G.E.® Blade K388P13, High Pressure Compressor, Stage 13
GE Engines Trio II
Part # K388P13=CK
8130-3 Eligible
8130-3 Eligible
The K388P13 high-pressure compressor blades are engineered to reduce fouling and enhance uptime in gas turbines. With a high-resistance mirror finish and made from durable super alloys, these blades help extend water-wash intervals and minimize engine shutdowns, maintaining compressor performance over time.The K388P13 high-pressure compressor blades are engineered to reduce fou
GE Engines TRIO II stage 13 High Pressure Compressor blades K388P13 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 13 high-pressure compressor blades K388P13 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 K388P13 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
Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
