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公开(公告)号:US12030822B2
公开(公告)日:2024-07-09
申请号:US16859827
申请日:2020-04-27
Applicant: Raytheon Technologies Corporation
Inventor: Olivier H. Sudre , Richard Wesley Jackson , Xuan Liu
CPC classification number: C04B41/5057 , C04B41/009 , C04B41/4539 , C04B41/4582 , C04B41/5024 , C04B41/522 , C04B41/87 , C04B41/89 , F01D5/284 , F01D5/288 , F01D25/005 , F05D2240/11 , F05D2240/35 , F05D2240/55 , F05D2300/222 , F05D2300/2261 , Y10T428/31504
Abstract: An article includes a ceramic-based substrate and a barrier layer on the ceramic-based substrate. The barrier layer includes a matrix, diffusive particles, and gettering particles. The gettering particles include at least one of non-gas-evolving particles and porous particles. An article and a method are also disclosed.
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公开(公告)号:US20230250727A1
公开(公告)日:2023-08-10
申请号:US18123526
申请日:2023-03-20
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Richard Wesley Jackson , Adam P. Generale , Xuan Liu , Mark F. Zelesky
IPC: F01D5/28
CPC classification number: F01D5/288 , F01D5/284 , F05D2300/6033 , F05D2300/611 , F05D2300/30 , F05D2300/6111 , F05D2300/21 , F05D2240/306 , F05D2240/305 , F05D2300/222 , F05D2300/15 , F05D2220/32
Abstract: An airfoil includes an airfoil wall that defines a leading end, a trailing end, and suction and pressure sides that join the leading end and the trailing end. The airfoil wall is formed of a silicon-containing ceramic. A first environmental barrier topcoat is disposed on the suction side of the airfoil wall, and a second, different environmental barrier topcoat is disposed on the pressure side of the airfoil wall. The first topcoat is vaporization-resistant and the second topcoat is resistant to calcium-magnesium-aluminosilicate.
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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:US20230278935A1
公开(公告)日:2023-09-07
申请号:US18138395
申请日:2023-04-24
Applicant: Raytheon Technologies Corporation
Inventor: Richard Wesley Jackson , James T. Beals , Xia Tang , Xuan Liu , David A. Litton , Brian T. Hazel
CPC classification number: C04B41/4527 , C04B41/5071 , C04B41/52
Abstract: A coated article including an article having a surface; an oxidation resistant bond coat layer deposited on the surface, the oxidation resistant bond coat layer comprising a metal silicide phase, a crystalline ceramic phase and an amorphous ceramic phase, wherein the metal silicide phase has an aspect ratio greater than 1:1 but less than 50:1.
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公开(公告)号:US20230241699A1
公开(公告)日:2023-08-03
申请号:US18152482
申请日:2023-01-10
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Nicholas M. LoRicco , Xuan Liu
IPC: B23H7/24
CPC classification number: B23H7/24
Abstract: An electrode includes a metallic electrode body that has a surface region that is enriched in at least one of aluminum or chromium. The aluminum and/or chromium that is vaporized from the surface region suppresses vaporization loss of aluminum or chromium from the machined surface of the metallic workpiece during electric discharge machining.
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6.
公开(公告)号:US20230044705A1
公开(公告)日:2023-02-09
申请号:US17395992
申请日:2021-08-06
Applicant: Raytheon Technologies Corporation
Inventor: Richard Wesley Jackson , James T. Beals , Xia Tang , Xuan Liu , David A. Litton , Brian T. Hazel
Abstract: A coated article including an article having a surface; an oxidation resistant bond coat layer deposited on the surface, the oxidation resistant bond coat layer comprising a metal silicide phase, a crystalline ceramic phase and an amorphous ceramic phase, wherein the metal silicide phase has an aspect ratio greater than 1:1 but less than 50:1.
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公开(公告)号:US20210277511A1
公开(公告)日:2021-09-09
申请号:US17172505
申请日:2021-02-10
Applicant: Raytheon Technologies Corporation
Inventor: Xuan Liu , Brian T. Hazel
Abstract: A method of treating a component for a gas turbine engine according to an example of the present disclosure includes, among other things, injecting a suspension stream into a plasma gas stream, the suspension stream having coating particles moving in the gas stream toward a component, and placing the coating particles on the component at a coating location to form a top coat that has a columnar microstructure such that a porosity of the columnar microstructure is between 4.0-7.0 percent, exclusive of the intersegment gaps.
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公开(公告)号:US12044146B2
公开(公告)日:2024-07-23
申请号:US18123526
申请日:2023-03-20
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Richard Wesley Jackson , Adam P. Generale , Xuan Liu , Mark F. Zelesky
IPC: F01D5/28
CPC classification number: F01D5/288 , F01D5/284 , F05D2220/32 , F05D2240/305 , F05D2240/306 , F05D2300/15 , F05D2300/21 , F05D2300/222 , F05D2300/30 , F05D2300/6033 , F05D2300/611 , F05D2300/6111
Abstract: An airfoil includes an airfoil wall that defines a leading end, a trailing end, and suction and pressure sides that join the leading end and the trailing end. The airfoil wall is formed of a silicon-containing ceramic. A first environmental barrier topcoat is disposed on the suction side of the airfoil wall, and a second, different environmental barrier topcoat is disposed on the pressure side of the airfoil wall. The first topcoat is vaporization-resistant and the second topcoat is resistant to calcium-magnesium-aluminosilicate.
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公开(公告)号:US11821337B1
公开(公告)日:2023-11-21
申请号:US17882180
申请日:2022-08-05
Applicant: Raytheon Technologies Corporation
Inventor: Rafael A. Perez Reisler , Andy Turko , Xuan Liu , Danielle E. Jencks , Glenn A. Cotnoir , Russell F. Croft
IPC: F01D5/28
CPC classification number: F01D5/288 , F05D2220/32 , F05D2230/10 , F05D2230/30 , F05D2230/314 , F05D2230/90 , F05D2300/611
Abstract: A gas turbine engine component includes a substrate having first surface and a second surface disposed opposite the first surface, a plurality of holes extending through the substrate from the first surface to the second surface, the holes defined by a plurality of respective walls each extending from the first surface to the second surface, a metallic bond coat disposed on the first surface, and an aluminide coating disposed on the first surface, the second surface, and the walls. The metallic bond coat is disposed between the first surface and the aluminide coating and the walls are free of the metallic bond coat.
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公开(公告)号:US11719105B2
公开(公告)日:2023-08-08
申请号:US17172746
申请日:2021-02-10
Applicant: Raytheon Technologies Corporation
Inventor: Michael N. Task , Xuan Liu , Russell A. Beers , Kevin W. Schlichting
CPC classification number: F01D5/288 , C23C2/04 , C23C10/08 , C23C10/24 , C23C16/045 , C23C16/06 , C23C28/021 , F01D5/187 , F05D2220/32 , F05D2230/90 , F05D2300/132 , F05D2300/611
Abstract: A method of coating a component including aluminizing an array of internal passageways within the component; and chromizing a portion of the array of internal passageways within the component. A component, including an airfoil having an array of aluminized internal passageways, the array of aluminized internal passageways chromized up to a demarcation.
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