Compare reaction turbines
All reaction turbines
|
CF34-3A/A1/A2/B1/B2
✕
|
CF34-3A1
✕
|
| EASA ID |
07P05GE220 |
1GE035 |
| Aircraft Engine Manufacturer |
General Electric Company |
GE Aircraft Engines |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A |
JP-5 |
| Geared Fan |
No |
No |
| Combustion Chamber |
SAC |
LEC II |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
6.25 |
6.25 |
| Overall Pressure Ratio |
19.3 |
19.7 |
| Maximum Takeoff Thrust (kN) |
41.01 |
41.01 |
| Hydrocarbon Take Off (g/kg fuel) |
0.06 |
0.06 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.05 |
0.06 |
| Hydrocarbon Approach (g/kg fuel) |
0.13 |
0.13 |
| Hydrocarbon Idle (g/kg fuel) |
4.69 |
3.95 |
| Hydrocarbon Unitary Average (g/kN) |
8.9 |
7.63 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
0.2 |
| Hydrocarbon Unitary Range (g/kN) |
|
7.41-7.78 |
| Hydrocarbon Unitary Characteristic (g/kN) |
13.7 |
11.8 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
69.9 |
60 |
| Hydrocarbon LTO (g) |
366 |
313 |
| Carbon Monoxide Take Off (g/kg fuel) |
0 |
0 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0 |
0 |
| Carbon Monoxide Approach (g/kg fuel) |
1.88 |
1.9 |
| Carbon Monoxide Idle (g/kg fuel) |
47.59 |
42.6 |
| Carbon Monoxide Unitary Average (g/kN) |
89.7 |
81.8 |
| Carbon Monoxide Unitary SD (g/kN) |
|
3.25 |
| Carbon Monoxide Unitary Range (g/kN) |
|
79.2-85.5 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
110.1 |
100.4 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
93.3 |
85.1 |
| NOx Take Off (g/kg fuel) |
11.28 |
11.61 |
| NOx Climb Out (g/kg fuel) |
9.68 |
10.14 |
| NOx Approach (g/kg fuel) |
6.63 |
6.86 |
| NOx Idle (g/kg fuel) |
3.72 |
3.82 |
| NOx Unitary Average (g/kN) |
26.3 |
27.8 |
| NOx Unitary SD (g/kN) |
|
1.61 |
| NOx Unitary Range (g/kN) |
|
26-29 |
| NOx Unitary Characteristic (g/kN) |
30.5 |
32.2 |
| NOx Unitaryto Standard (% of limit) |
38.8 |
40.6 |
| NOx Unitaryto CAEP2 (% of limit) |
48.5 |
50.7 |
| NOx Unitaryto CAEP4 (% of limit) |
50.9 |
53.2 |
| NOx Unitaryto CAEP6 (% of limit) |
52.1 |
54.5 |
| NOx Unitaryto CAEP8 (% of limit) |
56.4 |
58.9 |
| NOx LTO (g) |
1078 |
1137 |
| Smoke Take Off (SN) |
18.3 |
21.9 |
| Smoke Climb Out (SN) |
9.2 |
9.2 |
| Smoke Approach (SN) |
3.1 |
3.1 |
| Smoke Idle (SN) |
3.1 |
3.1 |
| Smoke Max (SN) |
18.3 |
21.9 |
| Smoke Sigma (SN) |
|
0.25 |
| Smoke Range (SN) |
|
21.7-22.2 |
| Smoke Characteristic (SN) |
23.6 |
28.2 |
| Smoke Characteristicto Regulatory (% of limit) |
78.1 |
93.3 |
| Fuel Flow Take Off (kg/s) |
0.3991 |
0.407 |
| Fuel Flow Climbout (kg/s) |
0.3288 |
0.3343 |
| Fuel Flow Approach (kg/s) |
0.116 |
0.119 |
| Fuel Flow Idle (kg/s) |
0.0489 |
0.0496 |
| Fuel LTO (kg) |
164 |
167 |
| Fuel Venting Compliant |
|
No |
| Carbon Monoxide LTO (g) |
3683 |
3350 |
| Emissions Data Status |
C |
C |
| Engine Status |
|
Out of production |
| NOx Compliance Demonstration |
2.3.2 e) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
0.8088 |
|
| nvPME Imass Climb Out (mg/kg) |
114.0471 |
|
| nvPME Imass Idle (mg/kg) |
1.4487 |
|
| nvPME Imass Max (mg/kg) |
287.0006 |
|
| nvPME Imass Take Off (mg/kg) |
287.0006 |
|
| nvPME Inum Approach (#/kg) |
80427050000000 |
|
| nvPME Inum Climb Out (#/kg) |
1333178000000000 |
|
| nvPME Inum Idle (#/kg) |
167524400000000 |
|
| nvPME Inum Max (#/kg) |
2006645000000000 |
|
| nvPME Inum Take Off (#/kg) |
2006645000000000 |
|
| nvPMLTO Mass (mg) |
10006.38 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
339.1479 |
|
| nvPMLTO Mass To CAEP11 (% of limit) |
35.0526 |
|
| nvPMLTO Number (#) |
107382800000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
3639545000000000 |
|
| nvPMLTO Number To CAEP11 (% of limit) |
31.4128 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
10129.73 |
|
| nvPM Mass Concentration Max (mg/m³) |
7869.784 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
90.6489 |
|