Invention Grant
- Patent Title: Seal assembly for a gas turbine engine
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Application No.: US16356082Application Date: 2019-03-18
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Publication No.: US11248492B2Publication Date: 2022-02-15
- Inventor: Joseph H. Polly , Sean P. McGee
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D25/18
- IPC: F01D25/18 ; F01D25/16 ; F01D11/00 ; F01D25/12 ; F01D25/24 ; F02C7/20 ; F02C7/28 ; F16J15/16 ; F16J15/34 ; F16J15/447

Abstract:
A seal assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a rotatable shaft defining a longitudinal axis, and a bearing housing extending along the longitudinal axis to define a bearing compartment. The bearing housing has a first seal land defined along an inner diameter of the bearing housing, a seal carrier fixedly attached to an outer periphery of the shaft, and a seal member extending outwardly from the seal carrier. The seal member defines a plurality of helical grooves facing radially outward to establish a first sealing relationship with the first seal land, and each one of the helical grooves has a major component extending in an axial direction relative to the longitudinal axis. A method of sealing for a gas turbine engine is also disclosed.
Public/Granted literature
- US20200300117A1 SEAL ASSEMBLY FOR A GAS TURBINE ENGINE Public/Granted day:2020-09-24
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