Maximum Takeoff Thrust
379.05 kN
Overall Pressure Ratio
43.97
Fuel Flow Take Off
2.7842 kg/s
NOx Unitaryto CAEP8
74.6193 % 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
Phase5 Tiled |
| 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
8.76 |
Overall Pressure Ratio
43.97 |
Afterburner
No |
Pictures
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All data (81 fields)
- Name
- Trent XWB-84EP
- EASA ID
- 07P27RR153
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.76
- Overall Pressure Ratio
- 43.97
- Maximum Takeoff Thrust (kN)
- 379.05
- Hydrocarbon Take Off (g/kg fuel)
- 0
- Hydrocarbon Climb Out (g/kg fuel)
- 0
- Hydrocarbon Approach (g/kg fuel)
- 0
- Hydrocarbon Idle (g/kg fuel)
- 0.9976
- Hydrocarbon Unitary Average (g/kN)
- 1.0405
- Hydrocarbon Unitary Sigma (g/kN)
- 0.3198
- Hydrocarbon Unitary Range (g/kN)
- 0.57-1.29
- Hydrocarbon Unitary Characteristic (g/kN)
- 1.1873
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 6.0575
- Hydrocarbon LTO (g)
- 394.3884
- Carbon Monoxide Take Off (g/kg fuel)
- 0.3142
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.368
- Carbon Monoxide Approach (g/kg fuel)
- 0.9085
- Carbon Monoxide Idle (g/kg fuel)
- 21.2878
- Carbon Monoxide Unitary Average (g/kN)
- 23.0167
- Carbon Monoxide Unitary SD (g/kN)
- 2.0805
- Carbon Monoxide Unitary Range (g/kN)
- 20.53-24.99
- Carbon Monoxide Unitary Characteristic (g/kN)
- 24.6247
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 20.8684
- NOx Take Off (g/kg fuel)
- 49.0289
- NOx Climb Out (g/kg fuel)
- 37.7525
- NOx Approach (g/kg fuel)
- 12.4251
- NOx Idle (g/kg fuel)
- 4.4684
- NOx Unitary Average (g/kN)
- 55.4242
- NOx Unitary SD (g/kN)
- 1.136
- NOx Unitary Range (g/kN)
- 54.47-56.74
- NOx Unitary Characteristic (g/kN)
- 58.2432
- NOx Unitaryto Standard (% of limit)
- 45.526
- NOx Unitaryto CAEP2 (% of limit)
- 56.9075
- NOx Unitaryto CAEP4 (% of limit)
- 61.3514
- NOx Unitaryto CAEP6 (% of limit)
- 67.028
- NOx Unitaryto CAEP8 (% of limit)
- 74.6193
- NOx LTO (g)
- 21007.3
- Smoke Take Off (SN)
- 5.9282
- Smoke Climb Out (SN)
- 6.6867
- Smoke Approach (SN)
- 7.7455
- Smoke Idle (SN)
- 1.6021
- Smoke Max (SN)
- 10.4
- Smoke Sigma (SN)
- 2.1
- Smoke Range (SN)
- 7.4-11.9
- Smoke Characteristic (SN)
- 11.3008
- Smoke Characteristicto Regulatory (% of limit)
- 68.7795
- Fuel Flow Take Off (kg/s)
- 2.7842
- Fuel Flow Climbout (kg/s)
- 2.2678
- Fuel Flow Approach (kg/s)
- 0.7399
- Fuel Flow Idle (kg/s)
- 0.2534
- Fuel LTO (kg)
- 989.19
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 8723.956
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 92.7906
- nvPME Imass Climb Out (mg/kg)
- 48.2243
- nvPME Imass Idle (mg/kg)
- 21.1697
- nvPME Imass Max (mg/kg)
- 120.1056
- nvPME Imass Take Off (mg/kg)
- 35.3835
- nvPME Inum Approach (#/kg)
- 1266186000000000
- nvPME Inum Climb Out (#/kg)
- 270426100000000
- nvPME Inum Idle (#/kg)
- 884639900000000
- nvPME Inum Max (#/kg)
- 1309446000000000
- nvPME Inum Take Off (#/kg)
- 135073100000000
- nvPMLTO Mass (mg)
- 43419.83
- nvPMLTO Mass Per Thrust (mg/kN)
- 129.3183
- nvPMLTO Mass To CAEP11 (% of limit)
- 60.4291
- nvPMLTO Number (#)
- 671315400000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1999395000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 71.9207
- nvPM Mass Concentration Characteristic (mg/m³)
- 2232.51
- nvPM Mass Concentration Max (mg/m³)
- 2029.574
- nvPM Mass Concentration To CAEP10 (% of limit)
- 60.0958