Turbine shroud segment feather seal located in radial shroud...

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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C416S191000

Reexamination Certificate

active

11183922

ABSTRACT:
A turbine shroud assembly is configured to adequately adjust a distribution of cooling air flow such that air leakage between radial shroud legs of adjacent shroud segments is minimized, while permitting cooling air to leak between platforms of adjacent shroud segments in order to cool sides of the platforms thereof.

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International Search Report dated Nov. 14, 2006 for corresponding PCT International Application No. PCT/CA2006/001183.

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