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公开(公告)号:US20190093498A1
公开(公告)日:2019-03-28
申请号:US16141803
申请日:2018-09-25
Applicant: Rolls-Royce Corporation , Rolls-Royce PLC
Inventor: Stephanie Gong , Taylor K. Blair , Ngunjoh Lawrence Ndamka , Li Li , Sunny Chang , Ann Bolcavage
Abstract: An article includes a substrate, a bond coat on the substrate, and a multilayer environmental barrier coating (EBC) on the bond coat. The multilayer EBC includes a first EBC layer defining a first thickness and a second EBC layer defining a second thickness. The first EBC layer includes a first rare earth disilicate and a first concentration of a sintering aid that includes alumina. The second EBC layer includes a second rare earth disilicate and a second concentration of the sintering aid that includes alumina, less than the first concentration of the sintering aid.
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公开(公告)号:US20190093497A1
公开(公告)日:2019-03-28
申请号:US16135036
申请日:2018-09-19
Applicant: Rolls-Royce Corporation , Rolls-Royce plc
Inventor: Ngunjoh Lawrence Ndamka , Li Li , Stephanie Gong , Sunny Chang , Ann Bolcavage , Taylor K. Blair
IPC: F01D11/12
Abstract: An article for use in a high-temperature environment that includes a substrate including a superalloy material, a ceramic, or a ceramic matrix composite, and an abradable coating on the substrate, the abradable coating including a rare earth silicate and a dislocator phase, the dislocator phase forms one or more distinct phase regions in the abradable coating and comprises at least one of hafnium diboride (HfB2), zirconium diboride (ZrB2), tantalum nitride (TaN or Ta2N), tantalum carbide (Ta2C) titanium diboride (TiB2), zirconium carbide (ZrC), hafnium carbide (HfC), tantalum diboride (TaB2), hafnium nitride (HfN), or niobium carbide (NbC).
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公开(公告)号:US20190017177A1
公开(公告)日:2019-01-17
申请号:US16034801
申请日:2018-07-13
Inventor: Matthew R. Gold , Michael Cybulsky , Stephanie Gong , Li Li
Abstract: An article that includes a substrate; a first layer including yttria and zirconia or hafnia, where the first layer has a columnar microstructure and includes predominately the zirconia or hafnia; a second layer on the first layer, the second layer including zirconia or hafnia, ytterbia, samaria, and at least one of lutetia, scandia, ceria, neodymia, europia, and gadolinia, where the second layer includes predominately zirconia or hafnia, and where the second layer has a columnar microstructure; and a third layer on the second layer, the third layer including zirconia or hafnia, ytterbia, samaria, and a rare earth oxide including at least one of lutetia, scandia, ceria, neodymia, europia, and gadolinia, where the third layer has a dense microstructure and has a lower porosity than the second layer.
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公开(公告)号:US20180370863A1
公开(公告)日:2018-12-27
申请号:US16014660
申请日:2018-06-21
Inventor: Li Li , Sungbo Shim , Sunny Chang
Abstract: A method of forming an impurity barrier layer on a CMC substrate may include introducing, to a heated plume of a thermal spray gun, a composite feedstock that includes a first coating material including a plurality of first particles; and a second coating material that may be different from the first coating material, where the second coating material at least partially encapsulates at least a portion of respective surfaces of the plurality of first particles; and directing, using the heated plume, at least the first coating material to a surface of a CMC substrate to deposit an impurity barrier layer including at least the first coating material.
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公开(公告)号:US12227464B2
公开(公告)日:2025-02-18
申请号:US17302996
申请日:2021-05-18
Inventor: Li Li , Matthew T. Kush , Robert Alexander Sean Golden , Jun Shi
IPC: C04B41/89 , C04B35/16 , C04B35/80 , C04B41/00 , C04B41/50 , C04B41/52 , C04B41/87 , F01D5/28 , C04B103/61 , C04B111/00 , C04B111/20
Abstract: An article may include a substrate, such as a silicon-containing ceramic matrix composite, an environmental barrier coating (EBC) layer on the substrate, and a CMAS-resistant EBC layer on the EBC layer. The EBC layer may include at least one rare-earth disilicate (REDS). The CMAS-resistant EBC layer may include at least one rare-earth monosilicate (REMS) configured to react with CMAS to form crystalline reaction products. The CMAS-resistant EBC layer may include a plurality of vertical cracks extending from a surface of the CMAS-resistant EBC layer at least partially into the CMAS-resistant EBC layer. Additionally, or alternatively, the EBC layer may include a plurality of vertical cracks extending from a surface of the EBC layer into at least a portion of the EBC layer.
