Turbine shroud hanger

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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415138, F01D 1118

Patent

active

055932762

ABSTRACT:
A turbine shroud hanger is supported from an annular outer casing and includes an annular radial flange and integral forward and aft legs at a radially inner end thereof. The legs extend axially oppositely to each other and include respective distal ends configured for supporting a plurality of arcuate shroud panels radially above a plurality of turbine rotor blades to define a tip clearance therebetween. The legs include circumferentially spaced apart forward and aft slots extending axially from the distal ends thereof toward the radial flange, and completely radially therethrough to bifurcate the legs into circumferential segments for reducing transient thermal expansion of the hanger to reduce in turn expansion of the tip clearance.

REFERENCES:
patent: 4101242 (1978-07-01), Coplin et al.
patent: 4303371 (1981-12-01), Eckert
patent: 4573866 (1986-03-01), Sandy, Jr. et al.
patent: 4627233 (1986-12-01), Baran, Jr.
patent: 4756153 (1988-07-01), Roberts et al.
patent: 4897021 (1990-01-01), Chaplin et al.
patent: 5071313 (1991-12-01), Nichols
patent: 5169287 (1992-12-01), Proctor et al.
patent: 5174714 (1992-12-01), Plemmons et al.
patent: 5181826 (1993-01-01), Rock
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CF34-3A1 gas turbine engine in production more than 1 year; 3 figures showing high pressure turbine shrouds and unpublished proposed temporary fix.

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