Compare reaction turbines
All reaction turbines
|
PW308C BS 1047
✕
|
PW308C Build Spec 1289
✕
|
| EASA ID |
01P07PW146 |
14PW103 |
| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
Pratt & Whitney Canada |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A-1 |
Jet A-1 |
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular |
TALON II |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
4.1 |
4.1 |
| Overall Pressure Ratio |
20.7 |
21.07 |
| Maximum Takeoff Thrust (kN) |
31.15 |
31.15 |
| Hydrocarbon Take Off (g/kg fuel) |
0.09 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.1 |
0 |
| Hydrocarbon Approach (g/kg fuel) |
0.14 |
0 |
| Hydrocarbon Idle (g/kg fuel) |
5.94 |
0.39 |
| Hydrocarbon Unitary Average (g/kN) |
13.63 |
1 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
0.7 |
| Hydrocarbon Unitary Range (g/kN) |
12.5-15.2 |
0.2-1.5 |
| Hydrocarbon Unitary Characteristic (g/kN) |
15.9 |
1.1 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
81.1 |
5.6 |
| Hydrocarbon LTO (g) |
425 |
30 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.81 |
0.5 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.97 |
0.57 |
| Carbon Monoxide Approach (g/kg fuel) |
5.23 |
4.18 |
| Carbon Monoxide Idle (g/kg fuel) |
42.3 |
37.05 |
| Carbon Monoxide Unitary Average (g/kN) |
101.54 |
95.1 |
| Carbon Monoxide Unitary SD (g/kN) |
|
5.9 |
| Carbon Monoxide Unitary Range (g/kN) |
99-105.9 |
88.4-99.8 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
109.8 |
102.8 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
93.1 |
87.1 |
| NOx Take Off (g/kg fuel) |
18.45 |
19.1 |
| NOx Climb Out (g/kg fuel) |
15.99 |
14.96 |
| NOx Approach (g/kg fuel) |
7.83 |
6.8 |
| NOx Idle (g/kg fuel) |
3.63 |
3.53 |
| NOx Unitary Average (g/kN) |
45.38 |
43.7 |
| NOx Unitary SD (g/kN) |
|
1.1 |
| NOx Unitary Range (g/kN) |
45-45.92 |
42.4-44.3 |
| NOx Unitary Characteristic (g/kN) |
48.1 |
46.3 |
| NOx Unitaryto Standard (% of limit) |
59.1 |
56.4 |
| NOx Unitaryto CAEP2 (% of limit) |
73.9 |
70.5 |
| NOx Unitaryto CAEP4 (% of limit) |
74.9 |
71.5 |
| NOx Unitaryto CAEP6 (% of limit) |
75.5 |
72 |
| NOx Unitaryto CAEP8 (% of limit) |
80.1 |
76.3 |
| NOx LTO (g) |
1414 |
1359 |
| Smoke Take Off (SN) |
4.8 |
6.6 |
| Smoke Climb Out (SN) |
3.9 |
6.8 |
| Smoke Approach (SN) |
1.4 |
2.2 |
| Smoke Idle (SN) |
1.3 |
5.7 |
| Smoke Max (SN) |
7.6 |
8.2 |
| Smoke Sigma (SN) |
|
0.7 |
| Smoke Range (SN) |
5.3-9.4 |
7.5-8.9 |
| Smoke Characteristic (SN) |
8.3 |
9.1 |
| Smoke Characteristicto Regulatory (% of limit) |
25.5 |
27.9 |
| Fuel Flow Take Off (kg/s) |
0.3669 |
0.37 |
| Fuel Flow Climbout (kg/s) |
0.3047 |
0.307 |
| Fuel Flow Approach (kg/s) |
0.1237 |
0.116 |
| Fuel Flow Idle (kg/s) |
0.0448 |
0.049 |
| Fuel LTO (kg) |
155 |
160 |
| Fuel Venting Compliant |
|
Yes |
| Carbon Monoxide LTO (g) |
3163 |
2961 |
| Emissions Data Status |
C |
C/R |
| Emissions Data Superseded |
|
Yes |
| Emissions Superseded By |
|
01P14PW147 |
| Engine Status |
Out of production |
|
| NOx Compliance Demonstration |
2.3.2 d) |
2.3.2 d) |
| nvPME Imass Approach (mg/kg) |
48.6296 |
|
| nvPME Imass Climb Out (mg/kg) |
169.9858 |
|
| nvPME Imass Idle (mg/kg) |
67.2158 |
|
| nvPME Imass Max (mg/kg) |
223.969 |
|
| nvPME Imass Take Off (mg/kg) |
223.969 |
|
| nvPME Inum Approach (#/kg) |
472672800000000 |
|
| nvPME Inum Climb Out (#/kg) |
942407400000000 |
|
| nvPME Inum Idle (#/kg) |
1026700000000000 |
|
| nvPME Inum Max (#/kg) |
1026700000000000 |
|
| nvPME Inum Take Off (#/kg) |
907645200000000 |
|
| nvPMLTO Mass (mg) |
16425.1 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
733.0457 |
|
| nvPMLTO Number (#) |
137608200000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
6141401000000000 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
1420.57 |
|
| nvPM Mass Concentration Max (mg/m³) |
1103.641 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
10.5229 |
|