Compare reaction turbines
All reaction turbines
|
Trent 1000-H2
✕
|
GEnx-1B58/P2
✕
|
| EASA ID |
12RR066 |
07P27GE231 |
| Aircraft Engine Manufacturer |
Rolls-Royce |
General Electric Company |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
|
Jet A |
| Geared Fan |
No |
No |
| Combustion Chamber |
Phase5 Tiled |
TAPS |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
9.49 |
9.3341 |
| Overall Pressure Ratio |
38.52 |
37.3864 |
| Maximum Takeoff Thrust (kN) |
287.1 |
271.3415 |
| Hydrocarbon Take Off (g/kg fuel) |
0 |
0.0137 |
| Hydrocarbon Climb Out (g/kg fuel) |
0 |
0.0146 |
| Hydrocarbon Approach (g/kg fuel) |
0 |
0.0551 |
| Hydrocarbon Idle (g/kg fuel) |
0.07 |
1.0642 |
| Hydrocarbon Unitary Average (g/kN) |
0.09 |
1.2547 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.08 |
0.1125 |
| Hydrocarbon Unitary Range (g/kN) |
0-0.17 |
1.13-1.33 |
| Hydrocarbon Unitary Characteristic (g/kN) |
0.1 |
1.9324 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
0.5 |
9.859 |
| Hydrocarbon LTO (g) |
24.81 |
340.4465 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.48 |
0.2042 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.43 |
1.0844 |
| Carbon Monoxide Approach (g/kg fuel) |
0.89 |
2.4301 |
| Carbon Monoxide Idle (g/kg fuel) |
9.82 |
17.7051 |
| Carbon Monoxide Unitary Average (g/kN) |
13.35 |
22.2993 |
| Carbon Monoxide Unitary SD (g/kN) |
3.36 |
0.4167 |
| Carbon Monoxide Unitary Range (g/kN) |
9.37-17.18 |
21.82-22.58 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
14.28 |
27.3712 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
12.1 |
23.1959 |
| NOx Take Off (g/kg fuel) |
40.46 |
17.528 |
| NOx Climb Out (g/kg fuel) |
31.49 |
11.4068 |
| NOx Approach (g/kg fuel) |
12.56 |
9.1084 |
| NOx Idle (g/kg fuel) |
5.21 |
4.2726 |
| NOx Unitary Average (g/kN) |
49.8 |
24.2551 |
| NOx Unitary SD (g/kN) |
0.77 |
0.57 |
| NOx Unitary Range (g/kN) |
49.13-50.61 |
23.87-24.91 |
| NOx Unitary Characteristic (g/kN) |
52.34 |
28.1153 |
| NOx Unitaryto Standard (% of limit) |
44.72 |
24.4965 |
| NOx Unitaryto CAEP2 (% of limit) |
55.9 |
30.6207 |
| NOx Unitaryto CAEP4 (% of limit) |
62.28 |
34.3823 |
| NOx Unitaryto CAEP6 (% of limit) |
68.86 |
38.1314 |
| NOx Unitaryto CAEP8 (% of limit) |
77.93 |
43.3259 |
| NOx LTO (g) |
14299 |
6581.406 |
| Smoke Take Off (SN) |
3.8 |
0.2924 |
| Smoke Climb Out (SN) |
4.8 |
0.2927 |
| Smoke Approach (SN) |
3.3 |
0.42 |
| Smoke Idle (SN) |
0.5 |
0.4916 |
| Smoke Max (SN) |
5.98 |
0.9582 |
| Smoke Sigma (SN) |
2.26 |
0.3273 |
| Smoke Range (SN) |
3-8.3 |
0.74-1.34 |
| Smoke Characteristic (SN) |
6.5 |
1.2333 |
| Smoke Characteristicto Regulatory (% of limit) |
36.64 |
6.8495 |
| Fuel Flow Take Off (kg/s) |
2.075 |
2.0468 |
| Fuel Flow Climbout (kg/s) |
1.715 |
1.6908 |
| Fuel Flow Approach (kg/s) |
0.582 |
0.5531 |
| Fuel Flow Idle (kg/s) |
0.233 |
0.198 |
| Fuel LTO (kg) |
817 |
750.7627 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
3832 |
6050.719 |
| 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) |
|
0.8772 |
| nvPME Imass Climb Out (mg/kg) |
|
0.0146 |
| nvPME Imass Idle (mg/kg) |
|
0.3003 |
| nvPME Imass Max (mg/kg) |
|
5.7777 |
| nvPME Imass Take Off (mg/kg) |
|
0.0157 |
| nvPME Inum Approach (#/kg) |
|
57880470000000 |
| nvPME Inum Climb Out (#/kg) |
|
10009410000 |
| nvPME Inum Idle (#/kg) |
|
35961110000000 |
| nvPME Inum Max (#/kg) |
|
244528700000000 |
| nvPME Inum Take Off (#/kg) |
|
4868807000 |
| nvPMLTO Mass (mg) |
|
213.7976 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
1.0953 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
0.5118 |
| nvPMLTO Number (#) |
|
18793290000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
96275700000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
3.4632 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
159.8387 |
| nvPM Mass Concentration Max (mg/m³) |
|
124.1787 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
3.7937 |