General Electric F414

Turbofan · General Electric Company
Reaction Turbines
Bypass Ratio
0.25
Diameter
889 mm
Length
3911.6 mm
Dry Weight
1109.033 kg
Thrust To Weight
5.3
Specific Fuel Consumption
23.9 g/(kN·s)

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 annular
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 0.25 Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Boeing F/A-18E/F Super Hornet General Electric F414 2 18.31 13.62
HAL TEDBF General Electric F414 2 16.3 11.2
HAL Tejas Mk2 General Electric F414 1 14.65 8.5
KAI KF-21 Boramae General Electric F414 2 16.9 11.2
All data (16 fields)
Name
General Electric F414
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1109.033
Diameter (mm)
889
Length (mm)
3911.6
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_F414
Geared Fan
No
Combustion Chamber
annular
Afterburner
Yes
Streams
2
Bypass Ratio
0.25
Thrust To Weight
5.3
Specific Fuel Consumption (g/(kN·s))
23.9
Compressor Description
axial compressor with 3 low-pressure stages and 7 high-pressure stages
Turbine Description
1 low-pressure stage and 1 high-pressure stage