Compare reaction turbines
All reaction turbines
|
PW4060
✕
|
CF6-80C2B5F/B6F/B7F
✕
|
| EASA ID |
12PW101 |
07P27GE219 |
| Aircraft Engine Manufacturer |
Pratt & Whitney |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A |
Jet A |
| Geared Fan |
No |
No |
| Combustion Chamber |
Phase III |
LEC |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
4.7 |
4.9797 |
| Overall Pressure Ratio |
29.7 |
32.6879 |
| Maximum Takeoff Thrust (kN) |
266.9 |
267.0271 |
| Hydrocarbon Take Off (g/kg fuel) |
0.08 |
0.0445 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.06 |
0.0492 |
| Hydrocarbon Approach (g/kg fuel) |
0.1 |
0.0986 |
| Hydrocarbon Idle (g/kg fuel) |
11.63 |
1.7269 |
| Hydrocarbon Unitary Average (g/kN) |
14.15 |
2.1044 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
0.0815 |
| Hydrocarbon Unitary Range (g/kN) |
|
2.01-2.16 |
| Hydrocarbon Unitary Characteristic (g/kN) |
18.41 |
3.2411 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
93.9 |
16.5362 |
| Hydrocarbon LTO (g) |
3775.9 |
561.9426 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.58 |
0.1634 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.49 |
0.1311 |
| Carbon Monoxide Approach (g/kg fuel) |
2.04 |
2.0183 |
| Carbon Monoxide Idle (g/kg fuel) |
44.46 |
19.3235 |
| Carbon Monoxide Unitary Average (g/kN) |
55.51 |
23.5351 |
| Carbon Monoxide Unitary SD (g/kN) |
|
0.2059 |
| Carbon Monoxide Unitary Range (g/kN) |
|
23.42-23.77 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
63.25 |
28.8881 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
53.6 |
24.4814 |
| NOx Take Off (g/kg fuel) |
31.74 |
26.6057 |
| NOx Climb Out (g/kg fuel) |
25.03 |
19.9646 |
| NOx Approach (g/kg fuel) |
11.91 |
11.3908 |
| NOx Idle (g/kg fuel) |
3.72 |
4.0816 |
| NOx Unitary Average (g/kN) |
49.96 |
42.7674 |
| NOx Unitary SD (g/kN) |
|
0.0991 |
| NOx Unitary Range (g/kN) |
|
42.7-42.88 |
| NOx Unitary Characteristic (g/kN) |
54.94 |
49.5739 |
| NOx Unitaryto Standard (% of limit) |
55.3 |
47.0448 |
| NOx Unitaryto CAEP2 (% of limit) |
69.1 |
58.806 |
| NOx Unitaryto CAEP4 (% of limit) |
82.6 |
68.495 |
| NOx Unitaryto CAEP6 (% of limit) |
93.9 |
77.0548 |
| NOx Unitaryto CAEP8 (% of limit) |
110.6 |
89.3289 |
| NOx LTO (g) |
13332.8 |
11420.05 |
| Smoke Take Off (SN) |
8 |
2.4564 |
| Smoke Climb Out (SN) |
5.6 |
2.691 |
| Smoke Approach (SN) |
0.4 |
0.4726 |
| Smoke Idle (SN) |
0.1 |
0.4522 |
| Smoke Max (SN) |
8 |
3.009 |
| Smoke Sigma (SN) |
|
0.3201 |
| Smoke Range (SN) |
|
2.79-3.38 |
| Smoke Characteristic (SN) |
9.3 |
3.873 |
| Smoke Characteristicto Regulatory (% of limit) |
52.2 |
21.4152 |
| Fuel Flow Take Off (kg/s) |
2.567 |
2.569 |
| Fuel Flow Climbout (kg/s) |
2.036 |
2.0742 |
| Fuel Flow Approach (kg/s) |
0.696 |
0.6715 |
| Fuel Flow Idle (kg/s) |
0.206 |
0.1959 |
| Fuel LTO (kg) |
865 |
848.4728 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
14815.2 |
6284.509 |
| Emissions Data Status |
C |
C |
| Engine Status |
Out of production |
|
| NOx Compliance Demonstration |
2.3.2 d) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
0.5606 |
| nvPME Imass Climb Out (mg/kg) |
|
26.135 |
| nvPME Imass Idle (mg/kg) |
|
0.435 |
| nvPME Imass Max (mg/kg) |
|
28.4323 |
| nvPME Imass Take Off (mg/kg) |
|
26.3595 |
| nvPME Inum Approach (#/kg) |
|
44784090000000 |
| nvPME Inum Climb Out (#/kg) |
|
235482000000000 |
| nvPME Inum Idle (#/kg) |
|
47637080000000 |
| nvPME Inum Max (#/kg) |
|
240727100000000 |
| nvPME Inum Take Off (#/kg) |
|
168377400000000 |
| nvPMLTO Mass (mg) |
|
10223.02 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
53.2174 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
24.8679 |
| nvPMLTO Number (#) |
|
104417300000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
543558800000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
19.5525 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
967.3084 |
| nvPM Mass Concentration Max (mg/m³) |
|
751.5019 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
22.8138 |