Compare reaction turbines
All reaction turbines
|
PW307D
✕
|
HTF7000 (AS907-1-1A)
✕
|
| EASA ID |
01P15PW144 |
11HN003 |
| Aircraft Engine Manufacturer |
Pratt & Whitney Canada |
Honeywell |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A-1 |
Jet A |
| Geared Fan |
No |
No |
| Combustion Chamber |
TALON II |
SABER-1 |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
4.2 |
4.2 |
| Overall Pressure Ratio |
21.44 |
21.95 |
| Maximum Takeoff Thrust (kN) |
29.91 |
30.62 |
| Hydrocarbon Take Off (g/kg fuel) |
0 |
0.05 |
| Hydrocarbon Climb Out (g/kg fuel) |
0 |
0.06 |
| Hydrocarbon Approach (g/kg fuel) |
0 |
0.12 |
| Hydrocarbon Idle (g/kg fuel) |
0.75 |
1.26 |
| Hydrocarbon Unitary Average (g/kN) |
1.8 |
3.27 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.5 |
0.64 |
| Hydrocarbon Unitary Range (g/kN) |
1.2-2.4 |
2.36-4.34 |
| Hydrocarbon Unitary Characteristic (g/kN) |
2.1 |
3.82 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
10.7 |
19.5 |
| Hydrocarbon LTO (g) |
54 |
100 |
| Carbon Monoxide Take Off (g/kg fuel) |
0 |
0.56 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.02 |
0.63 |
| Carbon Monoxide Approach (g/kg fuel) |
2.57 |
6.28 |
| Carbon Monoxide Idle (g/kg fuel) |
26.75 |
33.24 |
| Carbon Monoxide Unitary Average (g/kN) |
66.8 |
87.47 |
| Carbon Monoxide Unitary SD (g/kN) |
3.4 |
3.7 |
| Carbon Monoxide Unitary Range (g/kN) |
62.7-70.2 |
81.73-92.46 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
72.3 |
94.61 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
61.3 |
80.2 |
| NOx Take Off (g/kg fuel) |
20.61 |
17.9 |
| NOx Climb Out (g/kg fuel) |
15.44 |
16.17 |
| NOx Approach (g/kg fuel) |
7.85 |
8.81 |
| NOx Idle (g/kg fuel) |
4.32 |
3.91 |
| NOx Unitary Average (g/kN) |
46.6 |
45.39 |
| NOx Unitary SD (g/kN) |
3.5 |
2.26 |
| NOx Unitary Range (g/kN) |
43.4-51 |
39.54-47.24 |
| NOx Unitary Characteristic (g/kN) |
49.3 |
48.08 |
| NOx Unitaryto Standard (% of limit) |
59.4 |
64 |
| NOx Unitaryto CAEP2 (% of limit) |
74.3 |
71.6 |
| NOx Unitaryto CAEP4 (% of limit) |
75 |
72.5 |
| NOx Unitaryto CAEP6 (% of limit) |
75.4 |
73 |
| NOx Unitaryto CAEP8 (% of limit) |
79.8 |
77.3 |
| NOx LTO (g) |
1393 |
1388 |
| Smoke Take Off (SN) |
0.8 |
13.6 |
| Smoke Climb Out (SN) |
0.9 |
10.6 |
| Smoke Approach (SN) |
0 |
0.7 |
| Smoke Idle (SN) |
2 |
1.7 |
| Smoke Max (SN) |
2 |
13.6 |
| Smoke Sigma (SN) |
0.5 |
1.5 |
| Smoke Range (SN) |
1.4-2.5 |
9.2-13.6 |
| Smoke Characteristic (SN) |
2.2 |
15 |
| Smoke Characteristicto Regulatory (% of limit) |
6.7 |
45.7 |
| Fuel Flow Take Off (kg/s) |
0.3545 |
0.347 |
| Fuel Flow Climbout (kg/s) |
0.2769 |
0.288 |
| Fuel Flow Approach (kg/s) |
0.1115 |
0.104 |
| Fuel Flow Idle (kg/s) |
0.0462 |
0.048 |
| Fuel LTO (kg) |
150 |
152 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
1997 |
2678 |
| Emissions Data Status |
C |
C |
| Emissions Data Superseded |
Yes |
|
| Emissions Superseded By |
03P15PW193 |
|
| Engine Status |
|
Out of production |
| NOx Compliance Demonstration |
2.3.2 e) |
2.3.2 d) |
| nvPME Imass Approach (mg/kg) |
5.6523 |
|
| nvPME Imass Climb Out (mg/kg) |
38.7914 |
|
| nvPME Imass Idle (mg/kg) |
246.5516 |
|
| nvPME Imass Max (mg/kg) |
246.5516 |
|
| nvPME Imass Take Off (mg/kg) |
65.4134 |
|
| nvPME Inum Approach (#/kg) |
233847600000000 |
|
| nvPME Inum Climb Out (#/kg) |
636263000000000 |
|
| nvPME Inum Idle (#/kg) |
1880967000000000 |
|
| nvPME Inum Max (#/kg) |
1880967000000000 |
|
| nvPME Inum Take Off (#/kg) |
576002400000000 |
|
| nvPMLTO Mass (mg) |
19851.52 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
663.6134 |
|
| nvPMLTO Number (#) |
170174200000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
5688728000000000 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
1249.798 |
|
| nvPM Mass Concentration Max (mg/m³) |
970.968 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
8.9938 |
|