Maximum Takeoff Thrust
513.9 kN
Bypass Ratio
7.1
Overall Pressure Ratio
42.94
Fuel Flow Take Off
4.6 kg/s
NOx Unitaryto CAEP8
96.0526 % of limit

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber DAC
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 7.1 Overall Pressure Ratio 42.94 Afterburner No

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Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
GE90-115B General Electric Company 513.9 7.1 42.94 Compare
GE90-113B GE Aircraft Engines 504.9 7.17 41.21 Compare
GE90-110B1 General Electric Company 492.6851 7.23 40.6145 Compare
General Electric GE9X GE9X General Electric Company 489.3 10 60 Compare
All data (84 fields)
Name
GE90-115B
EASA ID
01P21GE217
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
DAC
Afterburner
No
Streams
2
Bypass Ratio
7.1
Overall Pressure Ratio
42.94
Maximum Takeoff Thrust (kN)
513.9
Hydrocarbon Take Off (g/kg fuel)
0.032
Hydrocarbon Climb Out (g/kg fuel)
0.024
Hydrocarbon Approach (g/kg fuel)
0.048
Hydrocarbon Idle (g/kg fuel)
3.636
Hydrocarbon Unitary Average (g/kN)
3.82
Hydrocarbon Unitary Sigma (g/kN)
0.25
Hydrocarbon Unitary Range (g/kN)
3.51-4.11
Hydrocarbon Unitary Characteristic (g/kN)
4.98
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
25.4082
Hydrocarbon LTO (g)
1964.047
Carbon Monoxide Take Off (g/kg fuel)
0.125
Carbon Monoxide Climb Out (g/kg fuel)
0.137
Carbon Monoxide Approach (g/kg fuel)
2.16
Carbon Monoxide Idle (g/kg fuel)
34.578
Carbon Monoxide Unitary Average (g/kN)
37.06
Carbon Monoxide Unitary SD (g/kN)
1.31
Carbon Monoxide Unitary Range (g/kN)
35.36-38.56
Carbon Monoxide Unitary Characteristic (g/kN)
42.23
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
35.7881
NOx Take Off (g/kg fuel)
51.068
NOx Climb Out (g/kg fuel)
36.44
NOx Approach (g/kg fuel)
16.166
NOx Idle (g/kg fuel)
5.511
NOx Unitary Average (g/kN)
66.39
NOx Unitary SD (g/kN)
1.09
NOx Unitary Range (g/kN)
64.6-67.83
NOx Unitary Characteristic (g/kN)
73
NOx Unitaryto Standard (% of limit)
57.9917
NOx Unitaryto CAEP2 (% of limit)
72.4897
NOx Unitaryto CAEP4 (% of limit)
78.596
NOx Unitaryto CAEP6 (% of limit)
86.0443
NOx Unitaryto CAEP8 (% of limit)
96.0526
NOx LTO (g)
34113.78
Smoke Take Off (SN)
3.38
Smoke Climb Out (SN)
2.23
Smoke Approach (SN)
1.6
Smoke Idle (SN)
1.34
Smoke Max (SN)
3.38
Smoke Sigma (SN)
1.55
Smoke Range (SN)
0.71-4.54
Smoke Characteristic (SN)
3.97
Smoke Characteristicto Regulatory (% of limit)
26.2642
Fuel Flow Take Off (kg/s)
4.6
Fuel Flow Climbout (kg/s)
3.566
Fuel Flow Approach (kg/s)
1.073
Fuel Flow Idle (kg/s)
0.341
Fuel LTO (kg)
1453.392
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
19038.99
Emissions Data Status
C
Emissions Data Superseded
Yes
Emissions Superseded By
07P27GE240
NOx Compliance Demonstration
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