Maximum Takeoff Thrust
327.9185 kN
Overall Pressure Ratio
45.7702
Fuel Flow Take Off
2.502 kg/s
NOx Unitaryto CAEP8
80.37 % 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
8.9394 |
Overall Pressure Ratio
45.7702 |
Afterburner
No |
Pictures
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All data (82 fields)
- Name
- Trent7000-72
- EASA ID
- 02P23RR141
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 8.9394
- Overall Pressure Ratio
- 45.7702
- Maximum Takeoff Thrust (kN)
- 327.9185
- 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)
- 0.4233
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.4098
- Carbon Monoxide Approach (g/kg fuel)
- 0.6309
- Carbon Monoxide Idle (g/kg fuel)
- 7.1561
- Carbon Monoxide Unitary Average (g/kN)
- 9.5952
- Carbon Monoxide Unitary SD (g/kN)
- 1.8003
- Carbon Monoxide Unitary Range (g/kN)
- 6.13-11.91
- Carbon Monoxide Unitary Characteristic (g/kN)
- 10.06
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 8.5
- NOx Take Off (g/kg fuel)
- 52.7363
- NOx Climb Out (g/kg fuel)
- 39.7275
- NOx Approach (g/kg fuel)
- 14.1775
- NOx Idle (g/kg fuel)
- 5.6084
- NOx Unitary Average (g/kN)
- 63.3859
- NOx Unitary SD (g/kN)
- 0.7701
- NOx Unitary Range (g/kN)
- 62.45-64.48
- NOx Unitary Characteristic (g/kN)
- 65.6304
- NOx Unitaryto Standard (% of limit)
- 49.8938
- NOx Unitaryto CAEP2 (% of limit)
- 62.3672
- NOx Unitaryto CAEP4 (% of limit)
- 66.6026
- NOx Unitaryto CAEP6 (% of limit)
- 72.5195
- NOx Unitaryto CAEP8 (% of limit)
- 80.37
- NOx LTO (g)
- 20784.36
- Smoke Take Off (SN)
- 8.7024
- Smoke Climb Out (SN)
- 11.9463
- Smoke Approach (SN)
- 8.9606
- Smoke Idle (SN)
- 2.0108
- 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)
- 95.9
- Fuel Flow Take Off (kg/s)
- 2.502
- Fuel Flow Climbout (kg/s)
- 2.0395
- Fuel Flow Approach (kg/s)
- 0.6708
- Fuel Flow Idle (kg/s)
- 0.2589
- Fuel LTO (kg)
- 939.1343
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 3146.298
- Emissions Data Status
- C
- Engine Status
- Out of Production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 74.0088
- nvPME Imass Climb Out (mg/kg)
- 84.073
- nvPME Imass Idle (mg/kg)
- 18.8269
- nvPME Imass Max (mg/kg)
- 152.4957
- nvPME Imass Take Off (mg/kg)
- 48.0692
- nvPME Inum Approach (#/kg)
- 857579100000000
- nvPME Inum Climb Out (#/kg)
- 283044600000000
- nvPME Inum Idle (#/kg)
- 447015900000000
- nvPME Inum Max (#/kg)
- 961993500000000
- nvPME Inum Take Off (#/kg)
- 145142500000000
- nvPMLTO Mass (mg)
- 47203.02
- nvPMLTO Mass Per Thrust (mg/kN)
- 200.0937
- nvPMLTO Mass To CAEP11 (% of limit)
- 93.5017
- nvPMLTO Number (#)
- 410040200000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1738161000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 62.5238
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 87.0358