Gas turbine high temperature turbine blade outer air seal...

Rotary kinetic fluid motors or pumps – Method of operation

Reexamination Certificate

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C415S139000, C415S173100, C415S178000, C415S214100

Reexamination Certificate

active

06997673

ABSTRACT:
A turbine shroud assembly includes forward and aft hangers, an axisymmetric plenum assembly, ceramic shroud segments, ceramic spacers, and forward and aft rope seals. The plenum assembly supplies impingement cooling to the shroud and the hangers. The impingement cooling to the forward and aft hangers is controlled independently to improve blade tip clearance. The rope seals are radially inward from the hangers and reduce cooling flow leakage. The turbine shroud assembly can operate in a higher temperature environment using less cooling flow than the prior art.

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