Maximum Takeoff Thrust
298.0353 kN
Overall Pressure Ratio
40.6539
Fuel Flow Take Off
2.2934 kg/s
NOx Unitaryto CAEP8
47.5272 % 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
9.0819 |
Overall Pressure Ratio
40.6539 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- GEnx-1B64/P2
- EASA ID
- 07P27GE232
- 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
- 9.0819
- Overall Pressure Ratio
- 40.6539
- Maximum Takeoff Thrust (kN)
- 298.0353
- Hydrocarbon Take Off (g/kg fuel)
- 0.0166
- Hydrocarbon Climb Out (g/kg fuel)
- 0.0124
- Hydrocarbon Approach (g/kg fuel)
- 0.0488
- Hydrocarbon Idle (g/kg fuel)
- 0.7642
- Hydrocarbon Unitary Average (g/kN)
- 0.8727
- Hydrocarbon Unitary Sigma (g/kN)
- 0.0691
- Hydrocarbon Unitary Range (g/kN)
- 0.79-0.92
- Hydrocarbon Unitary Characteristic (g/kN)
- 1.3441
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 6.8577
- Hydrocarbon LTO (g)
- 260.1053
- Carbon Monoxide Take Off (g/kg fuel)
- 0.121
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.3799
- Carbon Monoxide Approach (g/kg fuel)
- 1.9961
- Carbon Monoxide Idle (g/kg fuel)
- 15.5887
- Carbon Monoxide Unitary Average (g/kN)
- 18.3257
- Carbon Monoxide Unitary SD (g/kN)
- 0.3028
- Carbon Monoxide Unitary Range (g/kN)
- 17.98-18.54
- Carbon Monoxide Unitary Characteristic (g/kN)
- 22.4938
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 19.0625
- NOx Take Off (g/kg fuel)
- 23.934
- NOx Climb Out (g/kg fuel)
- 14.2842
- NOx Approach (g/kg fuel)
- 9.8033
- NOx Idle (g/kg fuel)
- 4.4471
- NOx Unitary Average (g/kN)
- 29.2866
- NOx Unitary SD (g/kN)
- 0.5624
- NOx Unitary Range (g/kN)
- 28.89-29.93
- NOx Unitary Characteristic (g/kN)
- 33.9476
- NOx Unitaryto Standard (% of limit)
- 27.9847
- NOx Unitaryto CAEP2 (% of limit)
- 34.9809
- NOx Unitaryto CAEP4 (% of limit)
- 38.4424
- NOx Unitaryto CAEP6 (% of limit)
- 42.2929
- NOx Unitaryto CAEP8 (% of limit)
- 47.5272
- NOx LTO (g)
- 8728.436
- Smoke Take Off (SN)
- 0.2921
- Smoke Climb Out (SN)
- 0.2925
- Smoke Approach (SN)
- 0.4586
- Smoke Idle (SN)
- 0.4833
- 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)
- 7.0279
- Fuel Flow Take Off (kg/s)
- 2.2934
- Fuel Flow Climbout (kg/s)
- 1.8856
- Fuel Flow Approach (kg/s)
- 0.6047
- Fuel Flow Idle (kg/s)
- 0.2083
- Fuel LTO (kg)
- 815.3006
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 5461.693
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 1.2957
- nvPME Imass Climb Out (mg/kg)
- 0.015
- nvPME Imass Idle (mg/kg)
- 0.2334
- nvPME Imass Max (mg/kg)
- 5.7777
- nvPME Imass Take Off (mg/kg)
- 0.0164
- nvPME Inum Approach (#/kg)
- 79731970000000
- nvPME Inum Climb Out (#/kg)
- 6299066000
- nvPME Inum Idle (#/kg)
- 26247340000000
- nvPME Inum Max (#/kg)
- 244528700000000
- nvPME Inum Take Off (#/kg)
- 4645585000
- nvPMLTO Mass (mg)
- 269.1916
- nvPMLTO Mass Per Thrust (mg/kN)
- 1.2555
- nvPMLTO Mass To CAEP11 (% of limit)
- 0.5867
- nvPMLTO Number (#)
- 20101950000000000
- nvPMLTO Number Per Thrust (#/kN)
- 93756310000000
- nvPMLTO Number To CAEP11 (% of limit)
- 3.3725
- nvPM Mass Concentration Characteristic (mg/m³)
- 159.8387
- nvPM Mass Concentration Max (mg/m³)
- 124.1787
- nvPM Mass Concentration To CAEP10 (% of limit)
- 3.9348