General Electric GE90

Turbofan · General Electric Company
Reaction Turbines

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 —
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 — Overall Pressure Ratio — Afterburner No

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Airplanes

Name Model Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Two Class Typical Seating Max Seating
Boeing New Large Airplane General Electric GE90 4 74.3712 79.248 606
777-200 777-200 General Electric GE90 2 73.86 64.8 313
All data (7 fields)
Name
General Electric GE90
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbofan
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_GE90
Geared Fan
No
Afterburner
No
Streams
2