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公开(公告)号：US11898465B2
公开(公告)日：2024-02-13
申请号：US17401914
申请日：2021-08-13
Applicant: Raytheon Technologies Corporation
Inventor： Brian Craig , James M. Koonankeil , Brian T. Hazel , Paul E. Denney , Dominic J. Mongillo
IPC: F01D5/28 , F01D5/00 , F01D5/18 , B23K26/382 , C23C4/073 , C23C4/11 , B23K101/00 , B23H9/10 , B23H9/14 , B23P9/00 , B23P15/02 , C23C4/06 , C23C4/12 , C23C4/16
CPC classification number: F01D5/288 , F01D5/005 , F01D5/186 , F01D5/284 , B23H9/10 , B23H9/14 , B23K26/389 , B23K2101/001 , B23P9/00 , B23P15/02 , B23P2700/06 , C23C4/06 , C23C4/073 , C23C4/11 , C23C4/12 , C23C4/16 , F05D2230/11 , F05D2230/90 , F05D2260/202 , F05D2300/2112
Abstract: A manufacturing method is provided. During this method, a preform component is provided for a turbine engine. The preform component includes a substrate. A preform meter section and a preform diffuser section are formed in the substrate. An internal coating is applied to at least the preform meter section to provide a meter section of a cooling aperture. External coating material is applied over the substrate. The applying of the external coating material forms an external coating over the substrate. The applying of the external coating also builds up the external coating material within the preform diffuser section to form a diffuser section of the cooling aperture.
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公开(公告)号：US20230416538A1
公开(公告)日：2023-12-28
申请号：US17849129
申请日：2022-06-24
Applicant: Raytheon Technologies Corporation
Inventor： Xia Tang , Richard Wesley Jackson, III , James T. Beals , David A. Litton , Brian T. Hazel
IPC: C09D5/08
CPC classification number: C09D5/084
Abstract: An article according to an exemplary embodiment of this disclosure, among other possible things includes a substrate and a barrier layer on the substrate. The barrier layer includes a bond coat comprising a matrix, diffusive particles disposed in the matrix, and gettering particles disposed in the matrix; a topcoat; and a porous interlayer disposed between the topcoat and the bond coat. The porous interlayer has a porosity that is greater than a porosity of the topcoat. A slurry composition for applying an interlayer to an article and method of applying a top coat to an article are also disclosed.
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公开(公告)号：US11813706B2
公开(公告)日：2023-11-14
申请号：US17401947
申请日：2021-08-13
Applicant: Raytheon Technologies Corporation
Inventor： Brian Craig , James M. Koonankeil , Brian T. Hazel , Paul E. Denney , Dominic J. Mongillo
IPC: B23P15/00
CPC classification number: B23P15/00 , B23P2700/06 , F05D2220/30 , F05D2230/90 , F05D2260/20
Abstract: A manufacturing method is provided during which a preform component for a turbine engine is provided. The preform component includes a substrate. An outer coating is applied over the substrate. A characteristic of the outer coating is determined. Instructions for forming a cooling aperture are revised based on the characteristic of the outer coating to provide revised instructions. The cooling aperture is formed in the outer coating and the substrate based on the revised instructions.
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公开(公告)号：US20230139765A1
公开(公告)日：2023-05-04
申请号：US17514371
申请日：2021-10-29
Applicant: Raytheon Technologies Corporation
Inventor： Elisa M. Zaleski , Brian T. Hazel , Kaylan M. Wessels
IPC: C04B35/195 , C04B35/622 , C04B35/657 , F02C7/00 , C23C16/30 , C23C14/08 , C23C16/455 , C23C28/04
Abstract: A calcium-magnesium-alumino-silicate (CMAS)-reactive thermal barrier coating including a ceramic coating; and a CMAS-reactive overlay coating, wherein the CMAS-reactive overlay coating conforms to a surface of the ceramic coating and comprises a compound that forms a stable high melting point crystalline precipitate when reacted with molten CMAS at a rate that is competitive with CMAS infiltration kinetics into the thermal barrier coating; wherein the CMAS-reactive overlay coating comprises a material selected from a group consisting of a non-rare earth oxide and a mixed non-rare earth oxide; and wherein the ceramic coating phase is chemically stable with the CMAS-reactive overlay coating.
