-
公开(公告)号：US12270091B2
公开(公告)日：2025-04-08
申请号：US17727093
申请日：2022-04-22
Applicant: General Electric Company
Inventor： Sathisha Chikkabikkodu Hanum , Mohandas Nayak , Surinder Singh Pabla , Biju Dasan
Abstract: A composition, a machine component coated with the same, and a method of coating the machine component are provided. The composition includes a CoNiCrAlY alloy, where three or more elements of the CoNiCrAlY alloy are present in equimolar amounts, one of the three or more elements of the CoNiCrAlY alloy being aluminum (Al), and where a molar fraction of Al is between about 0.20 and about 0.25. The composition further includes a transition metal boride including at least one of: cobalt boride (Co2B), titanium boride (TiB2), zirconium boride (ZrB2), tantalum boride (TaB2), niobium boride (NiB2), or molybdenum boride (Mo2B), and a refractory alloy.
-
公开(公告)号：US12109618B2
公开(公告)日：2024-10-08
申请号：US17197266
申请日：2021-03-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ibrahim Ucok , Yan Cui , Srikanth Chandrudu Kottilingam , Surinder Singh Pabla
IPC: B32B15/01 , B22F3/15 , B22F3/24 , B22F5/00 , B22F5/04 , B22F10/14 , B22F10/28 , B22F10/62 , B22F10/64 , B23K15/00 , B23K26/00 , B23K26/342 , B23K26/70 , B32B3/30 , B33Y10/00 , B33Y40/20 , B33Y70/00 , B33Y80/00 , C22C19/05 , C22C19/07 , C22C30/02 , C22C38/00 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/08 , C22C38/10 , C22C38/42 , C22C38/44 , C22C38/48 , C22C38/50 , C22C38/52 , C23C4/08 , C23C4/134 , C23C14/16 , C23C14/28 , C23C16/06 , C23C16/44 , C23C18/16 , C23C18/32 , F01D5/28 , F01D25/00 , F01D25/24 , B23K101/00
CPC classification number: B22F3/15 , B22F3/24 , B22F5/009 , B22F5/04 , B22F10/14 , B22F10/28 , B22F10/62 , B22F10/64 , B23K15/0086 , B23K15/0093 , B23K26/0006 , B23K26/342 , B23K26/70 , B32B3/30 , B32B15/01 , B33Y10/00 , B33Y40/20 , B33Y70/00 , B33Y80/00 , C22C19/055 , C22C19/056 , C22C19/057 , C22C19/07 , C22C30/02 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/08 , C22C38/105 , C22C38/42 , C22C38/44 , C22C38/48 , C22C38/50 , C22C38/52 , C23C4/08 , C23C4/134 , C23C14/16 , C23C14/28 , C23C16/06 , C23C16/44 , C23C18/1637 , C23C18/32 , F01D5/28 , F01D25/005 , F01D25/24 , B22F2003/242 , B22F2301/15 , B22F2301/35 , B22F2998/10 , B23K2101/001 , F05D2300/17 , Y02P10/25 , B22F2998/10 , B22F10/28 , B22F10/62 , B22F2003/242 , B22F10/64 , B22F3/15
Abstract: A process includes forming a printed article having an external surface and at least one microfeature with an internal surface by additive manufacture, coating the external surface and the internal surface of the printed article with a metallic microlayer to form a coated article, and densifying the coated article to form a component. After formation, the printed article has a porosity such that the printed article is not at full density. A densified component includes a printed article having an external surface and at least one microfeature with an internal surface and a metallic microlayer coating the external surface and the internal surface of the printed article. The printed article is formed by additive manufacture.
-
公开(公告)号：US20200263558A1
公开(公告)日：2020-08-20
申请号：US16280261
申请日：2019-02-20
Applicant: General Electric Company
IPC: F01D11/12
Abstract: Various embodiments include honeycomb structures including an abradable material, and a method of applying such honeycomb structures to steel components of a gas turbine engine in order to reduce rub damage. Particular embodiments include a honeycomb structure having a plurality of cells, each cell of the plurality of cells including a cell wall surrounding a void, and an abradable material within the void of each cell of the plurality of cells, the abradable material including a metallic alloy and hollow particles.
-
公开(公告)号：US20200263307A1
公开(公告)日：2020-08-20
申请号：US16280283
申请日：2019-02-20
Applicant: General Electric Company
Inventor： Krishnamurthy Anand , Eklavya Calla , Biju Dasan , Surinder Singh Pabla , Priyanka Saxena
Abstract: Various embodiments include a dense abradable coating, a method of reducing rub damage to a turbine engine part by applying the dense abradable coating thereto, and a turbine engine part having the abradable coating thereon. Particular embodiments include a dense abradable coating including a pore-free metallic composite, a high-aluminum containing brittle alloy, and a plurality of hollow abradable particles.
