G.E.® TRIO II Stage 12 Wide High Pressure Compressor Blade K289P18
GE Engines TRIO II
Part # K289P18=CK
8130-3 Eligible
8130-3 Eligible
The high-pressure compressor blade K289P18 is designed for GE Engines' TRIO II system, enhancing mass flow rates while reducing fouling. Its polished finish and durable super alloy construction help maintain compressor performance, extend water-wash intervals, and minimize engine downtime, contributing to improved operational efficiency in gas turbines.
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Allocation Control: Allocation control is a process used to ensure fair allocation of assets. It is applied to parts with limited availability and high customer demand. Due to the nature of allocation control items, there is the possibility that stock shown as available may already be allocated based on previously received customer order(s). Specific questions related to allocation control, please contact Boeing Customer Support.
Overview
GE Engines - TRIO II high-pressure compressor stage-12 wide blade K289P18 is designed significantly where high mass flow rate is required. These blades 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-12 compressor blades K289P18 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. K289P18 is fabricated from high strength super alloys with super polished protection coating that can withstand engine operating temperature and pressure.
Features & Benefits
High-mass flow rate
Reduces gas turbine engine downtime
Lowers the fouling rate
Resilient finishing 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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Allocation Control: Allocation control is a process used to ensure fair allocation of assets. It is applied to parts with limited availability and high customer demand. Due to the nature of allocation control items, there is the possibility that stock shown as available may already be allocated based on previously received customer order(s). Specific questions related to allocation control, please contact Boeing Customer Support.