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公开(公告)号：US10822687B2
公开(公告)日：2020-11-03
申请号：US15431805
申请日：2017-02-14
Applicant: General Electric Company
Inventor： Atanu Saha , Nicholas Edward Antolino , Don Mark Lipkin
IPC: C04B35/505 , C23C12/00 , C23C8/62 , C04B41/89 , C04B41/00 , C04B41/52 , F01D5/28 , C04B35/50 , C23C30/00
Abstract: Methods of forming an environmental barrier coating are disclosed. A method includes disposing a powder-based coating on a substrate, heat-treating the powder-based coating at a temperature greater than 800° C. and less than 1200° C. to form a porous coating that includes surface-connected pores, infiltrating at least some of the surface-connected pores of the porous coating with an infiltrant material to form an infiltrated coating, and sintering the infiltrated coating at a temperature greater than 1200° C. and less than 1500° C. to form the environmental barrier coating on the substrate.
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2.发明申请METHODS OF FORMING AN ARTICLE USING ELECTROPHORETIC DEPOSITION, AND RELATED ARTICLE 审中-公开使用电泳沉积法形成文章的方法和相关文章公开(公告)号：US20160160374A1
公开(公告)日：2016-06-09
申请号：US14563257
申请日：2014-12-08
Applicant: General Electric Company
Inventor： Nicholas Edward Antolino , Don Mark Lipkin , Stephen Francis Rutkowski
CPC classification number: C25D13/22 , C04B41/009 , C04B41/52 , C04B41/89 , C23C18/165 , C25D13/02 , C25D13/12 , F01D5/288 , F05D2230/31 , C04B35/565 , C04B35/806 , C04B35/584 , C04B35/58085 , C04B41/5096 , C04B41/5059 , C04B41/522 , C04B41/5071 , C04B41/0072 , C04B41/4564 , C04B41/5024 , C04B2103/0021 , C04B41/4541 , C04B41/5116 , C04B41/4539 , C04B41/4549 , C04B41/48 , C04B41/526
Abstract: In one example of the present technology, a method for forming an article includes disposing an electrically conductive coating on a substrate. The method further includes disposing a layer stack on the electrically conductive coating by (i) disposing a first barrier coating by electrophoretic deposition; (ii) heat treating the first barrier coating; (iii) disposing an electrically conductive layer on the first barrier coating; and (iv) optionally repeating steps (i) to (iii). The method further includes disposing a second barrier coating on an outermost electrically conductive layer in the layer stack by electrophoretic deposition; and heat treating the second barrier coating.
Abstract translation: 在本技术的一个示例中，用于形成物品的方法包括在基板上设置导电涂层。 该方法还包括通过（i）通过电泳沉积设置第一屏障涂层来将层叠层设置在导电涂层上; （ii）热处理第一阻隔涂层; （iii）在第一阻挡涂层上设置导电层; 和（iv）任选地重复步骤（i）至（iii）。 该方法还包括通过电泳沉积在层堆叠中的最外导电层上设置第二阻挡涂层; 并对第二阻隔涂层进行热处理。
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3.发明授权公开(公告)号：US10392947B2
公开(公告)日：2019-08-27
申请号：US14797235
申请日：2015-07-13
Applicant: General Electric Company
Inventor： Glen Harold Kirby , Nicholas Edward Antolino
IPC: B23B7/04 , F01D5/28 , C04B41/89 , C04B41/00 , C04B41/52 , B32B7/04 , B32B18/00 , B32B37/06 , C04B35/71 , C04B41/50 , C04B41/87 , F01D5/14 , F01D25/00 , F01D11/12
Abstract: A coating system on a CMC substrate is provided, along with methods of its tape deposition onto a substrate. The coating system can include a bond coat on a surface of the CMC substrate; a first rare earth silicate coating on the bond coat; a first sacrificial coating of a first reinforced rare earth silicate matrix on the at least one rare earth silicate layer; a second rare earth silicate coating on the sacrificial coating; a second sacrificial coating of a second reinforced rare earth silicate matrix on the second rare earth silicate coating; a third rare earth silicate coating on the second sacrificial coating; and an outer layer on the third rare earth silicate coating. The first sacrificial coating and the second sacrificial coating have, independently, a thickness of about 4 mils to about 40 mils.
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4.发明申请公开(公告)号：US20170362939A1
公开(公告)日：2017-12-21
申请号：US15185194
申请日：2016-06-17
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , Nicholas Edward Antolino
Abstract: In one aspect, a method for performing in situ repairs of internal components of a gas turbine engine may generally include inserting a repair tool within an interior of the gas turbine engine such that a tip end of the repair tool is positioned within the gas turbine engine and an exterior end is positioned outside the gas turbine engine. The method may also include positioning the tip end of the repair tool adjacent to a defect of an internal component, wherein the defect defines a fillable volume along a portion of the internal component. In addition, the method may include intermixing two or more constituents of a repair agent within the repair tool at a mixing location defined within the gas turbine engine, and expelling the repair agent from the tip end such that the fillable volume is at least partially filled with the repair agent.
