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公开(公告)号：US20190323111A1
公开(公告)日：2019-10-24
申请号：US16451430
申请日：2019-06-25
Applicant: General Electric Company
Inventor： William Thomas Carter , Todd Jay Rockstroh , Douglas Gerard Konitzer
IPC: C22F1/10 , B33Y50/02 , B23K26/144 , B23K26/70 , B23K26/342 , B22F3/105 , B23K26/00 , B33Y30/00 , B33Y10/00 , B23K26/14 , B22F5/04 , B23K26/03 , B33Y80/00
Abstract: Methods for direct writing of single crystal super alloys and metals are provided. The method can include: heating a substrate positioned on a base plate to a predetermined temperature using a first heater; using a laser to form a melt pool on a surface of the substrate; introducing a superalloy powder to the melt pool; measuring the temperature of the melt pool; receiving the temperature measured at a controller; and using an auxiliary heat source in communication with the controller to adjust the temperature of the melt pool. The predetermined temperature is below the substrate's melting point. The laser and the base plate are movable relative to each other, with the laser being used for direct metal deposition. An apparatus is also generally provided for direct writing of single crystal super alloys and metals.
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公开(公告)号：US20140377125A1
公开(公告)日：2014-12-25
申请号：US14482811
申请日：2014-09-10
Applicant: General Electric Company
Inventor： Wei-Jun Zhang , Douglas Gerard Konitzer , JOSHUA LEIGH MILLER
IPC: C22C19/05
CPC classification number: C22C19/057 , C30B11/00 , C30B29/52 , F01D5/28 , F05C2201/0466
Abstract: A nickel-based superalloy composition includes from about 5 to about 7 wt % aluminum, from about 4 to about 8 wt % tantalum, from about 3 to about 8 wt % chromium, from about 3 to about 7 wt % tungsten, from 1 to about 5 wt % molybdenum, from 1.5 to about 5 wt % rhenium, from 5 to about 14 wt % cobalt, from about 0 to about 1 wt % hafnium, from about 0.01 to about 0.03 wt % carbon, from about 0.002 to about 0.006 wt % boron, and balance nickel and incidental impurities. The composition may exhibit a sustained peak low cycle fatigue life at 1800° F./45 ksi of at least about 4000 cycles. The nickel-based superalloy composition may be used in single-crystal or directionally solidified superalloy articles, such as a blade, nozzle, a shroud, a splash plate, and a combustor of a gas turbine engine.
Abstract translation: 镍基超级合金组合物包括约5至约7重量％的铝，约4至约8重量％的钽，约3至约8重量％的铬，约3至约7重量％的钨，1至 约5重量％的钼，1.5至约5重量％的铼，5至约14重量％的钴，约0至约1重量％的铪，约0.01至约0.03重量％的碳，约0.002至约0.006 重量百分比的硼，余量为镍和杂质。 组合物可以在至少约4000个循环的1800°F / 45ksi下表现出持续的峰值低循环疲劳寿命。 镍基超合金组合物可以用于单晶或定向凝固的超合金制品，例如叶片，喷嘴，护罩，飞溅板和燃气涡轮发动机的燃烧器。
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公开(公告)号：US08858876B2
公开(公告)日：2014-10-14
申请号：US13665280
申请日：2012-10-31
Applicant: General Electric Company
Inventor： Wei-Jun Zhang , Douglas Gerard Konitzer , Joshua Leigh Miller
IPC: C22C19/05
CPC classification number: C22C19/057 , C30B11/00 , C30B29/52 , F01D5/28 , F05C2201/0466
Abstract: A nickel-based superalloy composition includes from about 5 to about 7 wt % aluminum, from about 4 to about 8 wt % tantalum, from about 3 to about 8 wt % chromium, from about 3 to about 7 wt % tungsten, from 1 to about 5 wt % molybdenum, from 1.5 to about 5 wt % rhenium, from 5 to about 14 wt % cobalt, from about 0 to about 1 wt % hafnium, from about 0.01 to about 0.03 wt % carbon, from about 0.002 to about 0.006 wt % boron, and balance nickel and incidental impurities. The composition may exhibit a sustained peak low cycle fatigue life at 1800° F./45 ksi of at least about 4000 cycles. The nickel-based superalloy composition may be used in single-crystal or directionally solidified superalloy articles, such as a blade, nozzle, a shroud, a splash plate, and a combustor of a gas turbine engine.
