| EASA ID |
1AA002 |
|
| Aircraft Engine Manufacturer |
Aviadvigatel |
Ivchenko-Progress ZMKB |
| Aircraft Engine Type |
Turbofan |
Open-rotor |
| Dry Weight (kg) |
|
1650 |
| Diameter (mm) |
|
970 |
| Length (mm) |
|
4205 |
| Wikipedia Article (URL) |
|
en.wikipedia.org/wiki/Progress_D-27 |
| Fuel |
TS-1 |
|
| Geared Fan |
No |
Yes |
| Combustion Chamber |
|
Annular combustion chamber |
| Afterburner |
No |
No |
| Streams |
2 |
1 |
| Bypass Ratio |
2.2 |
|
| Overall Pressure Ratio |
19.45 |
|
| Maximum Takeoff Thrust (kN) |
117.6 |
119 |
| 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 |
|
| Compressor Description |
|
5-stage axial flow low-pressure compressor (LPC); high-pressure compressor (HPC) with 2 axial stages and 1 centrifugal stage |
| Emissions Data Status |
R |
|
| Engine Status |
Out of production |
|
| Turbine Description |
|
1-stage high-pressure turbine (HPT), 1-stage low-pressure turbine (LPT), 4-stage free power turbine |