This high-pressure compressor blade, designed for GE Engines TRIO II stage 11, features a polished finish that reduces fouling and enhances uptime. Made from high-strength super alloys, it withstands extreme operating conditions, allowing for extended water-wash intervals and minimizing engine shutdowns, thereby maintaining compressor performance over time.
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Overview
GE Engines TRIO II stage 11 High Pressure Compressor blades K190P10 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 11 high-pressure compressor blades K190P10 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 K190P10 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
Technical Information
ATA Number
72
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
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