Abstract translation: 镍基超级合金组合物包括约5至约7重量％的铝，约4至约8重量％的钽，约3至约8重量％的铬，约3至约7重量％的钨，1至 约5重量％的钼，1.5至约5重量％的铼，5至约14重量％的钴，约0至约1重量％的铪，约0.01至约0.03重量％的碳，约0.002至约0.006 重量百分比的硼，余量为镍和杂质。 组合物可以在至少约4000个循环的1800°F / 45ksi下表现出持续的峰值低循环疲劳寿命。 镍基超合金组合物可以用于单晶或定向凝固的超合金制品，例如叶片，喷嘴，护罩，飞溅板和燃气涡轮发动机的燃烧器。
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公开(公告)号：US20240033810A1
公开(公告)日：2024-02-01
申请号：US18482060
申请日：2023-10-06
Applicant: General Electric Company
CPC classification number: B22C9/10 , B22C9/106 , B22D29/002 , B33Y10/00
Abstract: A method is provided for casting a component. Accordingly, a casting core is provided within a cavity of a component mold. The casting core defines an inner component shape and includes a core wall. The core wall defines a core outer surface and a core inner surface disposed opposite the core outer surface. The core inner surface defines a core cavity. The casting core also includes a removal facilitation feature. The component is cast within the cavity of the component mold with the casting core positioned therein. The cast component is removed from the component mold and the casting core is removed from the cast component.
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25.发明授权公开(公告)号：US11529672B2
公开(公告)日：2022-12-20
申请号：US17228168
申请日：2021-04-12
Applicant: General Electric Company
Inventor： Xi Yang , Michael Cole , Michael Brown , Gregory Terrence Garay , Tingfan Pang , Brian David Przeslawski , Douglas Gerard Konitzer
IPC: B22C9/10 , B22C9/04 , B22C9/24 , B22D29/00 , B28B1/00 , B33Y10/00 , B33Y80/00 , C04B35/622 , B28B7/34
Abstract: A method of forming a cast component and a method of forming a casting mold is described herein. The ceramic core-shell mold includes at least first core portion, a first shell portion, and at least one first cavity between the core portion and the first shell portion. The core-shell mold may be manufactured using an additive manufacturing process and may include an integrated ceramic filter. At least a portion of the ceramic core-shell mold and the wax gate component is coated with a second ceramic material. The wax gate component is then removed to form a second cavity in fluid communication with the first cavity.
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Patent Agency Ranking
公开(公告)号：US11499431B2
公开(公告)日：2022-11-15
申请号：US17142788
申请日：2021-01-06
Applicant: General Electric Company
IPC: F01D5/14 , G06F30/17 , G06F113/06
Abstract: An apparatus and method for forming an engine component for a turbine engine, the engine component comprising a wall bounding an interior; a panel portion defining a portion of the wall, the panel portion comprising: an outer wall; an inner wall spaced from the outer wall to define a wall gap; and a structural segment formed within the wall gap comprising at least one structural element. The method including calculating a factor and adjusting a variable until the factor is between a given range.
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公开(公告)号：US20220193770A1
公开(公告)日：2022-06-23
申请号：US17126245
申请日：2020-12-18
Applicant: General Electric Company
Inventor： Douglas Gerard Konitzer , Andrew William Emge , Andrew Ezekiel Wessman
Abstract: A method for additively manufacturing components includes additively printing a metallic preform such that the preform contains a predetermined amount of porosity. Furthermore, the method includes working the additively printed preform such that the preform incurs a predetermined amount of deformation. Moreover, the method includes heat treating the worked preform to form a final component.
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公开(公告)号：US20220080495A1
公开(公告)日：2022-03-17
申请号：US17532396
申请日：2021-11-22
Applicant: General Electric Company
Inventor： Xi Yang , Michael Cole , Michael Brown , Gregory Terrence Garay , Tingfan Pang , Brian David Przeslawski , Douglas Gerard Konitzer
Abstract: The present disclosure relates to a method of forming a cast component and a method of forming a casting mold. The method is performed by connecting at least one wax gate component to a ceramic core-shell mold. The ceramic core-shell mold includes at least a first core portion, a first shell portion, and a second shell portion, wherein the first shell portion is adapted to interface with at least the second shell portion to form at least one first cavity between the core portion and the first and second shell portions. The core-shell mold may be inspected and assembled prior to connection of the wax gate component. At least a portion of the ceramic core-shell mold and the wax gate component is coated with a second ceramic material. The wax gate component is then removed to form a second cavity in fluid communication with the first cavity.
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公开(公告)号：US20220080494A1
公开(公告)日：2022-03-17
申请号：US17019646
申请日：2020-09-14
Applicant: General Electric Company
Abstract: A method is provided for casting a component. Accordingly, a casting core is provided within a cavity of a component mold. The casting core defines an inner component shape and includes a core wall. The core wall defines a core outer surface and a core inner surface disposed opposite the core outer surface. The core inner surface defines a core cavity. The casting core also includes a removal facilitation feature. The component is cast within the cavity of the component mold with the casting core positioned therein. The cast component is removed from the component mold and the casting core is removed from the cast component.
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公开(公告)号：US11235378B2
公开(公告)日：2022-02-01
申请号：US16531842
申请日：2019-08-05
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Xi Yang , Michael Cole , Michael Brown , Gregory Terrence Garay , Tingfan Pang , Brian David Przeslawski , Douglas Gerard Konitzer
Abstract: Integrated core-shell investment casting molds include a filament structure corresponding to a cooling hole pattern in the surface of the turbine blade, stator vane, or shroud.
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