Maximum Takeoff Thrust
34.74 kN
Overall Pressure Ratio
17.9
Fuel Flow Take Off
0.3805 kg/s
NOx Unitaryto CAEP8
81.7 % 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
Type 3 (reduced emissions) |
| 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
4.77 |
Overall Pressure Ratio
17.9 |
Afterburner
No |
Pictures
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All data (74 fields)
- Name
- AE3007A1/1
- EASA ID
- 01P06AL029
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Combustion Chamber
- Type 3 (reduced emissions)
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.77
- Overall Pressure Ratio
- 17.9
- Maximum Takeoff Thrust (kN)
- 34.74
- Hydrocarbon Take Off (g/kg fuel)
- 0.03
- Hydrocarbon Climb Out (g/kg fuel)
- 0.03
- Hydrocarbon Approach (g/kg fuel)
- 0.03
- Hydrocarbon Idle (g/kg fuel)
- 3.88
- Hydrocarbon Unitary Average (g/kN)
- 8.08
- Hydrocarbon Unitary Characteristic (g/kN)
- 12.44
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 63.5
- Hydrocarbon LTO (g)
- 280
- Carbon Monoxide Take Off (g/kg fuel)
- 0.74
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.55
- Carbon Monoxide Approach (g/kg fuel)
- 6.8
- Carbon Monoxide Idle (g/kg fuel)
- 40.07
- Carbon Monoxide Unitary Average (g/kN)
- 88.9
- Carbon Monoxide Unitary Characteristic (g/kN)
- 109.12
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 92.5
- NOx Take Off (g/kg fuel)
- 16.1
- NOx Climb Out (g/kg fuel)
- 14.01
- NOx Approach (g/kg fuel)
- 7.12
- NOx Idle (g/kg fuel)
- 4.17
- NOx Unitary Average (g/kN)
- 38.38
- NOx Unitary Characteristic (g/kN)
- 44.49
- NOx Unitaryto Standard (% of limit)
- 58.7
- NOx Unitaryto CAEP2 (% of limit)
- 73.4
- NOx Unitaryto CAEP4 (% of limit)
- 75.4
- NOx Unitaryto CAEP6 (% of limit)
- 76.4
- NOx Unitaryto CAEP8 (% of limit)
- 81.7
- NOx LTO (g)
- 1333
- Smoke Take Off (SN)
- 0.01
- Smoke Climb Out (SN)
- 0.01
- Smoke Approach (SN)
- 0.01
- Smoke Idle (SN)
- 0.01
- Smoke Max (SN)
- 0.01
- Smoke Characteristic (SN)
- 0.01
- Smoke Characteristicto Regulatory (% of limit)
- 0
- Fuel Flow Take Off (kg/s)
- 0.3805
- Fuel Flow Climbout (kg/s)
- 0.3163
- Fuel Flow Approach (kg/s)
- 0.1125
- Fuel Flow Idle (kg/s)
- 0.0459
- Fuel LTO (kg)
- 156
- Carbon Monoxide LTO (g)
- 3088
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 9.8482
- nvPME Imass Climb Out (mg/kg)
- 34.8851
- nvPME Imass Idle (mg/kg)
- 18.4055
- nvPME Imass Max (mg/kg)
- 43.1427
- nvPME Imass Take Off (mg/kg)
- 43.1427
- nvPME Inum Approach (#/kg)
- 325901100000000
- nvPME Inum Climb Out (#/kg)
- 309219000000000
- nvPME Inum Idle (#/kg)
- 638163000000000
- nvPME Inum Max (#/kg)
- 638163000000000
- nvPME Inum Take Off (#/kg)
- 282685700000000
- nvPMLTO Mass (mg)
- 3907.795
- nvPMLTO Mass Per Thrust (mg/kN)
- 155.2
- nvPMLTO Mass To CAEP11 (% of limit)
- 15.4
- nvPMLTO Number (#)
- 76863340000000000
- nvPMLTO Number Per Thrust (#/kN)
- 3050000000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 25.3
- nvPM Mass Concentration Characteristic (mg/m³)
- 260
- nvPM Mass Concentration Max (mg/m³)
- 202.0917
- nvPM Mass Concentration To CAEP10 (% of limit)
- 2.1