Maximum Takeoff Thrust
33.05 kN
Overall Pressure Ratio
17.22
Fuel Flow Take Off
0.3589 kg/s
NOx Unitaryto CAEP8
80.7 % 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
4.81 |
Overall Pressure Ratio
17.22 |
Afterburner
No |
Pictures
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All data (74 fields)
- Name
- AE3007A1/3
- EASA ID
- 01P06AL030
- 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
- 4.81
- Overall Pressure Ratio
- 17.22
- Maximum Takeoff Thrust (kN)
- 33.05
- 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)
- 3.81
- Hydrocarbon Unitary Average (g/kN)
- 8.15
- Hydrocarbon Unitary Characteristic (g/kN)
- 12.55
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 64
- Hydrocarbon LTO (g)
- 269
- Carbon Monoxide Take Off (g/kg fuel)
- 0.5
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.5
- Carbon Monoxide Approach (g/kg fuel)
- 7.62
- Carbon Monoxide Idle (g/kg fuel)
- 38.47
- Carbon Monoxide Unitary Average (g/kN)
- 88.3
- Carbon Monoxide Unitary Characteristic (g/kN)
- 108.38
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 91.8
- NOx Take Off (g/kg fuel)
- 15.42
- NOx Climb Out (g/kg fuel)
- 13.49
- NOx Approach (g/kg fuel)
- 6.93
- NOx Idle (g/kg fuel)
- 4.27
- NOx Unitary Average (g/kN)
- 37.66
- NOx Unitary Characteristic (g/kN)
- 43.65
- NOx Unitaryto Standard (% of limit)
- 58.6
- NOx Unitaryto CAEP2 (% of limit)
- 73.3
- NOx Unitaryto CAEP4 (% of limit)
- 74.9
- NOx Unitaryto CAEP6 (% of limit)
- 75.7
- NOx Unitaryto CAEP8 (% of limit)
- 80.7
- NOx LTO (g)
- 1245
- 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)
- 0.3589
- Fuel Flow Climbout (kg/s)
- 0.2999
- Fuel Flow Approach (kg/s)
- 0.1077
- Fuel Flow Idle (kg/s)
- 0.0449
- Fuel LTO (kg)
- 151
- Carbon Monoxide LTO (g)
- 2919
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 9.9862
- nvPME Imass Climb Out (mg/kg)
- 32.8059
- nvPME Imass Idle (mg/kg)
- 18.7923
- nvPME Imass Max (mg/kg)
- 41.3455
- nvPME Imass Take Off (mg/kg)
- 41.3455
- nvPME Inum Approach (#/kg)
- 332255800000000
- nvPME Inum Climb Out (#/kg)
- 312347000000000
- nvPME Inum Idle (#/kg)
- 658652900000000
- nvPME Inum Max (#/kg)
- 658652900000000
- nvPME Inum Take Off (#/kg)
- 293709900000000
- nvPMLTO Mass (mg)
- 3696.384
- nvPMLTO Mass Per Thrust (mg/kN)
- 153.1
- nvPMLTO Mass To CAEP11 (% of limit)
- 15
- nvPMLTO Number (#)
- 76873510000000000
- nvPMLTO Number Per Thrust (#/kN)
- 3180000000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 26.1
- nvPM Mass Concentration Characteristic (mg/m³)
- 242
- nvPM Mass Concentration Max (mg/m³)
- 188.3518
- nvPM Mass Concentration To CAEP10 (% of limit)
- 1.9