Maximum Takeoff Thrust
358.0552 kN
Overall Pressure Ratio
48.7886
Fuel Flow Take Off
2.8017 kg/s
NOx Unitaryto CAEP8
88.6133 % 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
8.9171 |
Overall Pressure Ratio
48.7886 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- Trent 1000-N3
- EASA ID
- 02P23RR135
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.9171
- Overall Pressure Ratio
- 48.7886
- Maximum Takeoff Thrust (kN)
- 358.0552
- 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
- Hydrocarbon Unitary Average (g/kN)
- 0
- Hydrocarbon Unitary Sigma (g/kN)
- 0
- Hydrocarbon Unitary Range (g/kN)
- 0-0
- Hydrocarbon Unitary Characteristic (g/kN)
- 0
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 0
- Hydrocarbon LTO (g)
- 0
- Carbon Monoxide Take Off (g/kg fuel)
- 0.437
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.4305
- Carbon Monoxide Approach (g/kg fuel)
- 0.544
- Carbon Monoxide Idle (g/kg fuel)
- 6.0754
- Carbon Monoxide Unitary Average (g/kN)
- 7.8405
- Carbon Monoxide Unitary SD (g/kN)
- 1.2506
- Carbon Monoxide Unitary Range (g/kN)
- 6.54-9.43
- Carbon Monoxide Unitary Characteristic (g/kN)
- 8.28
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 7
- NOx Take Off (g/kg fuel)
- 64.4142
- NOx Climb Out (g/kg fuel)
- 46.5851
- NOx Approach (g/kg fuel)
- 14.7386
- NOx Idle (g/kg fuel)
- 6.1731
- NOx Unitary Average (g/kN)
- 74.6419
- NOx Unitary SD (g/kN)
- 0.8835
- NOx Unitary Range (g/kN)
- 73.24-75.47
- NOx Unitary Characteristic (g/kN)
- 77.7115
- NOx Unitaryto Standard (% of limit)
- 56.4857
- NOx Unitaryto CAEP2 (% of limit)
- 70.6071
- NOx Unitaryto CAEP4 (% of limit)
- 74.3101
- NOx Unitaryto CAEP6 (% of limit)
- 80.4989
- NOx Unitaryto CAEP8 (% of limit)
- 88.6133
- NOx LTO (g)
- 26724.58
- Smoke Take Off (SN)
- 7.6468
- Smoke Climb Out (SN)
- 10.0415
- Smoke Approach (SN)
- 9.9871
- Smoke Idle (SN)
- 1.8045
- Smoke Max (SN)
- 14.7
- Smoke Sigma (SN)
- 2
- Smoke Range (SN)
- 11.4-16.7
- Smoke Characteristic (SN)
- 16.4
- Smoke Characteristicto Regulatory (% of limit)
- 98.2
- Fuel Flow Take Off (kg/s)
- 2.8017
- Fuel Flow Climbout (kg/s)
- 2.2739
- Fuel Flow Approach (kg/s)
- 0.7324
- Fuel Flow Idle (kg/s)
- 0.267
- Fuel LTO (kg)
- 1010.184
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2807.177
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 82.915
- nvPME Imass Climb Out (mg/kg)
- 61.2044
- nvPME Imass Idle (mg/kg)
- 19.385
- nvPME Imass Max (mg/kg)
- 153.9402
- nvPME Imass Take Off (mg/kg)
- 40.9655
- nvPME Inum Approach (#/kg)
- 891064400000000
- nvPME Inum Climb Out (#/kg)
- 195325500000000
- nvPME Inum Idle (#/kg)
- 471721000000000
- nvPME Inum Max (#/kg)
- 931560000000000
- nvPME Inum Take Off (#/kg)
- 103709200000000
- nvPMLTO Mass (mg)
- 45841.11
- nvPMLTO Mass Per Thrust (mg/kN)
- 177.9651
- nvPMLTO Mass To CAEP11 (% of limit)
- 83.1612
- nvPMLTO Number (#)
- 423971000000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1645947000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 59.2067
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 89.9153