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