CPC C25D 5/615 (2020.08) [C25D 3/562 (2013.01); C25D 5/50 (2013.01); C25D 7/00 (2013.01); C25D 7/10 (2013.01); F02C 7/06 (2013.01); F02C 7/30 (2013.01); F05D 2230/90 (2013.01)] | 10 Claims |
1. An article for a gas turbine engine, comprising:
a substrate, and
a nickel phosphorous coating disposed on the substrate, the nickel phosphorus coating having a columnar microstructure, wherein the coating includes at least one region of pure nickel interspersed with columns of the columnar microstructure.
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