provided for forming shaped air holes, such as for use in turbine blades. Aspects of the disclosure relate to forming shaped portions of air holes using a short pulse laser, forming a metered hole corresponding to each shaped portion, and separately finishing the shaped portion using a short-pulse laser. In other embodiments, the order of these operations may be varied, such as to form the shaped portions and to finish the shaped portions using the short-pulse laser prior to forming the corresponding metered holes.
摘要翻译： 提供了用于形成诸如用于涡轮叶片的成形气孔的过程和系统。 本公开的方面涉及使用短脉冲激光器形成空气孔的成形部分，形成与每个成形部分相对应的计量孔，并且使用短脉冲激光单独精加工成形部分。 在其他实施例中，可以改变这些操作的顺序，诸如形成成形部分，并且在形成相应的计量孔之前使用短脉冲激光来完成成形部分。
-
10.发明授权Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine 失效用于利用涡轮发动机产生的废热的热电元件的混合布置公开(公告)号：US08578696B2
公开(公告)日：2013-11-12
申请号：US12849517
申请日：2010-08-03
CPC分类号： F02C6/18 , F01D25/30 , F02C3/00 , F05D2220/60 , F05D2240/127 , H01L35/30
摘要： Disclosed is a turbulated arrangement of thermoelectric elements for utilizing waste heat generated from a turbine engine. The turbulated arrangement of thermoelectric elements is located within the turbine casing at a heat exhaust end of the turbine engine. The turbulated arrangement of thermoelectric elements convert heat exhaust generated from the turbine engine into electrical energy. In one embodiment, the electrical energy generated from the turbulated arrangement of thermoelectric elements can be used to power electrical components located about the turbine engine.
摘要翻译： 公开了一种用于利用从涡轮发动机产生的废热的热电元件的混合布置。 热电元件的混浊布置位于涡轮机外壳内，在涡轮发动机的排热端。 热电元件的混合布置将从涡轮发动机产生的热排放转换为电能。 在一个实施例中，从热电元件的混沌布置产生的电能可用于为位于涡轮发动机周围的电气部件供电。
-
-
-
-
-
-
-
-
-
搜索结果
11 条记录 (耗时 0.027 秒)
