AE3007A1P

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
34.74 kN
Bypass Ratio
4.77
Overall Pressure Ratio
17.9
Fuel Flow Take Off
0.3806 kg/s
NOx Unitaryto CAEP8
84 % 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 1
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

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007A1/1 Rolls-Royce 34.74 4.77 17.9 Compare
AE3007A1P Rolls-Royce 34.74 4.77 17.9 Compare
AE3007A1 Rolls-Royce 34.91 4.77 17.97 Compare
AE3007A1 series Rolls-Royce 33.73 4.76 17.81 Compare
AE3007A1/3 Rolls-Royce 33.05 4.81 17.22 Compare
AE3007A3 Rolls-Royce 33 4.72 17.2 Compare
All data (55 fields)
Name
AE3007A1P
EASA ID
6AL014
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
Type 1
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)
0.222
Hydrocarbon Climb Out (g/kg fuel)
0.258
Hydrocarbon Approach (g/kg fuel)
0.658
Hydrocarbon Idle (g/kg fuel)
3.85
Hydrocarbon Unitary Average (g/kN)
8.88
Hydrocarbon Unitary Characteristic (g/kN)
11.55
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
58.9
Hydrocarbon LTO (g)
308
Carbon Monoxide Take Off (g/kg fuel)
0.77
Carbon Monoxide Climb Out (g/kg fuel)
0.97
Carbon Monoxide Approach (g/kg fuel)
3.93
Carbon Monoxide Idle (g/kg fuel)
23.8
Carbon Monoxide Unitary Average (g/kN)
53.75
Carbon Monoxide Unitary Characteristic (g/kN)
61.24
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
51.9
NOx Take Off (g/kg fuel)
19.57
NOx Climb Out (g/kg fuel)
16.56
NOx Approach (g/kg fuel)
7.07
NOx Idle (g/kg fuel)
3.47
NOx Unitary Average (g/kN)
41.57
NOx Unitary Characteristic (g/kN)
45.71
NOx Unitaryto Standard (% of limit)
60.3
NOx Unitaryto CAEP2 (% of limit)
75.4
NOx Unitaryto CAEP4 (% of limit)
77.9
NOx Unitaryto CAEP6 (% of limit)
78.5
NOx Unitaryto CAEP8 (% of limit)
84
NOx LTO (g)
1444
Smoke Take Off (SN)
1
Smoke Climb Out (SN)
0.01
Smoke Approach (SN)
0.01
Smoke Idle (SN)
0.01
Smoke Max (SN)
1
Smoke Characteristic (SN)
1.17
Smoke Characteristicto Regulatory (% of limit)
3.7
Fuel Flow Take Off (kg/s)
0.3806
Fuel Flow Climbout (kg/s)
0.3163
Fuel Flow Approach (kg/s)
0.1126
Fuel Flow Idle (kg/s)
0.046
Fuel LTO (kg)
157
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
1867
Emissions Data Status
C
Engine Status
Out of production