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公开(公告)号:US11220923B2
公开(公告)日:2022-01-11
申请号:US16384488
申请日:2019-04-15
Applicant: United Technologies Corporation
Inventor: Paul M. Lutjen , Jeremy Drake , Timothy M. Davis
Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and second seal sections away from one another.
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公开(公告)号:US10260364B2
公开(公告)日:2019-04-16
申请号:US14642040
申请日:2015-03-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Paul M. Lutjen , Jeremy Drake , Timothy M. Davis
Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and second seal sections away from one another.
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公开(公告)号:US09920869B2
公开(公告)日:2018-03-20
申请号:US14708825
申请日:2015-05-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Timothy M Davis , Jeremy Drake
IPC: F16L37/00 , F16L37/086 , F16L21/02 , F01D9/06 , F01D25/24
CPC classification number: F16L37/086 , F01D9/065 , F01D25/24 , F16L21/02
Abstract: A transfer tube includes a conduit with an inlet and an opposed outlet. The transfer tube also includes a retention tab extending from the inlet and a locking spring tab extending from the outlet. The locking spring tab includes a claw portion extending radially from the locking spring tab of the transfer tube.
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公开(公告)号:US20170298776A1
公开(公告)日:2017-10-19
申请号:US15099755
申请日:2016-04-15
Applicant: United Technologies Corporation
Inventor: Daniel S. Rogers , Jeremy Drake , Brian C. McLaughlin
CPC classification number: F01D25/28 , F01D11/08 , F01D25/24 , F01D25/246 , F05D2220/32 , F05D2230/64 , F05D2230/70 , F05D2230/72 , F05D2230/80 , F05D2240/11 , F05D2260/30
Abstract: A retention member for a component of a gas turbine engine and methods of using the same are provided. The retention member includes an annular body having a first side, a second side, a first end, and a second end, a retention element configured at the first end of the annular body and on the first side, the retention element configured to releasably engage with an interior surface of a case of the gas turbine engine, and a support element configured at the second end of the annular body, the support element configured to engage with a surface of at least one of a blade outer air seal or a blade outer air seal support.
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公开(公告)号:US20170292609A1
公开(公告)日:2017-10-12
申请号:US15092793
申请日:2016-04-07
Applicant: United Technologies Corporation
Inventor: Jeremy Drake , Raymond Surace
IPC: F16J15/3288 , F01D11/00 , F04D29/08 , F01D11/12
Abstract: Aspects of the disclosure are directed to a brush seal comprising: a first plate, a wire mesh adjacent the first plate, a bristle pack adjacent the wire mesh, and a second plate adjacent the bristle pack. Aspects of the disclosure are directed to a method comprising: positioning a wire mesh adjacent to a first plate, positioning a bristle pack adjacent to the wire mesh, positioning a second plate adjacent to the bristle pack, applying a toolset to hold the first plate, the wire mesh, the bristle pack, and the second plate in a stack-up, and performing an operation to form a brush seal from the stack-up of the first plate, the wire mesh, the bristle pack, and the second plate.
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