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公开(公告)号:US20210254719A1
公开(公告)日:2021-08-19
申请号:US16791269
申请日:2020-02-14
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Jonathan F. Zimmitti , Nasr A. Shuaib
IPC: F16J15/3284 , F02C7/28
Abstract: A seal assembly includes a housing that includes a seal flange at least partially defining a seal opening. A carbon seal is located at least partially in the seal opening and includes a first axially facing surface. The seal flange includes an axially facing surface that has a carbide based coating and a diamond-like carbon coating in engagement with the first axially facing surface on the carbon seal.
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公开(公告)号:US20210254628A1
公开(公告)日:2021-08-19
申请号:US16791298
申请日:2020-02-14
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Jonathan F. Zimmitti , Nasr A. Shuaib
Abstract: A seal assembly includes a housing at least partially defining a seal opening and at least partially surrounding a rotatable shaft. A carbon seal is located at least partially in the seal opening and includes a sealing surface. The rotatable shaft includes a radially facing surface that has a carbide based coating and a diamond-like carbon coating in engagement with the sealing surface on the carbon seal.
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公开(公告)号:US20210254486A1
公开(公告)日:2021-08-19
申请号:US16791324
申请日:2020-02-14
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Jonathan F. Zimmitti , Nasr A. Shuaib
Abstract: A seal assembly includes a carbon seal that has a sealing surface. A seal seat has a sealing surface and is positioned for rotation relative to the carbon seal. A diamond-like carbon coating at least partially forms the sealing surface on the seal seat.
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公开(公告)号:US20210079801A1
公开(公告)日:2021-03-18
申请号:US16570072
申请日:2019-09-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Pantcho P. Stoyanov , Eli N. Ross
Abstract: A seal assembly for a gas turbine engine may include a seal body coupled to an engine static structure of the gas turbine engine and a seal seat insert coupled to a radially extending portion of a shaft of the gas turbine engine. The seal body may be generally configured to be biased into contact with the seal seat insert to provide a sealing pressure between the seal body and the seal seat insert. In various embodiments, the seal seat insert is made from a ceramic material or a ceramic matrix composite.
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公开(公告)号:US20200088055A1
公开(公告)日:2020-03-19
申请号:US16574589
申请日:2019-09-18
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Mark B. Gossner
Abstract: A method for preparing a seal assembly for a gas turbine engine, comprising a seal comprising a carbon material; and a seal seat positioned for rotation relative to the seal, wherein the method comprises the steps of: pre-filming a sealing surface of the seal seat with a carbon-based tribofilm; and assembling the seal seat relative to the seal in a gas turbine engine.
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公开(公告)号:US20200056506A1
公开(公告)日:2020-02-20
申请号:US16104153
申请日:2018-08-17
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Mark B. Gossner
Abstract: A rotor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a rotor that has a hub carrying one or more rotatable blades. The rotor is mechanically attached to a shaft, and an annular seal is carried by the shaft. The annular seal includes a substrate and a first layer disposed on the substrate. The first layer includes copper, and a second layer is disposed on the first layer and arranged to establish a sealing relationship with the rotor. The second layer includes a solid lubricant. A method of sealing is also disclosed.
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公开(公告)号:US20180361471A1
公开(公告)日:2018-12-20
申请号:US15417873
申请日:2017-01-27
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Christopher W. Strock , Thomas J. Watson
CPC classification number: B22F1/0059 , B22F2301/052 , B22F2301/15 , B22F2301/205 , B22F2303/01 , B22F2303/05 , B22F2999/00 , C23C4/06 , C23C24/04 , F01D5/288 , F05D2230/90 , F05D2300/611
Abstract: A coated article comprising: a substrate; and a coating on the substrate comprising: a metallic matrix comprising, by weight: Al as a largest constituent; 3.0-6.0 Cr; 1.5-4.0 Mn; 0.1-3.5 Co; and 0.3-2.0 Zr; and a filler and optionally porosity.
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