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公开(公告)号:US20190160528A1
公开(公告)日:2019-05-30
申请号:US15822443
申请日:2017-11-27
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor: Randolph Carlton McGee , Ying She , Aaron T. Nardi
IPC: B22F1/00 , C22C14/00 , B22F3/14 , B22F3/22 , B23K26/342
Abstract: An example method of modifying a powder according to the present disclosure includes contacting a powder comprising particles with a nitrogen-containing gas and improved flowability of the powder. A method of providing a powder and a reactor are also disclosed.
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公开(公告)号:US20230116899A1
公开(公告)日:2023-04-13
申请号:US17850237
申请日:2022-06-27
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor: Randolph Carlton McGee , Ying She , Aaron T. Nardi
Abstract: An example method of modifying a powder according to the present disclosure includes contacting a powder comprising particles with a nitrogen-containing gas and improved flowability of the powder. A method of providing a powder and a reactor are also disclosed.
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公开(公告)号:US10702939B2
公开(公告)日:2020-07-07
申请号:US15945855
申请日:2018-04-05
Applicant: Hamilton Sundstrand Corporation
Inventor: Lawrence Binek , Aaron T. Nardi , John A. Ferro , Matthew William Miller , Raffi O. Mangoyan , Timothy E. Mandel, Jr.
Abstract: Aspects include supplying a plurality of nickel-enriched braze powder particles to a cold spray system through a particle supply inlet. The nickel-enriched braze powder particles are accelerated through a transfer tube and out an exit in the transfer tube towards a substrate to produce a braze cold-sprayed substrate. A component surface is positioned proximate to the braze cold-sprayed substrate. The braze cold-sprayed substrate is heated to bond the braze cold-sprayed substrate to the component surface.
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公开(公告)号:US20190308266A1
公开(公告)日:2019-10-10
申请号:US15945855
申请日:2018-04-05
Applicant: Hamilton Sundstrand Corporation
Inventor: Lawrence Binek , Aaron T. Nardi , John A. Ferro , Matthew William Miller , Raffi O. Mangoyan , Timothy E. Mandel, JR.
Abstract: Aspects include supplying a plurality of nickel-enriched braze powder particles to a cold spray system through a particle supply inlet. The nickel-enriched braze powder particles are accelerated through a transfer tube and out an exit in the transfer tube towards a substrate to produce a braze cold-sprayed substrate. A component surface is positioned proximate to the braze cold-sprayed substrate. The braze cold-sprayed substrate is heated to bond the braze cold-sprayed substrate to the component surface.
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5.
公开(公告)号:US20160298780A1
公开(公告)日:2016-10-13
申请号:US15185188
申请日:2016-06-17
Applicant: Hamilton Sundstrand Corporation
Inventor: Kevin M. Rankin , Blair A. Smith , Timothy R. Boysen , Aaron T. Nardi , Keith J. Brooky
CPC classification number: F16K25/005 , B64D13/00 , C23C4/18 , C23C24/106 , F16K1/22
Abstract: A disclosed method of hard coating a wear surface of a valve of an aircraft air management system is performed by depositing a hardface alloy powder onto the wear surface, heating the wear surface and the hardface alloy powder to transform the hardface alloy powder into a molten liquid mass, and subsequently cooling the molten liquid hardface alloy mass to solidify the hardface alloy onto the wear surface. The disclosed process provides for localized application and subsequent bonding of the hardface alloy to discrete portions of the wear surface. The solidified hardface alloy coating may then be machined to obtain specific wear surface geometries.
Abstract translation: 通过将硬质合金粉末沉积在磨损表面上,加热磨损表面和硬质合金粉末以将硬质合金粉末转变成熔融液体,从而实现了对飞机空气管理系统的阀的耐磨面进行硬涂覆的公开的方法 然后冷却熔融液体硬质合金质量以将硬质合金固化在磨损表面上。 所公开的方法提供了局部应用和随后将硬质合金粘合到磨损表面的离散部分上。 然后可以加工固化的硬质合金涂层以获得特定的磨损表面几何形状。
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公开(公告)号:US20170343113A1
公开(公告)日:2017-11-30
申请号:US15678317
申请日:2017-08-16
Applicant: Hamilton Sundstrand Corporation
Inventor: Peter J. Dowd , John M. Dehais , Blair A. Smith , Timothy R. Boysen , Keith J. Brooky , Aaron T. Nardi , Kevin M. Rankin
CPC classification number: F16K1/225 , F16K1/22 , F16K27/0218 , Y10T29/49412
Abstract: A thrust plate for a butterfly valve includes a thrust plate body that defines a recess that extends between a bottom thrust surface, side walls, and an open top. There is a nickel-based or cobalt-based wear-resistant coating located on the bottom thrust surface. The wear-resistant coating is harder than the thrust plate body.
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