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公开(公告)号:US11976013B2
公开(公告)日:2024-05-07
申请号:US16138580
申请日:2018-09-21
Applicant: Rolls-Royce Corporation , Rolls-Royce plc
Inventor: Stephanie Gong , Ngunjoh Lawrence Ndamka , Matthew R. Gold , Li Li , Taylor K. Blair , Sunny Chang , Ann Bolcavage
CPC classification number: C04B41/52 , B05B7/205 , C04B35/62807 , C04B35/6281 , C04B35/62813 , C04B35/62815 , C04B35/62828 , C04B35/62831 , C04B35/62884 , C04B41/4545 , C04B41/4582 , C04B41/5024 , C04B41/5031 , C04B41/5035 , C04B41/5042 , C04B41/5057 , C04B41/5068 , C04B41/507 , C04B41/85 , C04B41/89 , F01D5/288 , C04B2235/3208 , C04B2235/3224 , C04B2235/3248 , C04B2235/3813 , C04B2235/3886 , C04B41/5024 , C04B41/4527 , C04B41/5031 , C04B41/5045 , C04B2103/0021 , C04B41/52 , C04B41/5053 , C04B41/5057 , C04B41/5096 , C04B41/52 , C04B41/4527 , C04B41/5024 , C04B2103/0021
Abstract: An article may include a substrate including a ceramic matrix composite (CMC); a composite coating layer including a first coating material that includes a rare-earth disilicate and a second coating material that includes at least one of a rare-earth monosilicate, a CMAS-resistant material, or a high-temperature dislocating material, where the second coating material forms a substantially continuous phase in the composite coating layer.
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公开(公告)号:US11958787B2
公开(公告)日:2024-04-16
申请号:US17119345
申请日:2020-12-11
Inventor: Robert Alexander Sean Golden , Sungbo Shim , Li Li , Taylor K. Blair
CPC classification number: C04B41/522 , C04B35/80 , C04B41/0072 , C04B41/009 , C04B41/4521 , C04B41/5024 , C04B41/87 , C04B41/89
Abstract: The disclosure describes braze tape coatings and technique to form articles with differing physical properties in different layers or regions of the article. An example method includes forming a braze tape defining at least one layer that includes a first segment and a second segment. A portion of the second segment in the plane is adjacent to a portion of the first segment in a plane of the layer. The method also includes positioning the braze tape on a surface of a substrate, the plane of the layer of the braze tape being parallel to the surface of the substrate. The method also includes heating the braze tape to melt a constituent of at least one of the first coating material and the second coating material to form a densified coating on the surface of the substrate.
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公开(公告)号:US11952317B2
公开(公告)日:2024-04-09
申请号:US16657504
申请日:2019-10-18
Applicant: Rolls-Royce Corporation , Rolls-Royce plc
Inventor: Ngunjoh Lawrence Ndamka , Li Li , Stephanie Gong , Ann Bolcavage , Taylor K. Blair , Robert Golden
CPC classification number: C04B41/5024 , C04B41/4543 , F01D5/284 , F01D5/288
Abstract: An example article includes a substrate and a barrier coating on the substrate. The barrier coating includes a matrix including a rare-earth disilicate extending from an inner interface facing the substrate to an outer surface opposite the inner interface. The barrier coating includes a graded volumetric distribution of rare-earth oxide rich (REO-rich) phase regions in the matrix along a direction from the inner interface to the outer surface. The graded volumetric distribution defines a first volumetric density of the REO-rich phase regions at a first region of the matrix adjacent the outer surface. The graded volumetric distribution defines a second volumetric density of the REO-rich phase regions at a second region of the matrix adjacent the inner surface. The second volumetric density is different from the first volumetric density. An example technique includes forming the barrier coating on the substrate of a component.
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公开(公告)号:US20240076245A1
公开(公告)日:2024-03-07
申请号:US17929255
申请日:2022-09-01
Applicant: Rolls-Royce Corporation
Inventor: Gregory John Kenneth Harrington , Li Li , Robert Alexander Sean Golden
CPC classification number: C04B41/85 , C04B41/4582 , C04B41/5024 , C04B2235/402 , C04B2235/96
Abstract: An article having a coating system configured to inhibit or prevent crystallization of TGO at the operating temperature of the article. An article includes a substrate defining a surface and a coating layer that includes a dopant configured to inhibit crystallization of amorphous silicon dioxide thermally grown oxide on the bond coat at an operating temperature of the article. The dopant includes a glass modifier. By inhibiting or preventing TGO crystallization, the described coating systems may increase a useable life of the component.
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公开(公告)号:US11624289B2
公开(公告)日:2023-04-11
申请号:US17302003
申请日:2021-04-21
Inventor: Stephanie Gong , Scott Nelson , Sungbo Shim , Li Li , Robert Alexander Sean Golden
IPC: F01D5/28
Abstract: In some examples, the disclosure describes an article and a method of making the same that includes a substrate defining an outer surface, a barrier layer on the outer surface of the substrate, the barrier layer defining a textured surface having a plurality of cells, each cell having a geometry and a depth, and an overlying layer formed on the textured surface of the barrier layer. The barrier layer may be configured to reduce migration of material from the substrate to the overlaying layer to reduce or prevent formation of cristobalite phase thermally grown oxide.
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