Casing ring

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

Reexamination Certificate

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Details

C415S173500, C415S173600, C415S178000, C415S209200, C415S209300

Reexamination Certificate

active

06966752

ABSTRACT:
A jacket ring for the low-pressure-turbine region of a gas turbine, having a plurality of lined-up segments which are arranged between a moving blade ring with a shroud band and the casing of the gas turbine, which carry a run-in lining and which hold guide blades in a positive-locking manner, wherein each segment comprises a hot-gas-side seal carrier and a casing-side securing element, the seal carrier and the securing element are at the greatest possible distance from one another and only have common contact points which are as small as possible, and the securing element is axially supported directly on the casing of the gas turbine.

REFERENCES:
patent: 4242042 (1980-12-01), Schwarz
patent: 4512712 (1985-04-01), Baran, Jr.
patent: 4867639 (1989-09-01), Strangman
patent: 4925365 (1990-05-01), Crozet et al.
patent: 5240518 (1993-08-01), Linko, III et al.
patent: 0 618 349 (1994-10-01), None
patent: 0 844 369 (1998-05-01), None
patent: 0 974 734 (2000-01-01), None

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