Threaded fasteners used in jet engines experience seizing/galling prob
lems due to exposure to high temperatures, corrosive environments, and
vibration. Silver coating is commonly used to prevent sating and gall
ing. However, silver attacks waspaloy when exposed to high temperature
s and spreads outside the fastener and reacts with various materials u
sed in the engine. Alternative high-temperature coatings are selected
based on their thermal, oxidative and tribological properties. Physica
l vapor deposition (PVD) and sol-gel techniques were used to deposite
these coatings on waspaloy coupons and fasteners. The coatings were ch
aracterized by Auger electron spectroscopy and optical microscopy befo
re and after thermal treatments. Selected coatings were applied on fas
teners which were then assembled and exposed at 650 degrees C in air f
or 100 hours. The torques were measured during assembly and disassembl
y. Titanium nitride and palladium-coated fasteners showed the most con
sistent and low values of the ratio of break-loose torque to assembly
torque.