Powder coating of gas turbine engine components

摘要

In accordance with one embodiment of the invention, there is provided a method of coating a gas turbine engine component using a powder coating process. The method comprises providing a gas turbine engine component; and applying a powder coating to the gas turbine engine component using the powder coating process. The powder coating is applied in a dry form without an organic solvent. The method further comprises heating the applied powder coating to melt and fuse particles of the powder coating to the gas turbine engine component and cure the powder coating.