G.E.® K715P08 TRIO II Stage 7 Wide High Pressure Compressor Blade
GE Engines TRIO II
Part # K715P08=CK
8130-3 Eligible
8130-3 Eligible
The high-pressure compressor blade K715P08 is designed for GE Engines' TRIO II, focusing on high mass flow rates. Its polished finish reduces fouling, enhancing compressor performance and extending maintenance intervals. Made from durable super alloys, it withstands demanding engine conditions, contributing to improved operational efficiency and reduced downtime.The high-pressu
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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-7 wide blade K715P08 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-7 compressor blades K715P08 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. K715P08 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.