G.E. 4118T43P01 Stage 9 High Pressure Compressor Blade
GE Engine Services
Part # 4118T43P01=CZ
8130-3 Eligible
8130-3 Eligible
The high-pressure compressor blade 4118T43P01 is engineered to reduce fouling and enhance compressor performance in gas turbines. Its polished finish and durable super alloy construction allow for extended water-wash intervals and minimized engine downtime, contributing to improved operational efficiency and longevity of compressor components.
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Overview
GE Engines stage-9 High Pressure Compressor blades 4118T43P01 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 high-pressure compressor blades 4118T43P01 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. High Pressure Compressor blade 4118T43P01 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
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