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G.E.® CFMI-3 Non-LLP High Pressure Turbine Rotor Blade 1475M35P02

Part # 1475M35P02=G3
The GE Engines - CFMI-3 Non-LLP 1475M35P02 high pressure turbine rotor blade is designed to provide a pressure gradient along its length to ensure that the air is maintained at a suitably uniform axial velocity. The air stream's centrifugal force is countered by the rotor's centrifugal action due to the increased pressure at the tip. This high-resistance super polished high-pressure turbine rotor blade 1475M35P02 is fabricated from high strength super alloys that can withstand engine operating temperature. 1475M35P02 turbine rotor blades work to create the high-pressure and high-velocity air that is necessary for the engine to produce thrust. In such circumstances these turbine blade manages mechanical stress and also transfers heat to survive in these conditions.

FEATURES
• Resistant to oxidation and corrosion at high temperatures
• Reduces gas turbine engine downtime

BENEFITS
• Increased efficiency thus lowering the fuel consumption
• Highly reliable on harsh environmental conditions
Material is non forecasted. Orders can not be canceled or returned. Please see our returnspolicy for more information.
NSN
 
Cage Code
 
Country of origin
United States 
ECCN / USML
9A991.d 
Schedule B
8411917010 
Dimensions (L x W x H)
1 x 1 x 1 IN
Total Shelf Life (days)
No Information
Hazmat Code
Package Weight
.35 LB
FAA Approval Code
PC
ISBN
 
Condition
Color
 
Brand
 
Hazmat(Y/N)
LTL(Y/N)
8130-3 Eligible
Yes 
Forecasted
No
Item Replacement History
  • 1475M35P02

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