Compare reaction turbines
All reaction turbines
|
GP7270
✕
|
Trent XWB-75EP
✕
|
| EASA ID |
9EA001 |
07P27RR150 |
| Aircraft Engine Manufacturer |
Engine Alliance |
Rolls-Royce |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Fuel |
Jet A-1 |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
|
Phase5 Tiled |
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
8.71 |
9.02 |
| Overall Pressure Ratio |
36.62 |
39.31 |
| Maximum Takeoff Thrust (kN) |
332.39 |
334.03 |
| 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) |
4.04 |
1.4164 |
| Hydrocarbon Unitary Average (g/kN) |
0.8 |
1.6527 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.2 |
0.4139 |
| Hydrocarbon Unitary Range (g/kN) |
4.17-4.77 |
1.05-1.96 |
| Hydrocarbon Unitary Characteristic (g/kN) |
6.94 |
1.8858 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
35.4 |
9.6214 |
| Hydrocarbon LTO (g) |
1498 |
552.0363 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.11 |
0.3534 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.09 |
0.418 |
| Carbon Monoxide Approach (g/kg fuel) |
1.27 |
1.3025 |
| Carbon Monoxide Idle (g/kg fuel) |
33.58 |
25.159 |
| Carbon Monoxide Unitary Average (g/kN) |
37.6 |
30.422 |
| Carbon Monoxide Unitary SD (g/kN) |
1.1 |
2.3309 |
| Carbon Monoxide Unitary Range (g/kN) |
36.35-38.46 |
27.59-32.71 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
46.15 |
32.5473 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
39.1 |
27.5825 |
| NOx Take Off (g/kg fuel) |
41.73 |
39.8934 |
| NOx Climb Out (g/kg fuel) |
31.37 |
31.3823 |
| NOx Approach (g/kg fuel) |
12.9 |
11.091 |
| NOx Idle (g/kg fuel) |
5.24 |
4.1409 |
| NOx Unitary Average (g/kN) |
53.29 |
46.2575 |
| NOx Unitary SD (g/kN) |
0.312 |
0.6982 |
| NOx Unitary Range (g/kN) |
53.06-53.65 |
45.34-46.99 |
| NOx Unitary Characteristic (g/kN) |
61.77 |
48.6103 |
| NOx Unitaryto Standard (% of limit) |
54.6 |
40.9789 |
| NOx Unitaryto CAEP2 (% of limit) |
68.2 |
51.2237 |
| NOx Unitaryto CAEP4 (% of limit) |
77 |
56.7727 |
| NOx Unitaryto CAEP6 (% of limit) |
85.6 |
62.6561 |
| NOx Unitaryto CAEP8 (% of limit) |
97.5 |
70.7135 |
| NOx LTO (g) |
17713 |
15450.85 |
| Smoke Take Off (SN) |
4.06 |
6.2837 |
| Smoke Climb Out (SN) |
3.87 |
8.3124 |
| Smoke Approach (SN) |
2.2 |
6.5036 |
| Smoke Idle (SN) |
3.08 |
1.7494 |
| Smoke Max (SN) |
4.06 |
10.4 |
| Smoke Sigma (SN) |
0.689 |
2.1 |
| Smoke Range (SN) |
3.28-4.56 |
7.4-11.9 |
| Smoke Characteristic (SN) |
5.22 |
11.3008 |
| Smoke Characteristicto Regulatory (% of limit) |
30.7 |
66.4379 |
| Fuel Flow Take Off (kg/s) |
2.637 |
2.3733 |
| Fuel Flow Climbout (kg/s) |
2.169 |
1.9409 |
| Fuel Flow Approach (kg/s) |
0.711 |
0.6839 |
| Fuel Flow Idle (kg/s) |
0.234 |
0.2498 |
| Fuel LTO (kg) |
932 |
909.74 |
| Fuel Venting Compliant |
Yes |
Yes |
| Carbon Monoxide LTO (g) |
12497 |
10161.5 |
| 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) |
|
77.1091 |
| nvPME Imass Climb Out (mg/kg) |
|
67.9609 |
| nvPME Imass Idle (mg/kg) |
|
20.9809 |
| nvPME Imass Max (mg/kg) |
|
118.9647 |
| nvPME Imass Take Off (mg/kg) |
|
43.1756 |
| nvPME Inum Approach (#/kg) |
|
1219084000000000 |
| nvPME Inum Climb Out (#/kg) |
|
447187700000000 |
| nvPME Inum Idle (#/kg) |
|
873181000000000 |
| nvPME Inum Max (#/kg) |
|
1297893000000000 |
| nvPME Inum Take Off (#/kg) |
|
225178800000000 |
| nvPMLTO Mass (mg) |
|
42548.11 |
| nvPMLTO Mass Per Thrust (mg/kN) |
|
143.798 |
| nvPMLTO Mass To CAEP11 (% of limit) |
|
67.1953 |
| nvPMLTO Number (#) |
|
677413800000000000 |
| nvPMLTO Number Per Thrust (#/kN) |
|
2289426000000000 |
| nvPMLTO Number To CAEP11 (% of limit) |
|
82.3535 |
| nvPM Mass Concentration Characteristic (mg/m³) |
|
2232.51 |
| nvPM Mass Concentration Max (mg/m³) |
|
2029.574 |
| nvPM Mass Concentration To CAEP10 (% of limit) |
|
57.3795 |