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公开(公告)号:US11242588B2
公开(公告)日:2022-02-08
申请号:US16712130
申请日:2019-12-12
Applicant: General Electric Company
Abstract: Embodiments of the disclosure provide a system including: an enclosure having an interior sized to enclose and the workpiece and form a vacuum and pressurized atmosphere within the interior. A plurality of thermal applicators may be in thermal communication with first and second portions of the interior. First and second thermal applicators may independently heat and cool the first and second portions of the interior. The first thermal applicator may apply a first thermal treatment to a first portion of the workpiece in the first portion of the interior. A second thermal applicator may apply a second thermal treatment to a second portion of the workpiece in the second portion of the interior independently of the first thermal treatment.
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公开(公告)号:US20210246534A1
公开(公告)日:2021-08-12
申请号:US16784781
申请日:2020-02-07
Applicant: General Electric Company
Inventor: Yan Cui , Jon Conrad Schaeffer , Michael Douglas Arnett , Matthew Joseph Laylock , Brian Lee Tollison
Abstract: A nickel-based superalloy composition including by weight percent: Cobalt 7.5; Chromium 9.75; Aluminum 5.45; Titanium 1.0; Niobium 3.5; Tungsten 6.0; Molybdenum 1.5; Carbon 0.08; Hafnium 0.15; Boron 0.01; and Nickel 65.0; and incidental impurities.
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公开(公告)号:US20210189539A1
公开(公告)日:2021-06-24
申请号:US16718797
申请日:2019-12-18
Applicant: General Electric Company
Inventor: Michael Douglas Arnett , Jon Conrad Schaeffer , Arthur Samuel Peck , Maxim Konter
Abstract: In a non-limiting example, an article having a body including a nickel-based superalloy is provided. The nickel-based superalloy has a microstructure that includes a gamma phase matrix and a gamma prime phase including a plurality of rafting-resistant gamma prime particles dispersed in the gamma phase matrix. The plurality of the rafting-resistant gamma prime particles has an average particle perimeter of about 3 microns to about 15 microns, an average aspect ratio of about 1.2 to about 3, and where the microstructure of the nickel-based superalloy is substantially uniform throughout the body.
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公开(公告)号:US09671030B2
公开(公告)日:2017-06-06
申请号:US13690233
申请日:2012-11-30
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Paul Stephen Dimascio , Michael Douglas Arnett , Rebecca Evelyn Hefner , Christopher D. Higgins
CPC classification number: F16K31/002 , F01D11/003 , F01D11/18 , F01D17/085 , F05D2300/5021 , F16J15/164 , F16J15/445
Abstract: A metallic seal assembly, a turbine component, and a method of regulating flow in turbo-machinery are disclosed. The metallic seal assembly includes a sealing structure having thermally-responsive features. The thermally-responsive features deploy from or retract toward a surface of the sealing structure in response to a predetermined temperature change. The turbine component includes the metallic seal assembly. The method of regulating flow in turbo-machinery includes providing the metallic seal assembly and raising or retracting the thermally-responsive features in response to the predetermined temperature change.
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公开(公告)号:US11384414B2
公开(公告)日:2022-07-12
申请号:US16784781
申请日:2020-02-07
Applicant: General Electric Company
Inventor: Yan Cui , Jon Conrad Schaeffer , Michael Douglas Arnett , Matthew Joseph Laylock , Brian Lee Tollison
Abstract: A nickel-based superalloy composition including by weight percent: Cobalt 7.5; Chromium 9.75; Aluminum 5.45; Titanium 1.0; Niobium 3.5; Tungsten 6.0; Molybdenum 1.5; Carbon 0.08; Hafnium 0.15; Boron 0.01; and Nickel 65.0; and incidental impurities.
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公开(公告)号:US11199101B2
公开(公告)日:2021-12-14
申请号:US16712136
申请日:2019-12-12
Applicant: General Electric Company
Inventor: Michael Douglas Arnett , Jon Conrad Schaeffer , Arthur Samuel Peck
Abstract: Embodiments of the disclosure provide a turbomachine component, including: a base portion configured for mounting on a rotor; an airfoil portion having a first end coupled to the base portion, and a second end opposite the first end. A creep resistance of the airfoil portion is greater than the base portion, and a fracture toughness of the airfoil portion is less than the base portion. A tip portion may be coupled to the second end of the airfoil portion. A creep resistance of the tip portion is less than the airfoil portion and greater than the base portion. A fracture toughness of the tip portion is less than the base portion and greater than the airfoil portion.
