Plating turbine engine components
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United States of America Patent
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Sep 1, 1998
Grant Date -
N/A
app pub date -
Oct 16, 1996
filing date -
Oct 16, 1996
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Abstract
A process is provided for plating a coating onto a gas turbine engine component without detrimentally effecting air flow through cooling holes by injecting a maskant into the cooling passage to fill the cooling holes with the maskant, plating the external surface of the component with a coating, then removing the maskant from the component.
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