SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD
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United States of America Patent
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Issued Date -
May 16, 2024
app pub date -
Jun 30, 2023
filing date -
Nov 16, 2022
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Abstract
The present application provides a deformation correction system for a hot gas path surface of a turbine shroud. The deformation correction system may include a first die having a curved surface and a second die such that the hot gas path surface of the turbine shroud is positioned between the first die and the second die.
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