The stage 9 compressor blades 6020T80P02 are engineered to reduce fouling and enhance gas turbine performance. Their high-resistance mirror finish allows for extended offline water-wash intervals, minimizing engine shutdowns. Made from durable super alloys with a polished coating, these blades are designed to endure high operating temperatures and pressures.
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Overview
GE Engines stage 9 compressor blades 6020T80P02 are designed significantly to lower fouling rates and increase up time, preserving compressor performance over time. Compressor blade fouling is a significant process that causes gas turbine performance to decline over time. However, these high-resistance mirror finish polish of stage 9 compressor blades 6020T80P02 allow operators to prolong their offline water-wash intervals and shorten engine shutdowns. This considerably reduces the amount of fouling on vital gas turbine compressor components. Compressor blade 6020T80P02 is fabricated from high strength super alloys with super polished protection coating that can withstand engine operating temperature and pressure.
Features & Benefits
Reduces gas turbine engine downtime
Lowers the fouling rate
Resilient finish prevents the collection of dirt and debris in the blades
Increased water-washing intervals for gas turbine compressors
Highly reliable on harsh environmental conditions
Specifications
Overall Length: 1.028 Inches Nominal
Overall Height: 0.4435 Inches Nominal
Blade Attachment Method: Dovetail
Engine Section Location: Compressor
Material: Titanium Alloy Blade
Material Document and Classification: AMS 4928 ASSN STD Single Material Response Blade
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