EP1512841A3

Methods and apparatus to reduce seal rubbing within gas turbine engines

Abstract

A seal assembly for a gas turbine engine (10) includes a first stage disk (30) and a second stage disk (32), a disk retainer (53), and an interstage seal assembly (50) extending between the first and second stage disks. The interstage seal assembly includes a radially outer shell (54) extending radially outwardly from a web portion (58). The outer shell includes an upstream arm (60) and a downstream arm (62) extending outwardly from the outer shell, the disk retainer between the outer shell upstream arm and the first stage disk, the downstream arm coupled to the second stage disk.

EP1512841A3, drawing sheet 1
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Term ended

Projected expiry passed 1 September 2024, 2.1 years ago.

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