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公开(公告)号：US20210146433A1
公开(公告)日：2021-05-20
申请号：US17095201
申请日：2020-11-11
Inventor： Quinlan Yee Shuck , Scott Nelson , Raymond Ruiwen Xu , Brandon David Ribic , Matthew R. Gold
IPC: B22F3/00 , B33Y10/00 , B33Y30/00 , B33Y50/02 , B33Y70/10 , B33Y80/00 , B29C64/112 , B29C64/393 , C22C19/05 , C22C30/02
Abstract: An additive manufacturing technique may include depositing, via a filament delivery device, a filament onto a surface of a substrate. The filament includes a binder and a powder including at least one metal or alloy and at least one braze alloy. The technique also includes sacrificing the binder to form a preform. The technique also includes sintering the preform to form a component including the at least one metal or alloy and the at least one braze alloy.
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公开(公告)号：US20210024424A1
公开(公告)日：2021-01-28
申请号：US16522524
申请日：2019-07-25
Applicant: Rolls-Royce Corporation
Inventor： Li Li , Jun Shi , Scott Nelson , Taylor K. Blair
IPC: C04B35/622 , B05D1/38 , B05D3/12 , C04B35/16
Abstract: An example article includes a substrate and a barrier coating on the substrate extending from an inner interface facing the substrate to an outer surface opposite the inner interface. The barrier coating includes a bulk matrix and a plurality of discrete plugs inset within the bulk matrix and dispersed across the outer surface of the barrier coating. An example technique includes forming the barrier coating on the substrate of a component.
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公开(公告)号：US20200254548A1
公开(公告)日：2020-08-13
申请号：US16272664
申请日：2019-02-11
Applicant: Rolls-Royce Corporation
Inventor： Raymond Ruiwen Xu , Scott Nelson , Joseph Peter Henderkott
Abstract: A method may include removing a portion of a base component adjacent to a damaged portion of the base component to define a repair portion of the base component. The base component may include a cobalt- or nickel-based superalloy, and the repair portion of the base component may include a through-hole extending from a first surface of the base component to a second surface of the base component. The method also may include forming a braze sintered preform to substantially reproduce a shape of the through-hole. The braze sintered preform may include a Ni- or Co-based alloy. The method additionally may include placing the braze sintered preform in the through-hole and heating at least the braze sintered preform to cause the braze sintered preform to join to the repair portion of the base component and change a microstructure of the braze sintered preform to a brazed and diffused microstructure.
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公开(公告)号：US20190255732A1
公开(公告)日：2019-08-22
申请号：US16278265
申请日：2019-02-18
Inventor： Scott Nelson , Quinlan Shuck , Sean Landwehr , Sungbo Shim
IPC: B28B1/00 , B29C64/165 , B33Y10/00 , B33Y40/00 , C04B35/80 , C04B35/622 , C04B35/628 , C04B35/657
Abstract: A system and method for forming a porous ceramic preform is provided. The method may include forming a stacked powder structure including a binder layer and a powder layer on the binder layer. The binder layer may be formed by depositing a binder with a spray nozzle on a substrate. The powder layer may be formed by depositing a powder on the binder layer. The porous ceramic preform may be formed by heating the stacked powder structure to pyrolyze the binder. The porous ceramic preform is configured to be infiltrated by a molten material. The substrate may comprise a ceramic fiber preform. After melt infiltration of the porous ceramic preform and the ceramic fiber preform, a densified ceramic feature having a predetermined geometry may be formed on a ceramic matrix composite (CMC) component.
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公开(公告)号：US20190224912A1
公开(公告)日：2019-07-25
申请号：US16255102
申请日：2019-01-23
Inventor： Quinlan Yee Shuck , Scott Nelson , Brandon David Ribic , Matthew R. Gold
IPC: B29C64/135 , B29C64/118 , B29C64/393 , B33Y10/00 , B33Y30/00 , B33Y50/02
Abstract: An additive manufacturing assembly may include a surface-modified component to be incorporated into an additively manufactured component by adhering the at least one component to the additively manufactured component during an additive manufacturing technique. The surface-modified component includes a modified surface that is modified to have increased adhesion to the additively manufactured component. The additive manufacturing assembly also includes means for additively forming layers of material using the additive manufacturing technique and a computing device, the computing device is configured to control the means for additively forming layers to form a layer of material on the surface of the surface-modified component and control the means for additively forming layers to form, on the layer of material, at least one additional layer of material to form the additively manufactured component incorporating the surface-modified component.
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Patent Agency Ranking
公开(公告)号：US20190031570A1
公开(公告)日：2019-01-31
申请号：US15951707
申请日：2018-04-12
Inventor： Scott Nelson , Raymond Xu , Sean Landwehr , Juan Wei , Stephen Liu , Juan Carlos Madeni
Abstract: A braze alloy for joining or repairing ceramic matrix composite (CMC) components comprises a braze composition including silicon at a concentration from about 48 at. % to about 66 at. %, titanium at a concentration from about 1 at. % to about 35 at. %, and an additional element selected from aluminum, cobalt, vanadium, nickel, and chromium. The braze composition comprises a melting temperature of less than 1300° C.
