GE90-113B

Turbofan · GE Aircraft Engines

Reaction Turbines

Maximum Takeoff Thrust

504.9 kN

Bypass Ratio

7.17

Overall Pressure Ratio

41.21

Fuel Flow Take Off

4.53 kg/s

NOx Unitaryto CAEP8

104.5 % 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 7.17	Overall Pressure Ratio 41.21	Afterburner No

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Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
GE90-113B	General Electric Company	504.9	7.2	41.81	Compare
GE90-115B	General Electric Company	513.9	7.1	42.94	Compare
GE90-110B1	General Electric Company	492.6851	7.23	40.6145	Compare
Trent XWB-97	Rolls-Royce	436.7	8.04	48.57	Compare
GE90-94B	GE Aircraft Engines	432.8	8.33	40.53	Compare
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All data (66 fields)

Name: GE90-113B
EASA ID: 7GE098
Aircraft Engine Manufacturer: GE Aircraft Engines
Aircraft Engine Type: Turbofan
Fuel: Jet A-1
Geared Fan: No
Combustion Chamber: DAC
Afterburner: No
Streams: 2
Bypass Ratio: 7.17
Overall Pressure Ratio: 41.21
Maximum Takeoff Thrust (kN): 504.9
Hydrocarbon Take Off (g/kg fuel): 0.03
Hydrocarbon Climb Out (g/kg fuel): 0.03
Hydrocarbon Approach (g/kg fuel): 0.06
Hydrocarbon Idle (g/kg fuel): 4.37
Hydrocarbon Unitary Average (g/kN): 5.17
Hydrocarbon Unitary Sigma (g/kN): 0.11
Hydrocarbon Unitary Range (g/kN): 5.04-5.27
Hydrocarbon Unitary Characteristic (g/kN): 8
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 40.6
Hydrocarbon LTO (g): 2608
Carbon Monoxide Take Off (g/kg fuel): 0.08
Carbon Monoxide Climb Out (g/kg fuel): 0.07
Carbon Monoxide Approach (g/kg fuel): 2.11
Carbon Monoxide Idle (g/kg fuel): 39.72
Carbon Monoxide Unitary Average (g/kN): 47.55
Carbon Monoxide Unitary SD (g/kN): 0.48
Carbon Monoxide Unitary Range (g/kN): 47.12-48.06
Carbon Monoxide Unitary Characteristic (g/kN): 58.4
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 49.5
NOx Take Off (g/kg fuel): 47.74
NOx Climb Out (g/kg fuel): 35.08
NOx Approach (g/kg fuel): 16.2
NOx Idle (g/kg fuel): 5.16
NOx Unitary Average (g/kN): 65.37
NOx Unitary SD (g/kN): 0.98
NOx Unitary Range (g/kN): 64.29-66.21
NOx Unitary Characteristic (g/kN): 75.8
NOx Unitaryto Standard (% of limit): 61.9
NOx Unitaryto CAEP2 (% of limit): 77.4
NOx Unitaryto CAEP4 (% of limit): 84.7
NOx Unitaryto CAEP6 (% of limit): 93.1
NOx Unitaryto CAEP8 (% of limit): 104.5
NOx LTO (g): 33006
Smoke Take Off (SN): 3.88
Smoke Climb Out (SN): 2.39
Smoke Approach (SN): 1.44
Smoke Idle (SN): 0.9
Smoke Max (SN): 3.88
Smoke Sigma (SN): 1.04
Smoke Range (SN): 3.13-5.07
Smoke Characteristic (SN): 5
Smoke Characteristicto Regulatory (% of limit): 32.9
Fuel Flow Take Off (kg/s): 4.53
Fuel Flow Climbout (kg/s): 3.58
Fuel Flow Approach (kg/s): 1.11
Fuel Flow Idle (kg/s): 0.38
Fuel LTO (kg): 1518
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 24007
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 21GE183
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 d)