Invention Grant
- Patent Title: Sealing assembly for a gas turbine engine
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Application No.: US16053406Application Date: 2018-08-02
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Publication No.: US10851664B2Publication Date: 2020-12-01
- Inventor: Michel Labbe , Stuart Hodgson , Daniel Poirier
- 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: F02C7/28
- IPC: F02C7/28 ; F01D11/04

Abstract:
A controlled gap radial oil sealing assembly in a gas turbine engine having a centre rotational axis defining an axial direction, the controlled gap radial sealing assembly comprises a seal element located around a cooperating seal runner and sized to define a controlled sealing gap between them, the seal runner having an axial length extending beyond an axial width of the seal element into an oiled region of the engine. A first annular surface radially outwardly spaced from and extending substantially along the axial length of the seal runner, the first annular surface sealingly cooperating with a seal housing of the seal element, and a second annular surface axially extending to overlap at least a portion of the first annular surface, the second annular surface radially outwardly spaced from the first annular surface relative to the center axis.
Public/Granted literature
- US20200040754A1 SEALING ASSEMBLY FOR A GAS TURBINE ENGINE Public/Granted day:2020-02-06
Information query
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