Isolated turbine shroud

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

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Details

415177, 415178, F01D 1118

Patent

active

055624081

ABSTRACT:
A turbine shroud includes an annular shroud support joined to an annular outer casing and spaced radially inwardly therefrom to define an annular flow duct for receiving compressor bleed air. A plurality of shroud panels are joined to the shroud support and have a radially inner surface positionable radially above turbine rotor blades to define a tip clearance therebetween. An isolation shield is joined to the shroud support radially above the panels and includes a plurality of open-ended cells facing radially outwardly in the duct toward the outer casing for inducing drag in the bleed air flowable axially through the duct to thermally isolate the shroud support from the bleed air for controlling the tip clearance.

REFERENCES:
patent: 4101242 (1978-07-01), Coplin et al.
patent: 4303371 (1981-12-01), Eckert
patent: 4543039 (1985-09-01), Ruis et al.
patent: 4573866 (1986-03-01), Sandy, Jr. et al.
patent: 5165848 (1992-11-01), Plemmons
patent: 5169287 (1992-12-01), Proctor et al.
patent: 5174714 (1992-12-01), Plemmons et al.
patent: 5176495 (1993-01-01), Honkomp et al.
patent: 5195868 (1993-03-01), Plemmons et al.
patent: 5238365 (1993-08-01), Petsche
General Electric Company, CF34-3A1 gas turbine engine in production more than 1 year; 3 figures showing high pressure turbine shrouds and unpublished proposed temporary fix.

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