Turbine shroud ring

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Resilient

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Details

415139, 4151733, 415178, F01D 2526

Patent

active

060481706

ABSTRACT:
A variable diameter shroud ring (21) for the turbine of a gas turbine engine (10) comprises a support structure (25) which carries an annular array of circumferentially spaced apart ceramic segments (26). The radially outer surfaces of the segments (26) are overlaid by a plurality of circumferentially extending metallic sheets (38). The sheets (38) serve to inhibit gas leakage through gaps between the segments (26) as the diameter of the shroud ring (21) is varied.

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