D-30KU

Turbofan · Aviadvigatel

Reaction Turbines

Maximum Takeoff Thrust

112.7 kN

Bypass Ratio

2.35

Overall Pressure Ratio

17.4

Fuel Flow Take Off

1.52 kg/s

NOx Unitaryto CAEP8

135.3 % 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 —
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 2.35	Overall Pressure Ratio 17.4	Afterburner No

Pictures

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All data (53 fields)

Name: D-30KU
EASA ID: 1AA003
Aircraft Engine Manufacturer: Aviadvigatel
Aircraft Engine Type: Turbofan
Fuel: TS-1
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 2.35
Overall Pressure Ratio: 17.4
Maximum Takeoff Thrust (kN): 112.7
Hydrocarbon Take Off (g/kg fuel): 0.3
Hydrocarbon Climb Out (g/kg fuel): 0.4
Hydrocarbon Approach (g/kg fuel): 1.2
Hydrocarbon Idle (g/kg fuel): 10.5
Hydrocarbon Unitary Average (g/kN): 33.3
Hydrocarbon Unitary Sigma (g/kN): 6.55
Hydrocarbon Unitary Characteristic (g/kN): 37.4
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 191
Hydrocarbon LTO (g): 3753
Carbon Monoxide Take Off (g/kg fuel): 2.8
Carbon Monoxide Climb Out (g/kg fuel): 3.7
Carbon Monoxide Approach (g/kg fuel): 11.8
Carbon Monoxide Idle (g/kg fuel): 54
Carbon Monoxide Unitary Average (g/kN): 180.5
Carbon Monoxide Unitary SD (g/kN): 33.4
Carbon Monoxide Unitary Characteristic (g/kN): 191.7
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 162.5
NOx Take Off (g/kg fuel): 16.3
NOx Climb Out (g/kg fuel): 12.6
NOx Approach (g/kg fuel): 5.1
NOx Idle (g/kg fuel): 2.7
NOx Unitary Average (g/kN): 41.9
NOx Unitary SD (g/kN): 3.15
NOx Unitary Characteristic (g/kN): 43.8
NOx Unitaryto Standard (% of limit): 58.6
NOx Unitaryto CAEP2 (% of limit): 73.2
NOx Unitaryto CAEP4 (% of limit): 93.5
NOx Unitaryto CAEP6 (% of limit): 106.3
NOx Unitaryto CAEP8 (% of limit): 135.3
NOx LTO (g): 4720
Smoke Max (SN): 22.9
Smoke Characteristic (SN): 29.5
Smoke Characteristicto Regulatory (% of limit): 128.7
Fuel Flow Take Off (kg/s): 1.52
Fuel Flow Climbout (kg/s): 1.3
Fuel Flow Approach (kg/s): 0.5
Fuel Flow Idle (kg/s): 0.215
Fuel LTO (kg): 691
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 20341
Emissions Data Status: R
Engine Status: Out of production