Compare reaction turbines
All reaction turbines
|
GE90-76B
✕
|
Trent 1000-R3
✕
|
| EASA ID |
9GE124 |
02P23RR138 |
| Aircraft Engine Manufacturer |
General Electric Company |
Rolls-Royce |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A-1 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
PEC |
Phase5 Tiled |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
8.53 |
8.8835 |
| Overall Pressure Ratio |
35.5 |
49.5509 |
| Maximum Takeoff Thrust (kN) |
363.22 |
363.8735 |
| Hydrocarbon Take Off (g/kg fuel) |
0.03 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.03 |
0 |
| Hydrocarbon Approach (g/kg fuel) |
0.07 |
0 |
| Hydrocarbon Idle (g/kg fuel) |
3.21 |
0 |
| Hydrocarbon Unitary Average (g/kN) |
3.63 |
0 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.3 |
0 |
| Hydrocarbon Unitary Range (g/kN) |
3.43-3.98 |
0-0 |
| Hydrocarbon Unitary Characteristic (g/kN) |
5.59 |
0 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
28.5 |
0 |
| Hydrocarbon LTO (g) |
1318 |
0 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.31 |
0.434 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.32 |
0.4313 |
| Carbon Monoxide Approach (g/kg fuel) |
2.77 |
0.525 |
| Carbon Monoxide Idle (g/kg fuel) |
34.12 |
5.9151 |
| Carbon Monoxide Unitary Average (g/kN) |
39.57 |
7.6094 |
| Carbon Monoxide Unitary SD (g/kN) |
1.05 |
1.2472 |
| Carbon Monoxide Unitary Range (g/kN) |
38.85-40.77 |
6.32-9.17 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
48.6 |
8.04 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
41.2 |
6.8 |
| NOx Take Off (g/kg fuel) |
40.25 |
67.2866 |
| NOx Climb Out (g/kg fuel) |
32.43 |
47.8925 |
| NOx Approach (g/kg fuel) |
13.76 |
14.8882 |
| NOx Idle (g/kg fuel) |
5.1 |
6.2364 |
| NOx Unitary Average (g/kN) |
52.26 |
77.1665 |
| NOx Unitary SD (g/kN) |
0.72 |
0.8639 |
| NOx Unitary Range (g/kN) |
51.52-52.95 |
75.86-77.98 |
| NOx Unitary Characteristic (g/kN) |
60.6 |
80.3399 |
| NOx Unitaryto Standard (% of limit) |
54.6 |
57.7562 |
| NOx Unitaryto CAEP2 (% of limit) |
68.2 |
72.1953 |
| NOx Unitaryto CAEP4 (% of limit) |
77.7 |
75.7197 |
| NOx Unitaryto CAEP6 (% of limit) |
86.6 |
81.9279 |
| NOx Unitaryto CAEP8 (% of limit) |
99.1 |
90.0452 |
| NOx LTO (g) |
18984 |
28077.44 |
| Smoke Take Off (SN) |
0.94 |
7.8048 |
| Smoke Climb Out (SN) |
0.82 |
9.7465 |
| Smoke Approach (SN) |
1.4 |
10.154 |
| Smoke Idle (SN) |
1.56 |
1.7842 |
| Smoke Max (SN) |
1.56 |
14.7 |
| Smoke Sigma (SN) |
0.79 |
2 |
| Smoke Range (SN) |
0.82-2.4 |
11.4-16.7 |
| Smoke Characteristic (SN) |
2 |
16.4 |
| Smoke Characteristicto Regulatory (% of limit) |
12 |
98.6 |
| Fuel Flow Take Off (kg/s) |
2.796 |
2.8719 |
| Fuel Flow Climbout (kg/s) |
2.281 |
2.3219 |
| Fuel Flow Approach (kg/s) |
0.738 |
0.7435 |
| Fuel Flow Idle (kg/s) |
0.258 |
0.2699 |
| Fuel LTO (kg) |
999 |
1026.596 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
14371 |
2768.705 |
| Emissions Data Status |
C |
C |
| Engine Status |
Out of production |
Out of production |
| NOx Compliance Demonstration |
2.3.2 d) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
|
84.522 |
| nvPME Imass Climb Out (mg/kg) |
|
58.3213 |
| nvPME Imass Idle (mg/kg) |
|
19.4339 |
| nvPME Imass Max (mg/kg) |
|
154.1347 |
| nvPME Imass Take Off (mg/kg) |
|
40.8116 |
| nvPME Inum Approach (#/kg) |
|
896117500000000 |
| nvPME Inum Climb Out (#/kg) |
|
184355800000000 |
| nvPME Inum Idle (#/kg) |
|
474920300000000 |
| nvPME Inum Max (#/kg) |
|
932130000000000 |
| nvPME Inum Take Off (#/kg) |
|
99613180000000 |
| nvPMLTO Mass (mg) |
|
46062.68 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
175.9658 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
82.227 |
| nvPMLTO Number (#) |
|
428384800000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
1636490000000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
58.8665 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
3409.81 |
| nvPM Mass Concentration Max (mg/m³) |
|
2649.081 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
90.4434 |