D-30KP-2

Turbofan · Aviadvigatel
Reaction Turbines
Maximum Takeoff Thrust
117.6 kN
Bypass Ratio
2.2
Overall Pressure Ratio
19.45
Fuel Flow Take Off
1.67 kg/s
NOx Unitaryto CAEP8
140.4 % 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 —
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 2.2 Overall Pressure Ratio 19.45 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
D-30KU Aviadvigatel 112.7 2.35 17.4 Compare
D-30KU-154 Aviadvigatel 107.5 2.3 17 Compare
Progress D-27 Ivchenko-Progress ZMKB 119 Compare
Rolls-Royce Pegasus Bristol Engine Company (Bristol) 106 Compare
Dobrynin RD-7 Dobrynin 103 Compare
Kuznetsov NK-88 Kuznetsov Design Bureau 103 Compare
All data (57 fields)
Name
D-30KP-2
EASA ID
1AA002
Aircraft Engine Manufacturer
Aviadvigatel
Aircraft Engine Type
Turbofan
Fuel
TS-1
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
2.2
Overall Pressure Ratio
19.45
Maximum Takeoff Thrust (kN)
117.6
Hydrocarbon Take Off (g/kg fuel)
0.7
Hydrocarbon Climb Out (g/kg fuel)
0.8
Hydrocarbon Approach (g/kg fuel)
2.7
Hydrocarbon Idle (g/kg fuel)
13.3
Hydrocarbon Unitary Average (g/kN)
41.4
Hydrocarbon Unitary Sigma (g/kN)
8.6
Hydrocarbon Unitary Characteristic (g/kN)
47.2
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
241
Hydrocarbon LTO (g)
4874
Carbon Monoxide Take Off (g/kg fuel)
2.2
Carbon Monoxide Climb Out (g/kg fuel)
2.8
Carbon Monoxide Approach (g/kg fuel)
15.4
Carbon Monoxide Idle (g/kg fuel)
62.4
Carbon Monoxide Unitary Average (g/kN)
195
Carbon Monoxide Unitary SD (g/kN)
11.1
Carbon Monoxide Unitary Characteristic (g/kN)
208.6
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
176.8
NOx Take Off (g/kg fuel)
16.5
NOx Climb Out (g/kg fuel)
13.5
NOx Approach (g/kg fuel)
6.3
NOx Idle (g/kg fuel)
3.3
NOx Unitary Average (g/kN)
47.1
NOx Unitary SD (g/kN)
6.6
NOx Unitary Characteristic (g/kN)
49.5
NOx Unitaryto Standard (% of limit)
62.7
NOx Unitaryto CAEP2 (% of limit)
78.4
NOx Unitaryto CAEP4 (% of limit)
98.8
NOx Unitaryto CAEP6 (% of limit)
112.2
NOx Unitaryto CAEP8 (% of limit)
140.4
NOx LTO (g)
5510
Smoke Take Off (SN)
17.5
Smoke Climb Out (SN)
19.5
Smoke Approach (SN)
16
Smoke Idle (SN)
6.5
Smoke Max (SN)
19.5
Smoke Characteristic (SN)
25.1
Smoke Characteristicto Regulatory (% of limit)
110.9
Fuel Flow Take Off (kg/s)
1.67
Fuel Flow Climbout (kg/s)
1.42
Fuel Flow Approach (kg/s)
0.49
Fuel Flow Idle (kg/s)
0.21
Fuel LTO (kg)
703
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
22932
Emissions Data Status
R
Engine Status
Out of production