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公开(公告)号：US20230052181A1
公开(公告)日：2023-02-16
申请号：US17401966
申请日：2021-08-13
Applicant: Raytheon Technologies Corporation
Inventor： Brian Craig , James M. Koonankeil , Brian T. Hazel , Paul E. Denney , Dominic J. Mongillo
Abstract: A manufacturing method is provided during which a preform component for a turbine engine is provided. The preform component includes a substrate and a locating feature at an exterior surface of the substrate. An outer coating is applied over the substrate. The outer coating covers the locating feature. At least a portion of the preform component and the outer coating are scanned with an imaging system to provide scan data indicative of a location of the locating feature. A cooling aperture is formed in the substrate and the outer coating based on the scan data.
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Patent Agency Ranking
公开(公告)号：US20230015977A1
公开(公告)日：2023-01-19
申请号：US17378005
申请日：2021-07-16
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor： Brian T. Hazel , Raymond Surace , Robert A. White, III , Zhongfen Ding
Abstract: A seal system includes a ceramic component, a metallic component, a coating system. The ceramic component has a first surface region that defines a first surface roughness. The metallic component is situated adjacent to the first surface region and has a second surface region facing the first surface region. The coating system includes a silicon-containing layer on the surface region of the ceramic component and barrier layer on the silicon-containing layer. The silicon containing layer has a surface in contact with the barrier layer and the barrier layer has a surface in contact with the metallic component. The surface of the barrier layer has a second surface roughness that is less than the first surface roughness. The barrier layer serves to limit interaction between silicon of the silicon-containing layer and elements of the metallic component. The barrier layer includes at least one of mullite, zircon, or hafnon.
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公开(公告)号：US20210332482A1
公开(公告)日：2021-10-28
申请号：US17241469
申请日：2021-04-27
Applicant: Raytheon Technologies Corporation
Inventor： Brian T. Hazel , Xuan Liu , Kaylan M. Wessels , Elisa M. Zaleski , Kimberly Marilurene Adams , Richard W. Jackson
Abstract: A coated substrate has a substrate and a coating system having one or more ceramic layers. At least a first layer of one of the one or more ceramic layers is a columnar layer having as-deposited columns and intercolumn gaps. The intercolumn gaps have a mean width at least one of: at least 4.0 micrometers; and at least 1.5% of a thickness of said first layer.
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公开(公告)号：US12215865B2
公开(公告)日：2025-02-04
申请号：US17714064
申请日：2022-04-05
Applicant: Raytheon Technologies Corporation
Inventor： Tianli Zhu , Richard Wesley Jackson, III , John A. Sharon , James T. Beals , Brian T. Hazel
IPC: F23R3/00
Abstract: A gas turbine engine component having a substrate; a thermal barrier coating on the substrate having a porous microstructure; and a reflective layer conforming to the porous microstructure of the thermal barrier coating, wherein the reflective layer comprises a conforming nanolaminate defined by alternating layers of platinum group metal materials selected from the group consisting of platinum group metal-based alloys, platinum group metal intermetallic compounds, mixtures of platinum group metal with metal oxides and combinations thereof. A capping layer can be added over the reflective layer. A supporting layer can be added between the reflective layer and the thermal barrier coating. A process is also disclosed.
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公开(公告)号：US20240173743A1
公开(公告)日：2024-05-30
申请号：US18071055
申请日：2022-11-29
Applicant: Raytheon Technologies Corporation
Inventor： Brian T. Hazel , Robert A. White, III , Daniel S. Rogers , John E. Holowczak
IPC: B05D3/12
CPC classification number: B05D3/12 , F01D11/00 , F05D2230/10 , F05D2230/90 , F05D2300/6033
Abstract: A method of coating a seal slot according to an exemplary embodiment of this disclosure, among other possible things includes applying a coating to a slot in a component and machining the coating to provide an open width configured to receive a seal. after the applying, the slot has an initial open width that is smaller than the open width after the machining. A method of forming a sealing assembly is also disclosed.
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公开(公告)号：US20240166890A1
公开(公告)日：2024-05-23
申请号：US17991707
申请日：2022-11-21
Applicant: Raytheon Technologies Corporation
Inventor： Richard Wesley Jackson, III , Xia Tang , James T. Beals , David A. Litton , Brian T. Hazel
Abstract: An article includes a substrate and a bond coat disposed on the substrate. The bond coat includes a matrix, a plurality of gettering particles disposed in the matrix, a plurality of diffusive particles disposed in the matrix, a radiation-absorbing component disposed in the matrix, wherein the radiation-absorbing component is concentrated at an outer surface of the bond coat. An article and a method of protecting an article are also disclosed.
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