Compare reaction turbines
All reaction turbines
|
GE90-110B1
✕
|
GE90-115B
✕
|
| EASA ID |
7GE097 |
01P21GE217 |
| Aircraft Engine Manufacturer |
GE Aircraft Engines |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A-1 |
Jet A |
| Geared Fan |
No |
No |
| Combustion Chamber |
DAC |
DAC |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
7.34 |
7.1 |
| Overall Pressure Ratio |
39.73 |
42.94 |
| Maximum Takeoff Thrust (kN) |
492.6 |
513.9 |
| Hydrocarbon Take Off (g/kg fuel) |
0.03 |
0.032 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.03 |
0.024 |
| Hydrocarbon Approach (g/kg fuel) |
0.06 |
0.048 |
| Hydrocarbon Idle (g/kg fuel) |
4.55 |
3.636 |
| Hydrocarbon Unitary Average (g/kN) |
5.44 |
3.82 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.12 |
0.25 |
| Hydrocarbon Unitary Range (g/kN) |
5.31-5.51 |
3.51-4.11 |
| Hydrocarbon Unitary Characteristic (g/kN) |
8.4 |
4.98 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
42.7 |
25.4082 |
| Hydrocarbon LTO (g) |
2679 |
1964.047 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.07 |
0.125 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.07 |
0.137 |
| Carbon Monoxide Approach (g/kg fuel) |
2.29 |
2.16 |
| Carbon Monoxide Idle (g/kg fuel) |
40.59 |
34.578 |
| Carbon Monoxide Unitary Average (g/kN) |
49.15 |
37.06 |
| Carbon Monoxide Unitary SD (g/kN) |
0.47 |
1.31 |
| Carbon Monoxide Unitary Range (g/kN) |
48.72-49.65 |
35.36-38.56 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
60.3 |
42.23 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
51.1 |
35.7881 |
| NOx Take Off (g/kg fuel) |
44.44 |
51.068 |
| NOx Climb Out (g/kg fuel) |
33.85 |
36.44 |
| NOx Approach (g/kg fuel) |
15.78 |
16.166 |
| NOx Idle (g/kg fuel) |
5.11 |
5.511 |
| NOx Unitary Average (g/kN) |
62.15 |
66.39 |
| NOx Unitary SD (g/kN) |
1 |
1.09 |
| NOx Unitary Range (g/kN) |
61.05-63.02 |
64.6-67.83 |
| NOx Unitary Characteristic (g/kN) |
72 |
73 |
| NOx Unitaryto Standard (% of limit) |
60.3 |
57.9917 |
| NOx Unitaryto CAEP2 (% of limit) |
75.4 |
72.4897 |
| NOx Unitaryto CAEP4 (% of limit) |
83.3 |
78.596 |
| NOx Unitaryto CAEP6 (% of limit) |
91.9 |
86.0443 |
| NOx Unitaryto CAEP8 (% of limit) |
103.5 |
96.0526 |
| NOx LTO (g) |
30616 |
34113.78 |
| Smoke Take Off (SN) |
3.58 |
3.38 |
| Smoke Climb Out (SN) |
2.25 |
2.23 |
| Smoke Approach (SN) |
1.42 |
1.6 |
| Smoke Idle (SN) |
0.96 |
1.34 |
| Smoke Max (SN) |
3.58 |
3.38 |
| Smoke Sigma (SN) |
0.87 |
1.55 |
| Smoke Range (SN) |
3.03-4.58 |
0.71-4.54 |
| Smoke Characteristic (SN) |
4.6 |
3.97 |
| Smoke Characteristicto Regulatory (% of limit) |
30.2 |
26.2642 |
| Fuel Flow Take Off (kg/s) |
4.32 |
4.6 |
| Fuel Flow Climbout (kg/s) |
3.47 |
3.566 |
| Fuel Flow Approach (kg/s) |
1.08 |
1.073 |
| Fuel Flow Idle (kg/s) |
0.37 |
0.341 |
| Fuel LTO (kg) |
1479 |
1453.392 |
| Fuel Venting Compliant |
No |
Yes |
| Carbon Monoxide LTO (g) |
24212 |
19038.99 |
| Emissions Data Status |
C |
C |
| Emissions Data Superseded |
Yes |
Yes |
| Emissions Superseded By |
21GE182 |
07P27GE240 |
| NOx Compliance Demonstration |
2.3.2 d) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
7.3197 |
| nvPME Imass Climb Out (mg/kg) |
|
9.6569 |
| nvPME Imass Idle (mg/kg) |
|
5.3148 |
| nvPME Imass Max (mg/kg) |
|
14.9402 |
| nvPME Imass Take Off (mg/kg) |
|
14.9402 |
| nvPME Inum Approach (#/kg) |
|
143381200000000 |
| nvPME Inum Climb Out (#/kg) |
|
102767500000000 |
| nvPME Inum Idle (#/kg) |
|
162747500000000 |
| nvPME Inum Max (#/kg) |
|
162747500000000 |
| nvPME Inum Take Off (#/kg) |
|
89357420000000 |
| nvPMLTO Mass (mg) |
|
12145.26 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
32.8517 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
15.3513 |
| nvPMLTO Number (#) |
|
189167000000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
511677600000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
18.4057 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
586.5072 |
| nvPM Mass Concentration Max (mg/m³) |
|
456 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
17.5359 |