Compositional Bond Coat for Hindering/Reversing Creep Degradation in Environmental Barrier Coatings
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United States of America Patent
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Issued Date -
Jul 11, 2013
app pub date -
Jan 11, 2012
filing date -
Jan 11, 2012
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Abandoned
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Abstract
A gas turbine blade may have a bond coat applied to its surface. The bond coat may include silicon and a reactive material. The reactive material may react with thermally grown oxide generated at the bond layer to prevent and reverse creep. One or more protective layers may be applied to the bond layer.
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