Maximum Takeoff Thrust
436.7487 kN
Overall Pressure Ratio
48.4132
Fuel Flow Take Off
3.4978 kg/s
NOx Unitaryto CAEP8
93.5579 % 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 (improved) |
| 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
8.059 |
Overall Pressure Ratio
48.4132 |
Afterburner
No |
Pictures
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All data (81 fields)
- Name
- Trent XWB-97
- EASA ID
- 01P21RR125
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled (improved)
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.059
- Overall Pressure Ratio
- 48.4132
- Maximum Takeoff Thrust (kN)
- 436.7487
- 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)
- 0.0101
- Hydrocarbon Unitary Average (g/kN)
- 0.0108
- Hydrocarbon Unitary Sigma (g/kN)
- 0.0144
- Hydrocarbon Unitary Range (g/kN)
- 0-0.03
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.0126
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 0.0643
- Hydrocarbon LTO (g)
- 4.7214
- Carbon Monoxide Take Off (g/kg fuel)
- 0.356
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.3994
- Carbon Monoxide Approach (g/kg fuel)
- 0.8188
- Carbon Monoxide Idle (g/kg fuel)
- 7.7463
- Carbon Monoxide Unitary Average (g/kN)
- 9.1949
- Carbon Monoxide Unitary SD (g/kN)
- 1.5314
- Carbon Monoxide Unitary Range (g/kN)
- 7.44-10.28
- Carbon Monoxide Unitary Characteristic (g/kN)
- 9.9447
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 8.4277
- NOx Take Off (g/kg fuel)
- 66.0503
- NOx Climb Out (g/kg fuel)
- 48.5052
- NOx Approach (g/kg fuel)
- 14.8587
- NOx Idle (g/kg fuel)
- 5.6411
- NOx Unitary Average (g/kN)
- 76.798
- NOx Unitary SD (g/kN)
- 0.895
- NOx Unitary Range (g/kN)
- 75.77-77.36
- NOx Unitary Characteristic (g/kN)
- 81.3452
- NOx Unitaryto Standard (% of limit)
- 59.4514
- NOx Unitaryto CAEP2 (% of limit)
- 74.3142
- NOx Unitaryto CAEP4 (% of limit)
- 78.3473
- NOx Unitaryto CAEP6 (% of limit)
- 84.9235
- NOx Unitaryto CAEP8 (% of limit)
- 93.5579
- NOx LTO (g)
- 33539.74
- Smoke Take Off (SN)
- 9.3037
- Smoke Climb Out (SN)
- 6.901
- Smoke Approach (SN)
- 6.4964
- Smoke Idle (SN)
- 1.2609
- Smoke Max (SN)
- 9.3037
- Smoke Sigma (SN)
- 0.1888
- Smoke Range (SN)
- 9.1-9.5
- Smoke Characteristic (SN)
- 10.234
- Smoke Characteristicto Regulatory (% of limit)
- 64.7523
- Fuel Flow Take Off (kg/s)
- 3.4978
- Fuel Flow Climbout (kg/s)
- 2.798
- Fuel Flow Approach (kg/s)
- 0.9181
- Fuel Flow Idle (kg/s)
- 0.3008
- Fuel LTO (kg)
- 1205.897
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 4015.656
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 58.9524
- nvPME Imass Climb Out (mg/kg)
- 35.1256
- nvPME Imass Idle (mg/kg)
- 8.2628
- nvPME Imass Max (mg/kg)
- 64.7147
- nvPME Imass Take Off (mg/kg)
- 43.5427
- nvPME Inum Approach (#/kg)
- 926615300000000
- nvPME Inum Climb Out (#/kg)
- 210203400000000
- nvPME Inum Idle (#/kg)
- 483204600000000
- nvPME Inum Max (#/kg)
- 961000000000000
- nvPME Inum Take Off (#/kg)
- 194751000000000
- nvPMLTO Mass (mg)
- 36237.41
- nvPMLTO Mass Per Thrust (mg/kN)
- 93.6677
- nvPMLTO Mass To CAEP11 (% of limit)
- 43.77
- nvPMLTO Number (#)
- 537188100000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1388542000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 49.9476
- nvPM Mass Concentration Characteristic (mg/m³)
- 1338.788
- nvPM Mass Concentration Max (mg/m³)
- 1217.092
- nvPM Mass Concentration To CAEP10 (% of limit)
- 37.885