Invention Grant
- Patent Title: Seal arrangement for gas turbine engines
- Patent Title (中): 燃气涡轮发动机的密封装置
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Application No.: US13428360Application Date: 2012-03-23
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Publication No.: US08827637B2Publication Date: 2014-09-09
- Inventor: Richard Ivakitch , Andreas Eleftheriou
- Applicant: Richard Ivakitch , Andreas Eleftheriou
- Applicant Address: CA Longueuil, QC
- Assignee: Pratt & Whitney Canada Corp.
- Current Assignee: Pratt & Whitney Canada Corp.
- Current Assignee Address: CA Longueuil, QC
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F16J15/02
- IPC: F16J15/02

Abstract:
A seal arrangement for a gas turbine engine comprises a seal support having a hub portion and a peripheral rim portion. A seal member is mounted to a radially inner surface of the hub portion. A first set of circumferentially spaced-apart channel segments project from the peripheral rim portion of the seal support. A second set of circumferentially spaced-apart channel segments projects from a mating stationary structure of the gas turbine engine. The first and second sets of circumferentially spaced-apart channel segments circumferentially may be aligned to complementary form a circumferentially extending channel. A retaining ring may be mounted in the circumferentially extending channel for retaining the seal support on the mating stationary structure of the engine. The seal support may be provided with a diaphragm to provide flexibly between the seal member and the point of attachment of the seal support to the mating structure of the engine.
Public/Granted literature
- US20130249172A1 SEAL ARRANGEMENT FOR GAS TURBINE ENGINES Public/Granted day:2013-09-26
Information query
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