Maximum Takeoff Thrust
308.7066 kN
Overall Pressure Ratio
41.9509
Fuel Flow Take Off
2.3956 kg/s
NOx Unitaryto CAEP8
49.8742 % 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
TAPS |
| 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
8.987 |
Overall Pressure Ratio
41.9509 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- GEnx-1B67/P2
- EASA ID
- 07P27GE233
- Aircraft Engine Manufacturer
- General Electric Company
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Combustion Chamber
- TAPS
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.987
- Overall Pressure Ratio
- 41.9509
- Maximum Takeoff Thrust (kN)
- 308.7066
- Hydrocarbon Take Off (g/kg fuel)
- 0.0178
- Hydrocarbon Climb Out (g/kg fuel)
- 0.0129
- Hydrocarbon Approach (g/kg fuel)
- 0.0465
- Hydrocarbon Idle (g/kg fuel)
- 0.678
- Hydrocarbon Unitary Average (g/kN)
- 0.767
- Hydrocarbon Unitary Sigma (g/kN)
- 0.0595
- Hydrocarbon Unitary Range (g/kN)
- 0.7-0.81
- Hydrocarbon Unitary Characteristic (g/kN)
- 1.1813
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 6.0268
- Hydrocarbon LTO (g)
- 236.7739
- Carbon Monoxide Take Off (g/kg fuel)
- 0.1043
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.2699
- Carbon Monoxide Approach (g/kg fuel)
- 1.8451
- Carbon Monoxide Idle (g/kg fuel)
- 14.8574
- Carbon Monoxide Unitary Average (g/kN)
- 17.1052
- Carbon Monoxide Unitary SD (g/kN)
- 0.2777
- Carbon Monoxide Unitary Range (g/kN)
- 16.79-17.33
- Carbon Monoxide Unitary Characteristic (g/kN)
- 20.9957
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 17.7929
- NOx Take Off (g/kg fuel)
- 27.0679
- NOx Climb Out (g/kg fuel)
- 15.7902
- NOx Approach (g/kg fuel)
- 10.0996
- NOx Idle (g/kg fuel)
- 4.5143
- NOx Unitary Average (g/kN)
- 31.8489
- NOx Unitary SD (g/kN)
- 0.5664
- NOx Unitary Range (g/kN)
- 31.44-32.5
- NOx Unitary Characteristic (g/kN)
- 36.9178
- NOx Unitaryto Standard (% of limit)
- 29.796
- NOx Unitaryto CAEP2 (% of limit)
- 37.245
- NOx Unitaryto CAEP4 (% of limit)
- 40.6128
- NOx Unitaryto CAEP6 (% of limit)
- 44.5534
- NOx Unitaryto CAEP8 (% of limit)
- 49.8742
- NOx LTO (g)
- 9831.968
- Smoke Take Off (SN)
- 0.292
- Smoke Climb Out (SN)
- 0.2924
- Smoke Approach (SN)
- 0.4773
- Smoke Idle (SN)
- 0.48
- Smoke Max (SN)
- 0.9582
- Smoke Sigma (SN)
- 0.3273
- Smoke Range (SN)
- 0.74-1.34
- Smoke Characteristic (SN)
- 1.2333
- Smoke Characteristicto Regulatory (% of limit)
- 7.096
- Fuel Flow Take Off (kg/s)
- 2.3956
- Fuel Flow Climbout (kg/s)
- 1.9657
- Fuel Flow Approach (kg/s)
- 0.6253
- Fuel Flow Idle (kg/s)
- 0.2124
- Fuel LTO (kg)
- 841.5054
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 5280.472
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 1.497
- nvPME Imass Climb Out (mg/kg)
- 0.0152
- nvPME Imass Idle (mg/kg)
- 0.211
- nvPME Imass Max (mg/kg)
- 5.7777
- nvPME Imass Take Off (mg/kg)
- 0.0167
- nvPME Inum Approach (#/kg)
- 89763910000000
- nvPME Inum Climb Out (#/kg)
- 5399947000
- nvPME Inum Idle (#/kg)
- 23506410000000
- nvPME Inum Max (#/kg)
- 244528700000000
- nvPME Inum Take Off (#/kg)
- 5070391000
- nvPMLTO Mass (mg)
- 300.181
- nvPMLTO Mass Per Thrust (mg/kN)
- 1.3517
- nvPMLTO Mass To CAEP11 (% of limit)
- 0.6316
- nvPMLTO Number (#)
- 21261170000000000
- nvPMLTO Number Per Thrust (#/kN)
- 95735130000000
- nvPMLTO Number To CAEP11 (% of limit)
- 3.4437
- nvPM Mass Concentration Characteristic (mg/m³)
- 159.8387
- nvPM Mass Concentration Max (mg/m³)
- 124.1787
- nvPM Mass Concentration To CAEP10 (% of limit)
- 3.988