Compare reaction turbines
All reaction turbines
|
PW1525G
✕
|
PW1923G-A
✕
|
| EASA ID |
16PW110 |
01P20PW190 |
| Aircraft Engine Manufacturer |
Pratt & Whitney |
Pratt & Whitney |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A |
Jet A |
| Geared Fan |
Yes |
Yes |
| Combustion Chamber |
TALON X |
TALON X, Block-C |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
11.05 |
11.16 |
| Overall Pressure Ratio |
38.67 |
37.74 |
| Maximum Takeoff Thrust (kN) |
108.53 |
105.93 |
| Hydrocarbon Take Off (g/kg fuel) |
0.1 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.1 |
0 |
| Hydrocarbon Approach (g/kg fuel) |
0.1 |
0.1 |
| Hydrocarbon Idle (g/kg fuel) |
0.1 |
0.1 |
| Hydrocarbon Unitary Average (g/kN) |
0.3 |
0.2 |
| Hydrocarbon Unitary Range (g/kN) |
0.2-0.4 |
0.1-0.3 |
| Hydrocarbon Unitary Characteristic (g/kN) |
0.4 |
0.3 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
2 |
2 |
| Hydrocarbon LTO (g) |
30 |
19 |
| Carbon Monoxide Take Off (g/kg fuel) |
0 |
0 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.1 |
0 |
| Carbon Monoxide Approach (g/kg fuel) |
1.6 |
2.3 |
| Carbon Monoxide Idle (g/kg fuel) |
13 |
18.4 |
| Carbon Monoxide Unitary Average (g/kN) |
15.1 |
21.3 |
| Carbon Monoxide Unitary Range (g/kN) |
14.6-15.5 |
21.1-21.5 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
16.3 |
26.1 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
13.8 |
22 |
| NOx Take Off (g/kg fuel) |
28.1 |
24.2 |
| NOx Climb Out (g/kg fuel) |
21.2 |
19.3 |
| NOx Approach (g/kg fuel) |
11.1 |
10.2 |
| NOx Idle (g/kg fuel) |
6.1 |
5.7 |
| NOx Unitary Average (g/kN) |
37.6 |
34 |
| NOx Unitary Range (g/kN) |
36.5-38.3 |
33.7-34.2 |
| NOx Unitary Characteristic (g/kN) |
39.8 |
39.4 |
| NOx Unitaryto Standard (% of limit) |
33.9 |
34 |
| NOx Unitaryto CAEP2 (% of limit) |
42.4 |
43 |
| NOx Unitaryto CAEP4 (% of limit) |
47.2 |
48 |
| NOx Unitaryto CAEP6 (% of limit) |
52.2 |
53 |
| NOx Unitaryto CAEP8 (% of limit) |
59 |
60 |
| NOx LTO (g) |
4125 |
3599 |
| Smoke Take Off (SN) |
3.4 |
3.1 |
| Smoke Climb Out (SN) |
2.8 |
1.8 |
| Smoke Approach (SN) |
2.4 |
0.8 |
| Smoke Idle (SN) |
2.5 |
0.5 |
| Smoke Max (SN) |
3.8 |
3.1 |
| Smoke Range (SN) |
1.7-5.7 |
2.7-3.9 |
| Smoke Characteristic (SN) |
4.1 |
4 |
| Smoke Characteristicto Regulatory (% of limit) |
17.7 |
17 |
| Fuel Flow Take Off (kg/s) |
0.79 |
0.76 |
| Fuel Flow Climbout (kg/s) |
0.65 |
0.63 |
| Fuel Flow Approach (kg/s) |
0.23 |
0.22 |
| Fuel Flow Idle (kg/s) |
0.08 |
0.07 |
| Fuel LTO (kg) |
299 |
284.9 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
1719 |
2256 |
| Emissions Data Status |
C |
C |
| Emissions Data Superseded |
|
Yes |
| Emissions Superseded By |
|
04P20PW203 |
| Engine Status |
Out of production |
|
| NOx Compliance Demonstration |
2.3.2 e) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
0.2296 |
| nvPME Imass Climb Out (mg/kg) |
|
7.2769 |
| nvPME Imass Idle (mg/kg) |
|
0.5905 |
| nvPME Imass Max (mg/kg) |
|
12.3906 |
| nvPME Imass Take Off (mg/kg) |
|
12.3906 |
| nvPME Inum Approach (#/kg) |
|
13970460000000 |
| nvPME Inum Climb Out (#/kg) |
|
187373700000000 |
| nvPME Inum Idle (#/kg) |
|
73282520000000 |
| nvPME Inum Max (#/kg) |
|
202490300000000 |
| nvPME Inum Take Off (#/kg) |
|
193519900000000 |
| nvPMLTO Mass (mg) |
|
1084.455 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
14.23 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
2.7 |
| nvPMLTO Number (#) |
|
31072010000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
407720000000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
6.4 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
402.5 |
| nvPM Mass Concentration Max (mg/m³) |
|
312.7 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
6.3 |