Maximum Takeoff Thrust
363.8735 kN
Overall Pressure Ratio
49.5509
Fuel Flow Take Off
2.8719 kg/s
NOx Unitaryto CAEP8
90.0452 % 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
8.8835 |
Overall Pressure Ratio
49.5509 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- Trent 1000-R3
- EASA ID
- 02P23RR138
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.8835
- Overall Pressure Ratio
- 49.5509
- Maximum Takeoff Thrust (kN)
- 363.8735
- 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)
- 0.434
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.4313
- Carbon Monoxide Approach (g/kg fuel)
- 0.525
- Carbon Monoxide Idle (g/kg fuel)
- 5.9151
- Carbon Monoxide Unitary Average (g/kN)
- 7.6094
- Carbon Monoxide Unitary SD (g/kN)
- 1.2472
- Carbon Monoxide Unitary Range (g/kN)
- 6.32-9.17
- Carbon Monoxide Unitary Characteristic (g/kN)
- 8.04
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 6.8
- NOx Take Off (g/kg fuel)
- 67.2866
- NOx Climb Out (g/kg fuel)
- 47.8925
- NOx Approach (g/kg fuel)
- 14.8882
- NOx Idle (g/kg fuel)
- 6.2364
- NOx Unitary Average (g/kN)
- 77.1665
- NOx Unitary SD (g/kN)
- 0.8639
- NOx Unitary Range (g/kN)
- 75.86-77.98
- NOx Unitary Characteristic (g/kN)
- 80.3399
- NOx Unitaryto Standard (% of limit)
- 57.7562
- NOx Unitaryto CAEP2 (% of limit)
- 72.1953
- NOx Unitaryto CAEP4 (% of limit)
- 75.7197
- NOx Unitaryto CAEP6 (% of limit)
- 81.9279
- NOx Unitaryto CAEP8 (% of limit)
- 90.0452
- NOx LTO (g)
- 28077.44
- Smoke Take Off (SN)
- 7.8048
- Smoke Climb Out (SN)
- 9.7465
- Smoke Approach (SN)
- 10.154
- Smoke Idle (SN)
- 1.7842
- 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)
- 98.6
- Fuel Flow Take Off (kg/s)
- 2.8719
- Fuel Flow Climbout (kg/s)
- 2.3219
- Fuel Flow Approach (kg/s)
- 0.7435
- Fuel Flow Idle (kg/s)
- 0.2699
- Fuel LTO (kg)
- 1026.596
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2768.705
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 84.522
- nvPME Imass Climb Out (mg/kg)
- 58.3213
- nvPME Imass Idle (mg/kg)
- 19.4339
- nvPME Imass Max (mg/kg)
- 154.1347
- nvPME Imass Take Off (mg/kg)
- 40.8116
- nvPME Inum Approach (#/kg)
- 896117500000000
- nvPME Inum Climb Out (#/kg)
- 184355800000000
- nvPME Inum Idle (#/kg)
- 474920300000000
- nvPME Inum Max (#/kg)
- 932130000000000
- nvPME Inum Take Off (#/kg)
- 99613180000000
- nvPMLTO Mass (mg)
- 46062.68
- nvPMLTO Mass Per Thrust (mg/kN)
- 175.9658
- nvPMLTO Mass To CAEP11 (% of limit)
- 82.227
- nvPMLTO Number (#)
- 428384800000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1636490000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 58.8665
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 90.4434