Invention Grant
- Patent Title: Fluid-cooled seal arrangement for a gas turbine engine
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Application No.: US16127524Application Date: 2018-09-11
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Publication No.: US11066955B2Publication Date: 2021-07-20
- Inventor: Garth J. Vdoviak, Jr. , Gary L. Grogg
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F01D25/18
- IPC: F01D25/18 ; F16J15/16 ; F01D25/12 ; F02C7/28 ; F04D29/059 ; F04D29/063 ; F04D29/12 ; F04D29/32 ; F02C7/06 ; F16C33/66 ; F16C19/26
Abstract:
A component for a gas turbine engine includes a compartment housing that redirects oil from at least one passage in a rotational component onto a backside of a seal land.
Public/Granted literature
- US20190017414A1 FLUID-COOLED SEAL ARRANGEMENT FOR A GAS TURBINE ENGINE Public/Granted day:2019-01-17
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