G.E. 4129T04P09 Stage 4 High Pressure Compressor Blade
GE Engine Services
Part # 4129T04P09=CZ
8130-3 Eligible
8130-3 Eligible
G.E.® 4129T04P09 Stage 4 High Pressure Compressor Blade is a critical component designed for gas turbine engines, made from high-strength super alloys to withstand extreme operating conditions.
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Overview
4129T04P09 Stage 4 High Pressure Compressor Blade is a key component within the high-pressure compressor (HPC) section of a General Electric (GE) gas turbine engine. Its primary purpose is to compress incoming air to a high pressure before it enters the combustion chamber, which is crucial for efficient fuel combustion and thrust generation. The blade is fabricated from high-strength super alloys, engineered to endure the extreme mechanical stress and high temperatures encountered during engine operation. Specific design features help to lower fouling rates, increase the time between maintenance, and preserve compressor performance.
Features & Benefits
Constructed from high-strength super alloys for durability
Designed to withstand extreme mechanical stress and high temperatures
Compresses incoming air efficiently for optimal combustion
Helps lower fouling rates and increase maintenance intervals
Preserves compressor performance for enhanced engine efficiency
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