Maximum Takeoff Thrust
287.1372 kN
Overall Pressure Ratio
40.3476
Fuel Flow Take Off
2.1075 kg/s
NOx Unitaryto CAEP8
76.5202 % 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
9.282 |
Overall Pressure Ratio
40.3476 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- Trent 1000-H3
- EASA ID
- 02P23RR130
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 9.282
- Overall Pressure Ratio
- 40.3476
- Maximum Takeoff Thrust (kN)
- 287.1372
- 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)
- 0.427
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.385
- Carbon Monoxide Approach (g/kg fuel)
- 0.8262
- Carbon Monoxide Idle (g/kg fuel)
- 8.3928
- Carbon Monoxide Unitary Average (g/kN)
- 11.4447
- Carbon Monoxide Unitary SD (g/kN)
- 2.0505
- Carbon Monoxide Unitary Range (g/kN)
- 7.4-14.1
- Carbon Monoxide Unitary Characteristic (g/kN)
- 12
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 10.2
- NOx Take Off (g/kg fuel)
- 42.1376
- NOx Climb Out (g/kg fuel)
- 32.826
- NOx Approach (g/kg fuel)
- 13.0422
- NOx Idle (g/kg fuel)
- 5.2915
- NOx Unitary Average (g/kN)
- 52.3346
- NOx Unitary SD (g/kN)
- 0.892
- NOx Unitary Range (g/kN)
- 50.9-53.47
- NOx Unitary Characteristic (g/kN)
- 54.1879
- NOx Unitaryto Standard (% of limit)
- 44.8965
- NOx Unitaryto CAEP2 (% of limit)
- 56.1206
- NOx Unitaryto CAEP4 (% of limit)
- 61.7912
- NOx Unitaryto CAEP6 (% of limit)
- 68.0281
- NOx Unitaryto CAEP8 (% of limit)
- 76.5202
- NOx LTO (g)
- 15026.47
- Smoke Take Off (SN)
- 11.1422
- Smoke Climb Out (SN)
- 13.7777
- Smoke Approach (SN)
- 7.6908
- Smoke Idle (SN)
- 2.1653
- 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)
- 92.4
- Fuel Flow Take Off (kg/s)
- 2.1075
- Fuel Flow Climbout (kg/s)
- 1.7323
- Fuel Flow Approach (kg/s)
- 0.5983
- Fuel Flow Idle (kg/s)
- 0.2323
- Fuel LTO (kg)
- 823.1809
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 3286.042
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 64.1533
- nvPME Imass Climb Out (mg/kg)
- 114.0449
- nvPME Imass Idle (mg/kg)
- 18.3136
- nvPME Imass Max (mg/kg)
- 150.392
- nvPME Imass Take Off (mg/kg)
- 71.5551
- nvPME Inum Approach (#/kg)
- 811570200000000
- nvPME Inum Climb Out (#/kg)
- 417370300000000
- nvPME Inum Idle (#/kg)
- 434505600000000
- nvPME Inum Max (#/kg)
- 918210000000000
- nvPME Inum Take Off (#/kg)
- 236022300000000
- nvPMLTO Mass (mg)
- 48260.9
- nvPMLTO Mass Per Thrust (mg/kN)
- 233.6337
- nvPMLTO Mass To CAEP11 (% of limit)
- 109.1746
- nvPMLTO Number (#)
- 390335500000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1889636000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 67.9725
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 82.7371