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41.发明授权公开(公告)号：US10265792B2
公开(公告)日：2019-04-23
申请号：US15806565
申请日：2017-11-08
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Yan Cui , Srikanth Chandrudu Kottilingam , Brian Lee Tollison , Timothy Neal Pletcher , Richard Ryan Pilson
IPC: B23K1/00 , B22F7/06 , B22F5/04 , B23F5/00 , B23K9/04 , B23K15/00 , B23K35/36 , B23K35/02 , B32B15/01 , C23C30/00 , B22F5/00 , B23K10/02 , B23K26/34 , F01D5/14 , F01D5/28 , B22F7/04 , B23K101/00
Abstract: A hybrid article is disclosed including a coating disposed on and circumscribing the lateral surface of a core having a core material. The coating includes about 35% to about 95% of a first metallic material having a first melting point, and about 5% to about 65% of a second metallic material having a second melting point lower than the first melting point. The coating is sinter-bonded to the core. A method for forming the hybrid article is disclosed including disposing the core in a die, introducing a slurry having the metallic materials into a gap between the lateral surface and the die, and sintering the slurry, forming the coating. A method for closing an aperture of an article is disclosed including inserting the hybrid article into the aperture, and brazing the hybrid article to the article, welding the aperture with the hybrid article serving as weld filler, or both.
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公开(公告)号：US10227878B2
公开(公告)日：2019-03-12
申请号：US15065968
申请日：2016-03-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Srikanth Chandrudu Kottilingam , Yan Cui , Brian Lee Tollison , David Edward Schick
Abstract: An article and method of forming an article are provided. The article includes a side wall at least partially defining an inner region and an outer region of the article, the side wall having a first end and a second end, an end wall formed proximal to the first end of the side wall, the end wall defining a tip portion of the article, and a cooling channel formed in the side wall, within the tip portion. The method of forming an article includes positioning a first sheet of material having a channel formed therein over a first end of a body, positioning at least one additional sheet of material over the first sheet of material, and securing the first sheet of material and the at least one additional sheet of material to the body to form a tip portion including a cooling channel formed therein.
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公开(公告)号：US10126119B2
公开(公告)日：2018-11-13
申请号：US15407595
申请日：2017-01-17
Applicant: General Electric Company
Inventor： Brian Lee Tollison , Srikanth Chandrudu Kottilingam , Yan Cui , Bryan Joseph Germann
Abstract: A method of forming a passive strain indicator on a preexisting component includes directly depositing a plurality of fiducial markers on a portion of the outer surface of the preexisting component, the fiducial markers including a material that is compatible with the material of the outer surface. A method of evaluating a component includes initially scanning a plurality of fiducial markers on a portion of an outer surface of the component, subjecting the component to at least one duty cycle, subsequently scanning the plurality of fiducial markers after the at least one duty cycle, measuring a displacement of the plurality of fiducial markers by comparing the subsequent scan to the initial scan, and determining a remaining usable life of the component by looking up in a database a predetermined value of the remaining usable life of the component corresponding to the measured displacement of the plurality of fiducial markers.
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公开(公告)号：US20180202799A1
公开(公告)日：2018-07-19
申请号：US15407595
申请日：2017-01-17
Applicant: General Electric Company
Inventor： Brian Lee Tollison , Srikanth Chandrudu Kottilingam , Yan Cui , Bryan Joseph Germann
CPC classification number: G01B11/165 , G01B11/002 , G01B11/24 , G01B21/047 , G01M15/14
Abstract: A method of forming a passive strain indicator on a preexisting component includes directly depositing a plurality of fiducial markers on a portion of the outer surface of the preexisting component, the fiducial markers including a material that is compatible with the material of the outer surface. A method of evaluating a component includes initially scanning a plurality of fiducial markers on a portion of an outer surface of the component, subjecting the component to at least one duty cycle, subsequently scanning the plurality of fiducial markers after the at least one duty cycle, measuring a displacement of the plurality of fiducial markers by comparing the subsequent scan to the initial scan, and determining a remaining usable life of the component by looking up in a database a predetermined value of the remaining usable life of the component corresponding to the measured displacement of the plurality of fiducial markers.
