Surface Preparation
- The turbine blades were abrasive blast cleaned to achieve a surface cleanliness level of SA2.5 with a 75-micron profile, in accordance with ISO 8501/4 Standard SA2.5 (SSPCSP10/NACE 2). This preparation ensured that the repair materials would adhere effectively to the substrate.
Application of UPS 200 EG CERAMIC REPAIR PASTE
- The pitted and damaged sections on the leading edges of the turbine blades were rebuilt using UPS 200 EG. This step restored the structural integrity of the blades, filling in areas where material had been lost due to corrosion and wear.
Application of UPS 210 CR EFFICIENCY FLUID CERAMIC
- The blades were then coated by brush with UPS 210 CR. The material was applied in two coats to achieve a nominal total dry film thickness of 500 microns. This coating provided robust protection against future corrosion and wear, ensuring the long-term performance of the turbine blades.