G.E. 4118T44P01 Stage 10 High Pressure Compressor Blade
GE Engine Services
Part # 4118T44P01=CZ
8130-3 Eligible
8130-3 Eligible
The high-pressure compressor blades 4118T44P01 are engineered to reduce fouling and enhance operational uptime in gas turbines. Their polished finish and durable super alloy construction help extend water-wash intervals and minimize engine shutdowns, contributing to sustained compressor performance under demanding conditions.
Don't have an account? Register for an account here.
Overview
GE's high-pressure compressor blades 4118T44P01 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 high-pressure stage-10 compressor blades 4118T44P01 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 4118T44P01 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
Don't have an account? Register for an account here.
DISCLAIMER: Product information provided “as is.” Boeing may add, change, discontinue or remove this information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
