| EASA ID |
|
01P18PW153 |
| Aircraft Engine Manufacturer |
Ivchenko-Progress ZMKB |
Pratt & Whitney |
| 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 |
|
Jet A |
| Geared Fan |
Yes |
Yes |
| Combustion Chamber |
Annular combustion chamber |
TALON X, Block-C |
| Afterburner |
No |
No |
| Streams |
1 |
2 |
| Bypass Ratio |
|
12.28 |
| Overall Pressure Ratio |
|
31.66 |
| Maximum Takeoff Thrust (kN) |
119 |
120.43 |
| Hydrocarbon Take Off (g/kg fuel) |
|
0.02 |
| Hydrocarbon Climb Out (g/kg fuel) |
|
0.04 |
| Hydrocarbon Approach (g/kg fuel) |
|
0.02 |
| Hydrocarbon Idle (g/kg fuel) |
|
0.43 |
| Hydrocarbon Unitary Average (g/kN) |
|
0.51 |
| Hydrocarbon Unitary Characteristic (g/kN) |
|
0.6 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
|
3.1 |
| Hydrocarbon LTO (g) |
|
59 |
| Carbon Monoxide Take Off (g/kg fuel) |
|
0.22 |
| Carbon Monoxide Climb Out (g/kg fuel) |
|
0.3 |
| Carbon Monoxide Approach (g/kg fuel) |
|
5.36 |
| Carbon Monoxide Idle (g/kg fuel) |
|
27.93 |
| Carbon Monoxide Unitary Average (g/kN) |
|
32.43 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
|
35.07 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
|
30 |
| NOx Take Off (g/kg fuel) |
|
18.82 |
| NOx Climb Out (g/kg fuel) |
|
15.3 |
| NOx Approach (g/kg fuel) |
|
9.07 |
| NOx Idle (g/kg fuel) |
|
4.84 |
| NOx Unitary Average (g/kN) |
|
25.3 |
| NOx Unitary Characteristic (g/kN) |
|
27.29 |
| NOx Unitaryto Standard (% of limit) |
|
26 |
| NOx Unitaryto CAEP2 (% of limit) |
|
33 |
| NOx Unitaryto CAEP4 (% of limit) |
|
39 |
| NOx Unitaryto CAEP6 (% of limit) |
|
44 |
| NOx Unitaryto CAEP8 (% of limit) |
|
51 |
| NOx LTO (g) |
|
3096 |
| Smoke Take Off (SN) |
|
13.4 |
| Smoke Climb Out (SN) |
|
10.5 |
| Smoke Approach (SN) |
|
0.5 |
| Smoke Idle (SN) |
|
1.2 |
| Smoke Max (SN) |
|
13.4 |
| Smoke Characteristic (SN) |
|
14.8 |
| Smoke Characteristicto Regulatory (% of limit) |
|
66 |
| Fuel Flow Take Off (kg/s) |
|
0.8 |
| Fuel Flow Climbout (kg/s) |
|
0.67 |
| Fuel Flow Approach (kg/s) |
|
0.2322 |
| Fuel Flow Idle (kg/s) |
|
0.08 |
| Fuel LTO (kg) |
|
303 |
| Fuel Venting Compliant |
|
Yes |
| Carbon Monoxide LTO (g) |
|
3819 |
| 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 |
|
C |
| Engine Status |
|
Out of production |
| NOx Compliance Demonstration |
|
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
6.4464 |
| nvPME Imass Climb Out (mg/kg) |
|
32.0653 |
| nvPME Imass Idle (mg/kg) |
|
9.2971 |
| nvPME Imass Max (mg/kg) |
|
62.7674 |
| nvPME Imass Take Off (mg/kg) |
|
62.7674 |
| nvPME Inum Approach (#/kg) |
|
370765700000000 |
| nvPME Inum Climb Out (#/kg) |
|
676986000000000 |
| nvPME Inum Idle (#/kg) |
|
836628200000000 |
| nvPME Inum Max (#/kg) |
|
949866800000000 |
| nvPME Inum Take Off (#/kg) |
|
943036700000000 |
| nvPMLTO Mass (mg) |
|
6464.058 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
74.6043 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
17.8318 |
| nvPMLTO Number (#) |
|
216614100000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
2500032000000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
48.371 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
1856.632 |
| nvPM Mass Concentration Max (mg/m³) |
|
1442.417 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
30.7905 |
| Turbine Description |
1-stage high-pressure turbine (HPT), 1-stage low-pressure turbine (LPT), 4-stage free power turbine |
|