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公开(公告)号：US20170121232A1
公开(公告)日：2017-05-04
申请号：US15273095
申请日：2016-09-22
Applicant: Rolls-Royce Corporation
Inventor： Scott Nelson , Raymond J. Sinatra , Sean E. Landwehr , Mike R. Dunkin , Ashley Moretti
IPC: C04B41/85 , C23C4/134 , C23C14/22 , C04B41/91 , B05D1/18 , B05D1/02 , C04B35/565 , C23C4/12 , C23C16/44
CPC classification number: C04B41/85 , B05D1/02 , B05D1/18 , C04B35/565 , C04B41/009 , C04B41/50 , C04B41/91 , C23C4/12 , C23C4/134 , C23C14/22 , C23C16/44 , F01D5/282 , F01D5/288 , F05D2300/2261 , C04B35/806 , C04B41/0036 , C04B41/53
Abstract: In some examples, the disclosure describes an article and a method of making the same that includes a substrate including a ceramic or a ceramic matrix composite including silicon carbide, where the substrate defines an outer substrate surface and a plurality of grooves formed in the outer substrate surface, where each respective groove of the plurality of grooves exhibits an anchor tooth that spans an edge of the respective groove, and where the plurality of grooves define an average groove width less than about 20 micrometers, and a coating formed on the outer surface of the substrate, where the coating at least partially fills the plurality of grooves of the substrate.
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公开(公告)号：US20160325368A1
公开(公告)日：2016-11-10
申请号：US15144367
申请日：2016-05-02
Applicant: Rolls-Royce Corporation
Inventor： Sean E. Landwehr , Scott Nelson , Jacque Sue Bader
CPC classification number: B23K1/19 , B23K1/002 , B23K1/0056 , B23K3/0607 , B23K35/0244 , B23K35/30 , B23K35/3612 , B23K35/3613 , B23K2103/52
Abstract: The disclosure describes techniques for joining a first part including a ceramic or a CMC and a second part including a ceramic or a CMC using brazing. A technique may include positioning a filler material in a joint region between the first and second parts and a metal or alloy on a bulk surface of the filler material. The metal or alloy may be locally heated to melt the metal or alloy, which may infiltrate the filler material. A constituent of the molten metal or alloy may react with a constituent of the filler material to join the first and second parts. Another technique may include depositing a powder that includes the filler material and the metal or alloy in the joint region. Substantially simultaneously with depositing the powder, the powder may be locally heated. A constituent of the molten metal or alloy may react with a constituent of the filler material to join the first and second parts.
Abstract translation: 本公开描述了使用钎焊将包括陶瓷或CMC的第一部分和包括陶瓷或CMC的第二部分接合的技术。 技术可以包括将填充材料定位在第一和第二部分之间的接合区域中，以及在填料材料的整体表面上的金属或合金。 金属或合金可以局部加热以熔化可能渗透填料的金属或合金。 熔融金属或合金的成分可与填料的成分反应，从而使第一和第二部分接合。 另一种技术可以包括在接合区域中沉积包括填充材料和金属或合金的粉末。 基本上同时沉积粉末，粉末可以局部加热。 熔融金属或合金的成分可与填料的成分反应，从而使第一和第二部分接合。
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公开(公告)号：US12293527B2
公开(公告)日：2025-05-06
申请号：US17932962
申请日：2022-09-16
Applicant: Rolls-Royce Corporation
Inventor： Scott Nelson , Baily Thomas , Abdalla R. Nassar , Jason Scherer , John Grubbs
Abstract: A powder flow monitoring system may include a computing device configured to receive image data representing illuminated powder of a powder stream between a powder delivery device and a build surface of a component, generate a representation of the powder stream based on the image data, and output the representation of the powder stream for display at a display device.
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公开(公告)号：US11707788B2
公开(公告)日：2023-07-25
申请号：US17098019
申请日：2020-11-13
Inventor： Quinlan Yee Shuck , Scott Nelson , Raymond Ruiwen Xu , Brandon David Ribic , Matthew R. Gold
IPC: B22F10/18 , B33Y10/00 , B29C64/165 , B29C64/393 , B22F10/85 , F16L59/065 , B33Y50/02 , B29K505/00 , B33Y80/00 , B33Y30/00
CPC classification number: B33Y80/00 , B22F10/18 , B22F10/85 , B29C64/165 , B29C64/393 , B33Y10/00 , B33Y30/00 , B33Y50/02 , F16L59/065 , B29K2505/00 , B22F2998/10 , B22F1/10 , B22F10/18 , B22F3/1021
Abstract: In some examples, an additive manufacturing technique for forming a vacuum insulator. For example, a method including forming an article including a first layer, a second layer, and at least one support member extending between the first and second layer by depositing a filament via a filament delivery device, wherein the filament includes a sacrificial binder and a powder, and wherein the first layer, second layer, and at least one support member define an open cavity within the article; removing the binder; and sintering the article to form the vacuum insulator, wherein the vacuum insulator defines a vacuum environment in the cavity.
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