Invention Grant
- Patent Title: Internally cooled seal runner and method of cooling seal runner of a gas turbine engine
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Application No.: US14746246Application Date: 2015-06-22
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Publication No.: US10753219B2Publication Date: 2020-08-25
- Inventor: Michel Labbe
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F16J15/16 ; F01D25/18 ; F01D25/12 ; F02C7/28

Abstract:
The seal runner has an annular body secured to a rotating shaft of the gas turbine engine whereas ring segments are secured to a case of the gas turbine, with the seal runner having a radially-outer surface having a contacting portion adapted to rubbingly receive ring segments of the contact seal assembly during use, the seal runner having a radially-inner surface opposite to the radially-outer surface. The method includes rotating the seal runner relative to the ring segments and generating heat from the rubbing engagement therebetween; and feeding a flow of cooling fluid against the radially-inner surface to cool the seal runner from said generated heat including maintaining a pool of cooling fluid having a given depth against the radially-inner surface.
Public/Granted literature
- US20160348792A1 INTERNALLY COOLED SEAL RUNNER AND METHOD OF COOLING SEAL RUNNER OF A GAS TURBINE ENGINE Public/Granted day:2016-12-01
Information query