AE3007C1

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

31.46 kN

Bypass Ratio

5.1

Overall Pressure Ratio

16.58

Fuel Flow Take Off

0.3222 kg/s

NOx Unitaryto CAEP8

76.4 % 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 5.1	Overall Pressure Ratio 16.58	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
AE3007C1	Rolls-Royce	31.46	5.1	16.58	Compare
LF507-1F, -1H	Textron Lycoming	31	5.1	13	Compare
AE3007C2	Rolls-Royce	32.73	4.99	17.44	Compare
ALF 502L-2	Textron Lycoming	33.4	5.1	13.15	Compare
ALF 502R-5	Textron Lycoming	31	5.6	12	Compare
AE3007C	Rolls-Royce	29.62	5.2	15.8	Compare

All data (54 fields)

Name: AE3007C1
EASA ID: 6AL023
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: 5.1
Overall Pressure Ratio: 16.58
Maximum Takeoff Thrust (kN): 31.46
Hydrocarbon Take Off (g/kg fuel): 0.24
Hydrocarbon Climb Out (g/kg fuel): 0.277
Hydrocarbon Approach (g/kg fuel): 0.661
Hydrocarbon Idle (g/kg fuel): 4.837
Hydrocarbon Unitary Average (g/kN): 10.95
Hydrocarbon Unitary Characteristic (g/kN): 14.25
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 72.7
Hydrocarbon LTO (g): 344
Carbon Monoxide Take Off (g/kg fuel): 0.87
Carbon Monoxide Climb Out (g/kg fuel): 1.07
Carbon Monoxide Approach (g/kg fuel): 3.96
Carbon Monoxide Idle (g/kg fuel): 26.04
Carbon Monoxide Unitary Average (g/kN): 58.61
Carbon Monoxide Unitary Characteristic (g/kN): 66.78
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 56.6
NOx Take Off (g/kg fuel): 17.9
NOx Climb Out (g/kg fuel): 15.35
NOx Approach (g/kg fuel): 7.05
NOx Idle (g/kg fuel): 3.37
NOx Unitary Average (g/kN): 37.36
NOx Unitary Characteristic (g/kN): 41.08
NOx Unitaryto Standard (% of limit): 56.2
NOx Unitaryto CAEP2 (% of limit): 70.2
NOx Unitaryto CAEP4 (% of limit): 71.4
NOx Unitaryto CAEP6 (% of limit): 71.9
NOx Unitaryto CAEP8 (% of limit): 76.4
NOx LTO (g): 1175
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): 3.6
Fuel Flow Take Off (kg/s): 0.3222
Fuel Flow Climbout (kg/s): 0.2689
Fuel Flow Approach (kg/s): 0.0991
Fuel Flow Idle (kg/s): 0.0418
Fuel LTO (kg): 138
Carbon Monoxide LTO (g): 1842
Emissions Data Status: C
Engine Status: Out of production