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5.发明申请公开(公告)号：US20210222556A1
公开(公告)日：2021-07-22
申请号：US17072265
申请日：2020-10-16
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , Nicholas Edward Antolino
Abstract: In one aspect, a method for performing in situ repairs of internal components of a gas turbine engine may generally include inserting a repair tool within an interior of the gas turbine engine such that a tip end of the repair tool is positioned within the gas turbine engine and an exterior end is positioned outside the gas turbine engine. The method may also include positioning the tip end of the repair tool adjacent to a defect of an internal component, wherein the defect defines a fillable volume along a portion of the internal component. In addition, the method may include intermixing two or more constituents of a repair agent within the repair tool at a mixing location defined within the gas turbine engine, and expelling the repair agent from the tip end such that the fillable volume is at least partially filled with the repair agent.
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Patent Agency Ranking
6.发明公开公开(公告)号：US20240150251A1
公开(公告)日：2024-05-09
申请号：US17979866
申请日：2022-11-03
Applicant: General Electric Company
Inventor： Atanu Saha , Don Mark Lipkin , Sreerama Prasad R , Mamatha Nagesh , Nicholas Edward Antolino
CPC classification number: C04B41/522 , C04B41/0072 , C04B41/009 , C04B41/4539 , C04B41/5024 , C04B41/5096 , C04B41/87 , C04B41/89
Abstract: Methods for repairing a defect in a multilayered coating on a silicon-containing substrate are provided, along with the resulting compared component. The method includes: applying a first patch slurry into the defect; drying the first patch slurry to form a dried first patch layer; applying a second patch slurry into the defect and on the dried first patch layer; and drying the second patch slurry to form a second dried patch layer.
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公开(公告)号：US20230234895A1
公开(公告)日：2023-07-27
申请号：US17584496
申请日：2022-01-26
Applicant: General Electric Company
Inventor： Glen Harold Kirby , Nathaniel Patrick Brown , Guruvenket Srinivasan , Reza Sarrafi-Nour , Nicholas Edward Antolino , Julin Wan , Anant Achyut Setlur , Taryn Elizabeth Hewitt
CPC classification number: C04B41/522 , C04B41/009 , C04B41/5096 , C04B41/5024 , C04B41/4529 , C04B41/0072
Abstract: Environmental barrier coatings including a bondcoat layer including silicon and a rare earth silicate-based hermetic layer and rare earth silicate-based non-hermetic layer are provided. The rare earth silicate-based hermetic layer is deposited on the bondcoat via a thermal spray process and has an elastic modulus ranging from 100 GPa to 180 GPa. The at least one rare earth silicate-based non-hermetic layer is deposited on the rare earth silicate-based hermetic layer and has an elastic modulus ranging from 50 GPa to 100 GPa. Coated gas turbine engine components and methods for coating gas turbine engine components are also provided.
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8.发明申请公开(公告)号：US20220169551A1
公开(公告)日：2022-06-02
申请号：US17108657
申请日：2020-12-01
Applicant: General Electric Company
Inventor： Atanu Saha , Manepalli Satya Kishore , Nicholas Edward Antolino , Don Mark Lipkin , Mamatha Nagesh
Abstract: Methods for forming a sintered patch on a silicon-based substrate are disclosed. The methods include applying a patch slurry on the silicon-based substrate, drying the patch slurry on the silicon-based substrate to form a dried patch material, and sintering the dried patch material in an oxidizing atmosphere to form a sintered patch on the silicon-based substrate. The patch slurry includes a patch material containing silicates in a fluid carrier.
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9.发明授权公开(公告)号：US10822950B2
公开(公告)日：2020-11-03
申请号：US15185194
申请日：2016-06-17
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , Nicholas Edward Antolino
Abstract: In one aspect, a method for performing in situ repairs of internal components of a gas turbine engine may generally include inserting a repair tool within an interior of the gas turbine engine such that a tip end of the repair tool is positioned within the gas turbine engine and an exterior end is positioned outside the gas turbine engine. The method may also include positioning the tip end of the repair tool adjacent to a defect of an internal component, wherein the defect defines a fillable volume along a portion of the internal component. In addition, the method may include intermixing two or more constituents of a repair agent within the repair tool at a mixing location defined within the gas turbine engine, and expelling the repair agent from the tip end such that the fillable volume is at least partially filled with the repair agent.
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公开(公告)号：US20190077692A1
公开(公告)日：2019-03-14
申请号：US16057925
申请日：2018-08-08
Applicant: General Electric Company
Inventor： Atanu SAHA , Don Mark Lipkin , Satya Kishore Manepalli , Nicholas Edward Antolino
Abstract: A method for forming a patch repair on a silicon-based component is disclosed. The method includes applying a patch on a damaged area of a silicon-based component, drying the patch to form a dried patch, and sintering in situ the dried patch to form a patch repaired portion of the silicon-based component. The patch includes a patching material and the patching material includes a plurality of nanoparticles having a median particle size less than 100 nanometers. The plurality of nanoparticles includes at least one of silicon, silicon alloy, silica, or a metal silicate.
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