Turbine shroud thermal distortion control

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

Reexamination Certificate

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Details

C415S177000, C415S116000

Reexamination Certificate

active

07665960

ABSTRACT:
A shroud suitable for use in a gas turbine engine exhibits substantially uniform thermal growth.

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