-
公开(公告)号：US09597746B2
公开(公告)日：2017-03-21
申请号：US14322028
申请日：2014-07-02
Applicant: General Electric Company
Inventor： Joshua Lee Margolies , Surinder Singh Pabla
CPC classification number: B23K9/24 , B05B7/224 , B23K9/04 , C23C4/131 , Y10T428/2927
Abstract: A composite wire for use with a wire arc spray system and related methods. The composite wire can include: a low melting point material at a core region thereof and a cladding including a metal surrounding the core region, the low metal point material having a melting point less than that of the metal, wherein the low melting point material includes a polymer in the form of a powder having particles having a size of from approximately 1 nanometer to approximately 100 nanometers.
-
Patent Agency Ranking
公开(公告)号：US09567554B2
公开(公告)日：2017-02-14
申请号：US14152335
申请日：2014-01-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sanji Ekanayake , Surinder Singh Pabla , Murali Krishna Kalaga , Alston Ilford Scipio , Ishmael Dean El
IPC: B08B7/00 , C11D11/00 , F01D25/00 , C11D3/37 , B08B3/04 , B08B3/10 , C11D7/34 , C11D7/50 , B08B3/02 , B08B17/02
CPC classification number: C11D11/0041 , B08B3/02 , B08B3/04 , B08B3/102 , B08B17/025 , C11D3/044 , C11D3/18 , C11D3/3427 , C11D3/3749 , C11D7/34 , C11D7/5027 , F01D25/002
Abstract: A cleaning method and a cleaning fluid are provided. The cleaning method includes accessing a plurality of turbine components attached to a turbine assembly, the turbine assembly being a portion of a turbomachine, positioning at least one cleaning vessel over at least one of the turbine components, forming a liquid seal with a sealing bladder, providing a cleaning fluid to the cleaning vessel, and draining the cleaning fluid from the cleaning vessel. The cleaning fluid includes a carrier fluid and a solvent additive for removing fouling material from the turbine component. An alternative cleaning method is also provided.
Abstract translation: 提供清洁方法和清洗液。 清洁方法包括进入附接到涡轮机组件的多个涡轮机部件，涡轮组件是涡轮机的一部分，将至少一个清洁容器定位在至少一个涡轮部件上，与密封囊形成液体密封， 向清洁容器提供清洁流体，并且从清洁容器排出清洁流体。 清洁流体包括载体流体和用于从涡轮机部件去除结垢材料的溶剂添加剂。 还提供了替代的清洁方法。
-
公开(公告)号：US09347126B2
公开(公告)日：2016-05-24
申请号：US13801478
申请日：2013-03-13
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Surinder Singh Pabla , Joshua Lee Margolies , Eklavya Calla , Padmaja Parakala
Abstract: A process of fabricating a thermal barrier coating is disclosed. The process includes cold spraying a substrate with a feedstock to form a thermal barrier coating and concurrently oxidizing one or more of the substrate, the feedstock, and the thermal barrier coating. The cold spraying is in a region having an oxygen concentration of at least 10%. In another embodiment, the process includes heating a feedstock with a laser and cold spraying a substrate with the feedstock to form a thermal barrier coating. At least a portion of the feedstock is retained in the thermal barrier coating. In another embodiment, the process of fabricating a thermal barrier coating includes heating a substrate with a laser and cold spraying the substrate with a feedstock to form a thermal barrier coating.
Abstract translation: 公开了一种制造隔热涂层的工艺。 该方法包括用原料冷却基材以形成热障涂层并同时氧化基材，原料和热障涂层中的一种或多种。 冷喷雾处于氧浓度为10％以上的区域。 在另一个实施方案中，该方法包括用激光加热原料并用原料冷却喷涂基材以形成热障涂层。 原料的至少一部分保留在热障涂层中。 在另一个实施方案中，制造热障涂层的方法包括用激光加热衬底并用原料冷喷涂衬底以形成热障涂层。
-
公开(公告)号：US20160076457A1
公开(公告)日：2016-03-17
申请号：US14484965
申请日：2014-09-12
Applicant: General Electric Company
Inventor： Sanji Ekanayake , Murali Krishna Kalaga , Surinder Singh Pabla , Alston Ilford Scipio
CPC classification number: F02C7/30 , B05B12/12 , B08B3/02 , C11D3/162 , C11D11/0041 , C23C2222/20 , F01D5/288 , F01D25/002 , F04D29/705 , F05D2220/32 , F05D2260/95 , F05D2270/11
Abstract: Disclosed herein are methods and systems for treating a surface, such as a gas turbine surface, with a filming treatment. The system includes a storage tank configured to contain a filming agent, a plurality of nozzles, and supply conduit coupled to the storage tank on a first end and the plurality of nozzles on a second end, wherein the system is configured to deliver the filming agent from the storage tank and to discharge the filming agent through the plurality of nozzles and the filming agent includes siloxane, fluorosilane, mercapto silane, amino silane, tetraethyl orthosilicate, succinic anhydride silane, or a combination including at least one of the foregoing.
