G.E. 4125T65G02 Stage 2 High Pressure Turbine Blade
GE Engine Services
Part # 4125T65G02=CZ
8130-3 Eligible
8130-3 Eligible
The high-pressure turbine blade 4125T65G02 is designed for GE engines, extracting energy from extreme temperatures and pressures. Made from durable super alloys, it withstands mechanical stress and heat, contributing to the generation of high-velocity air essential for engine thrust and supporting the compressor and other systems.
Don't have an account? Register for an account here.
Overview
GE engine stage-2 high pressure turbine blades 4125T65G02 are responsible for extracting energy from high pressure and temperature. Turbine blades must operate under extreme circumstances, to provide additional power to drive the compressor and other systems in the engine. This high-resistance super polished high-pressure stage-2 turbine blade 4125T65G02 is fabricated from high strength super alloys that can withstand engine operating temperature. 4125T65G02 turbine blades work to create the high-pressure and high-velocity air that is necessary for the engine to produce thrust. In such circumstances 4125T65G02 turbine blade manages mechanical stress and also transfers heat to survive in these conditions.
Features & Benefits
Resistant to oxidation and corrosion at high temperatures
Reduces gas turbine engine downtime
Increased efficiency thus lowering the fuel consumption
Don't have an account? Register for an account here.
DISCLAIMER: Product information provided “as is.” Boeing may add, change, discontinue or remove this information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
