AE3007A1

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
34.91 kN
Bypass Ratio
4.77
Overall Pressure Ratio
17.97
Fuel Flow Take Off
0.3826 kg/s
NOx Unitaryto CAEP8
84.2 % 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 17.97 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007A1 Rolls-Royce 34.91 4.77 17.97 Compare
AE3007A1/1 Rolls-Royce 34.74 4.77 17.9 Compare
AE3007A1P Rolls-Royce 34.74 4.77 17.9 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
AE3007A1
EASA ID
6AL005
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
17.97
Maximum Takeoff Thrust (kN)
34.91
Hydrocarbon Take Off (g/kg fuel)
0.221
Hydrocarbon Climb Out (g/kg fuel)
0.257
Hydrocarbon Approach (g/kg fuel)
0.655
Hydrocarbon Idle (g/kg fuel)
3.818
Hydrocarbon Unitary Average (g/kN)
8.78
Hydrocarbon Unitary Characteristic (g/kN)
11.42
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
58.3
Hydrocarbon LTO (g)
307
Carbon Monoxide Take Off (g/kg fuel)
0.77
Carbon Monoxide Climb Out (g/kg fuel)
0.96
Carbon Monoxide Approach (g/kg fuel)
3.91
Carbon Monoxide Idle (g/kg fuel)
23.73
Carbon Monoxide Unitary Average (g/kN)
53.38
Carbon Monoxide Unitary Characteristic (g/kN)
60.82
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
51.5
NOx Take Off (g/kg fuel)
19.66
NOx Climb Out (g/kg fuel)
16.63
NOx Approach (g/kg fuel)
7.1
NOx Idle (g/kg fuel)
3.47
NOx Unitary Average (g/kN)
41.71
NOx Unitary Characteristic (g/kN)
45.87
NOx Unitaryto Standard (% of limit)
60.4
NOx Unitaryto CAEP2 (% of limit)
75.5
NOx Unitaryto CAEP4 (% of limit)
77.6
NOx Unitaryto CAEP6 (% of limit)
78.7
NOx Unitaryto CAEP8 (% of limit)
84.2
NOx LTO (g)
1456
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)
0.3826
Fuel Flow Climbout (kg/s)
0.318
Fuel Flow Approach (kg/s)
0.113
Fuel Flow Idle (kg/s)
0.0461
Fuel LTO (kg)
157
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
1865
Emissions Data Status
R
Engine Status
Out of production