Compare reaction turbines
All reaction turbines
|
PW1923G-A
✕
|
| EASA ID |
04P20PW203 |
| Aircraft Engine Manufacturer |
Pratt & Whitney |
| Aircraft Engine Type |
Turbofan |
| Fuel |
Jet A |
| Geared Fan |
Yes |
| Combustion Chamber |
TALON X, Block-C |
| Afterburner |
No |
| Streams |
2 |
| Bypass Ratio |
11.16 |
| Overall Pressure Ratio |
37.74 |
| Maximum Takeoff Thrust (kN) |
105.93 |
| Hydrocarbon Take Off (g/kg fuel) |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0 |
| Hydrocarbon Approach (g/kg fuel) |
0.1 |
| Hydrocarbon Idle (g/kg fuel) |
0.1 |
| Hydrocarbon Unitary Average (g/kN) |
0.2 |
| Hydrocarbon Unitary Range (g/kN) |
0.1-0.3 |
| Hydrocarbon Unitary Characteristic (g/kN) |
0.3 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
2 |
| Hydrocarbon LTO (g) |
19 |
| Carbon Monoxide Take Off (g/kg fuel) |
0 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0 |
| Carbon Monoxide Approach (g/kg fuel) |
2.3 |
| Carbon Monoxide Idle (g/kg fuel) |
18.4 |
| Carbon Monoxide Unitary Average (g/kN) |
21.3 |
| Carbon Monoxide Unitary Range (g/kN) |
21.1-21.5 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
26.1 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
22 |
| NOx Take Off (g/kg fuel) |
24.2 |
| NOx Climb Out (g/kg fuel) |
19.3 |
| NOx Approach (g/kg fuel) |
10.2 |
| NOx Idle (g/kg fuel) |
5.7 |
| NOx Unitary Average (g/kN) |
34 |
| NOx Unitary Range (g/kN) |
33.7-34.2 |
| NOx Unitary Characteristic (g/kN) |
39.4 |
| NOx Unitaryto Standard (% of limit) |
34 |
| NOx Unitaryto CAEP2 (% of limit) |
43 |
| NOx Unitaryto CAEP4 (% of limit) |
48 |
| NOx Unitaryto CAEP6 (% of limit) |
53 |
| NOx Unitaryto CAEP8 (% of limit) |
60 |
| NOx LTO (g) |
3599 |
| Smoke Take Off (SN) |
3.1 |
| Smoke Climb Out (SN) |
1.8 |
| Smoke Approach (SN) |
0.8 |
| Smoke Idle (SN) |
0.5 |
| Smoke Max (SN) |
3.1 |
| Smoke Range (SN) |
2.7-3.9 |
| Smoke Characteristic (SN) |
4 |
| Smoke Characteristicto Regulatory (% of limit) |
17 |
| Fuel Flow Take Off (kg/s) |
0.76 |
| Fuel Flow Climbout (kg/s) |
0.63 |
| Fuel Flow Approach (kg/s) |
0.22 |
| Fuel Flow Idle (kg/s) |
0.07 |
| Fuel LTO (kg) |
284.9 |
| Fuel Venting Compliant |
Yes |
| Carbon Monoxide LTO (g) |
2256 |
| Emissions Data Status |
C |
| NOx Compliance Demonstration |
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 |