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公开(公告)号:US20210180461A1
公开(公告)日:2021-06-17
申请号:US16712136
申请日:2019-12-12
Applicant: General Electric Company
Inventor: Michael Douglas Arnett , Jon Conrad Schaeffer , Arthur Samuel Peck
Abstract: Embodiments of the disclosure provide a turbomachine component, including: a base portion configured for mounting on a rotor; an airfoil portion having a first end coupled to the base portion, and a second end opposite the first end. A creep resistance of the airfoil portion is greater than the base portion, and a fracture toughness of the airfoil portion is less than the base portion. A tip portion may be coupled to the second end of the airfoil portion. A creep resistance of the tip portion is less than the airfoil portion and greater than the base portion. A fracture toughness of the tip portion is less than the base portion and greater than the airfoil portion.
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公开(公告)号:US10266926B2
公开(公告)日:2019-04-23
申请号:US13868481
申请日:2013-04-23
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Ganjiang Feng , Jon Conrad Schaeffer , Michael Douglas Arnett
Abstract: A cast nickel-base superalloy that includes iron added substitutionally for nickel. The cast nickel base superalloy comprises, in weight percent about 1-6% iron, about 7.5-19.1% cobalt, about 7-22.5% chromium, about 1.2-6.2% aluminum, optionally up to about 5% titanium, optionally up to about 6.5% tantalum, optionally up to about 1% Nb, about 2-6% W, optionally up to about 3% Re, optionally up to about 4% Mo, about 0.05-0.18% C, optionally up to about 0.15% Hf, about 0.004-0.015 B, optionally up to about 0.1% Zr, and the balance Ni and incidental impurities. The superalloy is characterized by a γ′ solvus temperature that is within 5% of the γ′ solvus temperature of the superalloy that does not include 1-6% Fe and a mole fraction of γ′ that is within 15% of the mole fraction of the superalloy that does not include 1-6% Fe.
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公开(公告)号:US10253396B2
公开(公告)日:2019-04-09
申请号:US15255383
申请日:2016-09-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Jon Conrad Schaeffer , Shan Liu , Martin M. Morra , Michael Douglas Arnett
IPC: C22C19/05 , F01D5/28 , F01D9/04 , F01D25/00 , C22C19/03 , C22C30/00 , C22C45/00 , C22C45/04 , C22F1/10
Abstract: A modified alloy is disclosed including a base alloy composition and an additive gamma prime antioxidant. The base alloy composition includes a concentration of a gamma prime antioxidant less than an effective concentration of the gamma prime antioxidant. The additive gamma prime antioxidant is intermixed with the base alloy composition to form the modified alloy, preferentially segregating to a gamma prime phase of the modified alloy and increasing the concentration of the gamma prime antioxidant to be at least the effective concentration of the gamma prime antioxidant. The effective concentration imparts reduced oxidation susceptibility of the gamma prime phase. An article is disclosed including the modified alloy. A coated article is disclosed including a coating disposed on a surface of an article having the base alloy composition. The coated article includes a reduced stress accelerated gamma prime oxidation static crack growth susceptibility in comparison with the base alloy composition.
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公开(公告)号:US11725260B1
公开(公告)日:2023-08-15
申请号:US17716405
申请日:2022-04-08
Applicant: General Electric Company
Inventor: Yan Cui , Jon Conrad Schaeffer , Michael Douglas Arnett , Matthew Joseph Laylock , Brian Lee Tollison
CPC classification number: C22C19/056 , C22F1/10
Abstract: Compositions, and articles and methods for forming articles which include said compositions, are disclosed. The compositions include, by weight percent, about 13.7% to about 14.3% chromium (Cr), about 9.0% to about 9.9% cobalt (Co), about 4.0% to about 5.25% aluminum (Al), about 0.5% to about 3.0% titanium (Ti), about 4.5% to about 5.0% tungsten (W), about 1.4% to about 1.7% molybdenum (Mo), about 3.25% to about 3.75% niobium (Nb), about 0.08% to about 0.12% carbon (C), about 0.005% to about 0.04% zirconium (Zr), about 0.010% to about 0.014% boron (B), and balance nickel (Ni) and incidental impurities.
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