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公开(公告)号:US11732372B2
公开(公告)日:2023-08-22
申请号:US16538493
申请日:2019-08-12
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Timothy A. Weers
IPC: C25D1/00 , C22C38/40 , F01D5/28 , C22C19/05 , G01V1/00 , C25D3/66 , C25D3/56 , G01S19/14 , G01V1/26 , C22C38/18 , C22C38/58
CPC classification number: C25D1/00 , C22C19/05 , C22C38/40 , C25D3/56 , C25D3/562 , C25D3/66 , C25D3/665 , F01D5/28 , G01S19/14 , G01V1/003 , C22C38/18 , C22C38/58 , F05D2300/132 , F05D2300/17 , G01V1/26
Abstract: An article comprising a turbine component formed of a nickel-chromium (Ni—Cr) alloy including from 2 to 50 wt % chromium balanced by nickel is disclosed. The Ni—Cr alloy is thicker than at least 125 μm to make a self-supporting turbine component, and the turbine component includes a rotor blade, a stator, or a vane. The Ni—Cr alloy is electroformed on a mandrel by providing an external supply of current to an anode and a cathode in a plating bath containing a solvent, a surfactant, and an ionic liquid including choline chloride, nickel chloride, and chromium chloride.
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公开(公告)号:US20200347506A1
公开(公告)日:2020-11-05
申请号:US16927417
申请日:2020-07-13
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Lesia V. Protsailo , Michael N. Task
IPC: C25D5/12 , C25D7/00 , C25D5/50 , C23C18/50 , C23C18/16 , F01D5/18 , C23C18/32 , C22C27/06 , C25D3/56 , C25D5/16 , C25D5/18
Abstract: Disclosed herein is a method of coating, comprising providing an article having an internal passage therein to be coated; electrolytically applying a first layer that comprises chromium or a chromium alloy onto a surface of the internal passage; electrolytically applying a second layer comprising aluminum or an aluminum alloy onto the first layer; and heat treating the article to promote interdiffusion between the first layer and the second layer.
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公开(公告)号:US20230139403A1
公开(公告)日:2023-05-04
申请号:US18089081
申请日:2022-12-27
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Poulomi Sannigrahi
Abstract: A coated steel substrate has a steel substrate having a surface. A coating layer is atop the surface. The coating layer includes: aluminum activated by indium; and a ceramic binder. The coating also may comprise of multiple layers with different properties to facilitate the galvanic protection capability.
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公开(公告)号:US11572626B2
公开(公告)日:2023-02-07
申请号:US17021304
申请日:2020-09-15
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Poulomi Sannigrahi
Abstract: A coated steel substrate has a steel substrate having a surface. A coating layer is atop the surface. The coating layer includes: aluminum activated by indium; and a ceramic binder. The coating also may comprise of multiple layers with different properties to facilitate the galvanic protection capability.
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公开(公告)号:US20220127745A1
公开(公告)日:2022-04-28
申请号:US17077181
申请日:2020-10-22
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , James O. Hansen
Abstract: A sealing process includes impregnating an oxide layer of an anodized metal with a corrosion inhibitor by contacting the oxide layer with a first corrosion inhibitor solution at a first temperature and sealing the impregnated oxide layer of an anodized metal by contacting the impregnated oxide layer with a second corrosion inhibitor solution at a second temperature, wherein the first corrosion inhibitor solution has a corrosion inhibitor concentration greater than the second corrosion inhibitor solution and the first temperature is less than the second temperature.
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公开(公告)号:US20220154361A1
公开(公告)日:2022-05-19
申请号:US17097614
申请日:2020-11-13
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Mimi Nguyen-Vu
Abstract: Disclosed are methods of anodizing a metal component. In the methods an anodization bath includes an organic acid.
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公开(公告)号:US20220154350A1
公开(公告)日:2022-05-19
申请号:US17097736
申请日:2020-11-13
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Weilong Zhang
Abstract: Disclosed is a method of providing corrosion protection to an anodized metal including providing a metal having an anodization layer wherein the anodization layer includes a barrier portion; contacting the anodization layer with a first solution at a first temperature to seal the barrier portion; and contacting the anodization layer with the sealed barrier portion with a second solution at a second temperature to deposit a precipitated rare earth compound in the anodization layer with the sealed barrier portion; wherein the first solution includes a transition metal oxyanion and has a pH of 3 to 6 and the second solution includes a trivalent rare earth cation.
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公开(公告)号:US20210164107A1
公开(公告)日:2021-06-03
申请号:US17021304
申请日:2020-09-15
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Poulomi Sannigrahi
Abstract: A coated steel substrate has a steel substrate having a surface. A coating layer is atop the surface. The coating layer includes: aluminum activated by indium; and a ceramic binder. The coating also may comprise of multiple layers with different properties to facilitate the galvanic protection capability.
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公开(公告)号:US20200291780A1
公开(公告)日:2020-09-17
申请号:US16889281
申请日:2020-06-01
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , William J. Brindley , Monika D. Kinstler
IPC: F01D5/00 , C25D7/00 , C25D3/56 , C25D5/12 , C25D5/18 , C25D5/50 , C25D17/10 , F01D5/28 , C25D3/66 , C22C19/05 , C22F1/10 , F01D9/02
Abstract: An cicctrodcposited nickel-chromium-aluminum (Ni—Cr—Al) composite including nickel- chromium alloy and aluminum, and alloys or compounds formed by Al, Cr and Ni applied on turbine components comprises from 2 to 50 wt % chromium, from 0.1 to 6 wt % aluminum, and a remaining balance of nickel, wherein the Ni—Cr—Al composite is heat-treated to form an aluminum compound and to restore materials lost during repair processes of the turbine components.
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公开(公告)号:US20200291797A1
公开(公告)日:2020-09-17
申请号:US16889248
申请日:2020-06-01
Applicant: Raytheon Technologies Corporation
Inventor: Lei Chen , Zhiwei Yang , William J. Brindley , Monika D. Kinstler , Bruce R. Saxton
IPC: F01D5/28 , C25D5/50 , C25D3/66 , C25D3/56 , C22C19/05 , C25D3/12 , C25D5/40 , C25D7/00 , F01D9/02 , F01D25/00
Abstract: A nickel-chromium (Ni—Cr) alloy and a method for electrodepositing the Ni—Cr alloy on a turbine engine component for dimensionally restoring the engine component are described. The engine component is restored by rebuilding wall thickness with the Ni—Cr alloy including from 2 to 50 wt % chromium balanced with nickel. The turbine component coated with the Ni—Cr alloy is heat-treated at a high temperature to homogenize composition of the alloy to mimic the base alloy and to restore materials lost during repair of the turbine component.
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