CF6-50E2

Turbofan · GE Aircraft Engines
Reaction Turbines
Maximum Takeoff Thrust
230.4 kN
Bypass Ratio
4.3
Overall Pressure Ratio
29.8
Fuel Flow Take Off
2.487 kg/s
NOx Unitaryto CAEP8
129 % of limit

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber —
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 4.3 Overall Pressure Ratio 29.8 Afterburner No

Pictures

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CF6-50C1 GE Aircraft Engines 230.4 4.3 28.44 Compare
CF6-50C1, -C2 GE Aircraft Engines 230.4 4.3 29.8 Compare
CF6-50C2 GE Aircraft Engines 230.4 4.3 28.44 Compare
CF6-50E GE Aircraft Engines 230.4 4.3 28.44 Compare
CF6-50E1 GE Aircraft Engines 230.4 4.3 28.44 Compare
CF6-50E2 General Electric Company 230.4 4.3 28.44 Compare
All data (58 fields)
Name
CF6-50E2
EASA ID
1GE009
Aircraft Engine Manufacturer
GE Aircraft Engines
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.3
Overall Pressure Ratio
29.8
Maximum Takeoff Thrust (kN)
230.4
Hydrocarbon Take Off (g/kg fuel)
0.6
Hydrocarbon Climb Out (g/kg fuel)
0.7
Hydrocarbon Approach (g/kg fuel)
1
Hydrocarbon Idle (g/kg fuel)
21.8
Hydrocarbon Unitary Average (g/kN)
33.5
Hydrocarbon Unitary Sigma (g/kN)
3.8
Hydrocarbon Unitary Characteristic (g/kN)
37.3
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
190.1
Hydrocarbon LTO (g)
7715
Carbon Monoxide Take Off (g/kg fuel)
0.5
Carbon Monoxide Climb Out (g/kg fuel)
0.5
Carbon Monoxide Approach (g/kg fuel)
4.3
Carbon Monoxide Idle (g/kg fuel)
61.8
Carbon Monoxide Unitary Average (g/kN)
93.7
Carbon Monoxide Unitary SD (g/kN)
4.6
Carbon Monoxide Unitary Characteristic (g/kN)
99
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
83.9
NOx Take Off (g/kg fuel)
36.3
NOx Climb Out (g/kg fuel)
29.7
NOx Approach (g/kg fuel)
9.5
NOx Idle (g/kg fuel)
3.6
NOx Unitary Average (g/kN)
61.8
NOx Unitary SD (g/kN)
0.5
NOx Unitary Characteristic (g/kN)
64.3
NOx Unitaryto Standard (% of limit)
64.6
NOx Unitaryto CAEP2 (% of limit)
80.7
NOx Unitaryto CAEP4 (% of limit)
96.5
NOx Unitaryto CAEP6 (% of limit)
109.7
NOx Unitaryto CAEP8 (% of limit)
129
NOx LTO (g)
14247
Smoke Take Off (SN)
4.1
Smoke Climb Out (SN)
2.7
Smoke Approach (SN)
2.7
Smoke Idle (SN)
4.5
Smoke Max (SN)
4.5
Smoke Sigma (SN)
1.5
Smoke Characteristic (SN)
4.8
Smoke Characteristicto Regulatory (% of limit)
25.5
Fuel Flow Take Off (kg/s)
2.487
Fuel Flow Climbout (kg/s)
1.975
Fuel Flow Approach (kg/s)
0.66
Fuel Flow Idle (kg/s)
0.215
Fuel LTO (kg)
859
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
21591
Emissions Data Status
PR
Engine Status
Out of production