AE3007C

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
29.62 kN
Bypass Ratio
5.2
Overall Pressure Ratio
15.8
Fuel Flow Take Off
0.301 kg/s
NOx Unitaryto CAEP8
73.2 % 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 5.2 Overall Pressure Ratio 15.8 Afterburner No

Pictures

No pictures yet for this family.

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007C Rolls-Royce 29.62 5.2 15.8 Compare
ALF 502R-3 Textron Lycoming 29.8 5.7 11.4 Compare
LF507-1F, -1H Textron Lycoming 31 5.1 13 Compare
AE3007C1 Rolls-Royce 31.46 5.1 16.58 Compare
ALF 502R-5 Textron Lycoming 31 5.6 12 Compare
HTF7500E (AS907-3-1E-A1) Honeywell 29.4 4.2 21.05 Compare
All data (56 fields)
Name
AE3007C
EASA ID
6AL021
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
5.2
Overall Pressure Ratio
15.8
Maximum Takeoff Thrust (kN)
29.62
Hydrocarbon Take Off (g/kg fuel)
0.254
Hydrocarbon Climb Out (g/kg fuel)
0.291
Hydrocarbon Approach (g/kg fuel)
0.696
Hydrocarbon Idle (g/kg fuel)
4.953
Hydrocarbon Unitary Average (g/kN)
10.79
Hydrocarbon Unitary Characteristic (g/kN)
14.04
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
71.6
Hydrocarbon LTO (g)
320
Carbon Monoxide Take Off (g/kg fuel)
0.94
Carbon Monoxide Climb Out (g/kg fuel)
1.16
Carbon Monoxide Approach (g/kg fuel)
4.28
Carbon Monoxide Idle (g/kg fuel)
26.32
Carbon Monoxide Unitary Average (g/kN)
57.18
Carbon Monoxide Unitary Characteristic (g/kN)
65.15
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
55.2
NOx Take Off (g/kg fuel)
16.88
NOx Climb Out (g/kg fuel)
14.57
NOx Approach (g/kg fuel)
6.78
NOx Idle (g/kg fuel)
3.36
NOx Unitary Average (g/kN)
35.47
NOx Unitary Characteristic (g/kN)
39
NOx Unitaryto Standard (% of limit)
54.5
NOx Unitaryto CAEP2 (% of limit)
68.1
NOx Unitaryto CAEP4 (% of limit)
68.8
NOx Unitaryto CAEP6 (% of limit)
69.1
NOx Unitaryto CAEP8 (% of limit)
73.2
NOx LTO (g)
1050
Smoke Take Off (SN)
1
Smoke Climb Out (SN)
0.01
Smoke Approach (SN)
0.01
Smoke Idle (SN)
0.01
Smoke Max (SN)
0
Smoke Characteristic (SN)
1.17
Smoke Characteristicto Regulatory (% of limit)
3.5
Fuel Flow Take Off (kg/s)
0.301
Fuel Flow Climbout (kg/s)
0.2527
Fuel Flow Approach (kg/s)
0.0943
Fuel Flow Idle (kg/s)
0.0377
Fuel LTO (kg)
127
Carbon Monoxide LTO (g)
1695
Emissions Data Status
C
Emissions Data Superseded
Yes
Emissions Superseded By
8AL025
Engine Status
Out of production