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公开(公告)号：US20170089216A1
公开(公告)日：2017-03-30
申请号：US14865015
申请日：2015-09-25
Applicant: General Electric Company
Inventor： Yan Cui , Ganjiang Feng , Srikanth Chandrudu Kottilingam , Dechao Lin , Brian Lee Tollison
CPC classification number: F01D21/003 , F01D5/12 , F01D5/147 , F01D17/02 , F05D2260/80 , Y02T50/673
Abstract: Embodiments of the present disclosure provide turbine buckets, turbomachinery, and related methods for identifying bucket deformation. A turbine bucket according to embodiments of the present disclosure can include an airfoil extending radially from a base, relative to a rotor axis of a turbomachine; and a magnetized material coupled to the airfoil proximal to a radially outer end thereof. To identify bucket deformation, a magnetic sensor can measure a magnetic field strength of the magnetized material, and a computing device in communication with the magnetic sensor can identify the turbine bucket as being one of deformed and non-deformed based on the magnetic field strength of the magnetized material.
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Patent Agency Ranking
公开(公告)号：US20160326613A1
公开(公告)日：2016-11-10
申请号：US14706151
申请日：2015-05-07
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Yan Cui , Ganjiang Feng , Srikanth Chandrudu Kottilingam , Matthew Laylock , Brian Lee Tollison
IPC: C22C19/05 , B23K26/342 , B22F3/24 , C22F1/10 , B22F3/105
CPC classification number: C22C19/055 , B22F3/1055 , B22F3/24 , B22F2003/248 , B23K26/342 , B33Y10/00 , B33Y80/00 , C22C1/0433 , C22C19/05 , C22F1/10 , Y02P10/295
Abstract: An article and a method for forming the article are disclosed. The article comprising a composition, wherein the composition comprises, by weight percent, about 20.0% to about 22.0% chromium (Cr), about 18.0% to about 20.0% cobalt (Co), about 1.0% to about 2.0% tungsten (W), about 3.0% to about 6.0% niobium (Nb), about 0.5% to about 1.5% titanium (Ti), about 2.0% to about 3.0% aluminum (Al), about 0.5% to about 1.5% molybdenum (Mo), about 0.03% to about 0.18% carbon (C), up to about 0.15% tantalum (Ta), up to about 0.20% hafnium (Hf), up to about 0.20% iron (Fe),balance nickel (Ni) and incidental impurities. The amount of Al is present according to the following formula: Al≦−(0.5*Ti)+3.75 The composition is weldable, has a microstructure comprising between about 35 vol % and 45 vol % gamma prime (γ′) and is substantially devoid of Eta and reduced content of TCP phases at elevated working temperatures. A method of making an article and a method of operating a gas turbine are also disclosed.
Abstract translation: 组合物是可焊接的，具有包含约35vol％至45vol％的γ'（γ'）的微结构，并且在升高的工作温度下基本上不含Eta并且降低了TCP相的含量。 还公开了制造物品的方法和操作燃气轮机的方法。
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47.发明申请公开(公告)号：US20160115799A1
公开(公告)日：2016-04-28
申请号：US14522824
申请日：2014-10-24
Applicant: General Electric Company
Inventor： Dechao Lin , Wei Chen , Xiaoxue Diao , Paul Stephen Dimascio , Srikanth Chandrudu Kottilingam , Brian Lee Tollison
CPC classification number: B23K9/16 , B23K9/0026 , B23K9/046 , B23K9/23 , B23K2101/001 , B23K2101/045 , F01D5/186 , F05D2230/232 , F05D2230/30 , F05D2240/127 , F05D2260/2212 , F23R3/002 , F23R3/005 , F23R2900/00018 , F23R2900/03045 , Y02T50/676
Abstract: A method of forming a plurality of turbulators on a turbomachine surface includes depositing a portion of material on the turbomachine surface forming a first portion of the plurality of turbulators, adding additional material to the first portion, and establishing a desired dimension of the plurality of turbulators.
