| EASA ID |
|
1AA002 |
| Aircraft Engine Manufacturer |
Ivchenko-Progress ZMKB |
Aviadvigatel |
| Aircraft Engine Type |
Open-rotor |
Turbofan |
| 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 |
Yes |
No |
| Combustion Chamber |
Annular combustion chamber |
|
| Afterburner |
No |
No |
| Streams |
1 |
2 |
| Bypass Ratio |
|
2.2 |
| Overall Pressure Ratio |
|
19.45 |
| Maximum Takeoff Thrust (kN) |
119 |
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 |
| 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 |
|