Abstract translation: 本文公开了用于通过成膜处理来处理诸如燃气轮机表面的表面的方法和系统。 该系统包括一个储存箱，其被配置为容纳一个成膜剂，多个喷嘴，以及在第一端上连接到储罐的供应导管，以及在第二端上的多个喷嘴，其中该系统构造成输送成膜剂 并且通过多个喷嘴排出成膜剂，并且成膜剂包括硅氧烷，氟硅烷，巯基硅烷，氨基硅烷，原硅酸四乙酯，琥珀酸酐硅烷或包含至少一种前述物质的组合。
-
公开(公告)号：US20160010471A1
公开(公告)日：2016-01-14
申请号：US13793189
申请日：2013-03-11
Applicant: General Electric Company
Inventor： Surinder Singh Pabla , Kirshnamurthy Anand , Murali Krishna Kalaga , Joshua Lee Margolies , Eklavya Calla , Padmaja Parakala
CPC classification number: F01D5/288 , C04B35/48 , C04B35/50 , C04B35/62805 , C04B35/62884 , C04B35/62886 , C04B2235/3224 , C04B2235/3227 , C04B2235/3246 , C04B2235/5436 , C04B2235/72 , C04B2235/9607 , C23C4/11 , F01D5/225 , F01D9/041 , F02C7/25 , F05D2220/32 , F05D2230/90 , F05D2240/35 , F05D2260/231 , F05D2300/2118
Abstract: A coating system and a method of forming the coating system capable of enabling components to survive in high temperatures environments, such as the hostile thermal environment of a gas turbine. The coating system is formed of a ceramic powder having powder particles each having an inner core formed of a first material and an outer region formed of a second material on the surface of the inner core. The inner core has a lower thermal conductivity than the outer region and the outer region has improved erosion resistance relative to the inner core.
Abstract translation: 涂覆系统和形成涂层系统的方法，其能够使组分在诸如燃气轮机的恶劣热环境的高温环境中存活。 该涂层系统由具有由第一材料形成的内芯和在内芯表面上由第二材料形成的外部区域的粉末颗粒形成的陶瓷粉末形成。 内芯具有比外部区域更低的热导率，并且外部区域相对于内部芯部具有改善的耐腐蚀性。
-
公开(公告)号：US20150147185A1
公开(公告)日：2015-05-28
申请号：US14090871
申请日：2013-11-26
Applicant: General Electric Company
IPC: F01D5/20
CPC classification number: F01D5/20 , B22F3/1055 , B22F5/04 , B23K26/0622 , B23K26/342 , B23K35/327 , B23K2101/001 , B23K2101/34 , B23K2103/08 , B23K2103/16 , B23K2103/26 , B29C64/153 , C22C32/0047 , C22C32/0057 , C23C28/30 , F01D5/28 , F01D5/288 , F01D11/12 , F05D2300/175 , F05D2300/226 , F05D2300/2282 , F05D2300/506 , Y02P10/295 , Y10T29/49337
Abstract: Turbine buckets include a pressure side, a suction side opposite the pressure side, and a bucket squealer tip attached to the pressure side and the suction side. The bucket squealer tip includes a plurality of high hot hardness shroud-cutting deposits deposited on its exterior surface that have a hardness of at least about 1100 kg mm−2 and a melting temperature of at least about 1500° C.
Abstract translation: 涡轮铲斗包括压力侧，与压力侧相对的吸入侧，以及附接到压力侧和吸力侧的铲斗尖端尖端。 铲斗尖尖包括沉积在其外表面上的多个高热硬度护罩切割沉积物，其具有至少约1100kg / mm 2的硬度和至少约1500℃的熔化温度。
-
-
-
-
-
-
-
-
-
Search Results
48
records
(took 0.018 seconds)