Abstract translation: 在涡轮机表面上形成多个湍流器的方法包括将一部分材料沉积在涡轮机表面上，形成多个湍流器的第一部分，向第一部分添加额外的材料，以及建立多个湍流器的期望尺寸 。
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公开(公告)号：US20150129644A1
公开(公告)日：2015-05-14
申请号：US14602865
申请日：2015-01-22
Applicant: General Electric Company
Inventor： Yan Cui , Srikanth Chandrudu Kottilingam , Dechao Lin , Brian Lee Tollison
CPC classification number: B23K35/304 , B23K31/02 , B23K35/0261 , B23K35/3033 , C22C19/051 , C22C19/056 , C22C19/057
Abstract: A metal chemistry includes an amount of chromium weight of between about 9.0% and about 16% by weight, an amount of cobalt of between about 7.0% and about 14% by weight, an amount of molybdenum of between about 10% and about 20% by weight, an amount of iron of between about 1.0% and about 5.0% by weight, an amount of aluminum of between about 0.05% and about 0.75% by weight, an amount of titanium of between about 0.5% and about 2.0% by weight, an amount of manganese not to exceed about 0.8% by weight, an amount of carbon of between about 0.02% and about 0.10% by weight, an amount of a titanium+aluminum alloy of between about 0.55% and about 2.75% by weight, and an amount of nickel.
Abstract translation: 金属化学性质包括约9.0％至约16％重量的铬重量，约7.0％至约14％重量的钴的量，约10％至约20％的钼的量， 的铁量为约1.0％至约5.0％，铝的量为约0.05％至约0.75％重量，钛的量为约0.5％至约2.0％重量 ，锰的量不超过约0.8重量％，碳量在约0.02重量％至约0.10重量％之间，钛+铝合金的量在约0.55重量％至约2.75重量％之间， 和一定量的镍。
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49.发明申请公开(公告)号：US20150030460A1
公开(公告)日：2015-01-29
申请号：US13948240
申请日：2013-07-23
Applicant: General Electric Company
Inventor： Srikanth Chandrudu Kottilingam , Yan Cui , Brian Lee Tollison , David Edward Schick , Jonathan Matthew Lomas , Gareth William David Lewis
CPC classification number: F01D5/005 , B23P6/005 , B23P2700/06 , F01D5/182 , F01D5/186 , F01D5/187 , F01D5/20 , F05D2230/22 , F05D2230/236 , F05D2230/80 , F05D2240/307 , Y02T50/671 , Y02T50/676 , Y10T29/49318 , Y10T29/49737 , Y10T29/49902
Abstract: Methods for modifying a plurality of cooling holes of a component include disposing a recess-shaped modification in a recess of the component comprising a plurality of cooling hole outlets, wherein the recess-shaped modification is formed to substantially fill the recess and comprising a plurality of modified cooling holes passing there through. The method further includes aligning the plurality of modified cooling holes of the recess-shaped modification with the plurality of cooling hole outlets of the component, and, bonding the recess-shaped modification disposed in the recess to the component, wherein the plurality of modified cooling holes of the recess-shaped modification is fluidly connected with the plurality of cooling holes of the component.
Abstract translation: 用于修改部件的多个冷却孔的方法包括在包括多个冷却孔出口的部件的凹部中设置凹陷形变型，其中所述凹形修改形成为基本上填充所述凹部并且包括多个 修改后的冷却孔通过。 该方法还包括将凹形变形体的多个改进的冷却孔与部件的多个冷却孔出口对准，并且将设置在凹部中的凹形修改件与部件结合，其中多个改进的冷却 凹形变形体的孔与部件的多个冷却孔流体连接。
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公开(公告)号：US11753724B2
公开(公告)日：2023-09-12
申请号：US17816472
申请日：2022-08-01
Applicant: General Electric Company
Inventor： Yan Cui , Matthew Joseph Laylock , Brian Lee Tollison
Abstract: Methods of forming a desired geometry at a location on a superalloy part are disclosed. The method may include directing particles of a powder mixture including a low melt temperature superalloy powder and a high melt temperature superalloy powder to the location on the superalloy part at a velocity sufficient to cause the superalloy powders to deform and to form a mechanical bond but not a metallurgical bond to the superalloy part. The directing of particles continues until the desired geometry is formed. Heat is applied to the powder mixture on the repair location. The heat causes the low melt temperature superalloy powder to melt, creating the metallurgical bonding at the location. Another method uses the same directing to form a preform for repairing the location on the part. The low melt temperature superalloy powder melts at less than 1287° C., and the high melt temperature superalloy powder melts at greater than 1287° C.
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