Optimizing slurry viscosity and particle content resolves the trade-off between fluidity and coating density during high-velocity spraying.
Incorporating a soluble sulfate salt into the zinc spraying material slows the corrosion rate and extends service life without increasing material consumption.
Optimizing ceramic surface roughness between 2.5 and 7 micrometers resolves coating adhesion failures while maintaining sliding surface integrity.
Blending ceramic particles into a thermoplastic matrix creates durable wear surfaces that lower manufacturing costs compared to exotic alloys.
A bimodal eutectic aluminum-silicon matrix powder with controlled molten fraction enables low stress metallic coating deposition.
Thermal spray processing creates a multi-phase complex oxide structure that withstands chlorine plasma, reducing contamination in semiconductor manufacturing.
Opposing gas flow prevents pore clogging during oxide deposition, preserving structural integrity and eliminating expensive unblocking operations.
Dynamic wire positioning compensates for assembly tolerances, preventing spatter and unmelted particles in thermal coatings.
Thermal spraying deposits a molybdenum layer that reduces friction and wear across diverse alloy materials without requiring material-specific treatments.
Machining profile patterns into turbine shroud ceramic coatings removes material uniformly, preventing bucket damage from thermal expansion rubbing.
Co-based alloy coating on steam turbine rotor blade contact surfaces prevents fretting wear and fatigue damage during high output operation.
Pulsed excimer lasers melt porous ceramic coatings to reduce porosity and prevent particle shedding in plasma chambers.
Segmented ceramic outer layers accommodate differential expansion to prevent cracking in gas turbine engine coatings.
Thermal vaporization deposits fluoride anions on oxide coatings, resolving plasma-induced contamination and yield loss in semiconductor etching.
YOF-based slurry enables suspension plasma spray deposition of dense, corrosion-resistant coatings with controlled crystal structures.
A plasma-sprayed gadolinia-stabilized zirconia layer blocks molten sand penetration into turbine engine thermal barrier coatings.
Variable thickness coatings on cylinder liners reduce friction at top and bottom dead centers while minimizing material usage compared to uniform layers.
Porous ceramic agglomerates replace organic binders in thermal spray processes, resolving the trade-off between erosion resistance and blade abradability.
Iron-chromium wire arc spraying deposits dense functional layers on engine components.