General Electric CF700

Bypass Ratio

Diameter

838.2 mm

Length

1917.7 mm

Dry Weight

333.3904 kg

Thrust To Weight

6.6

Specific Fuel Consumption

18.978 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 —
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 2	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
Dassault Falcon 20	General Electric CF700	2	17.15	16.3	14

All data (16 fields)

Name: General Electric CF700
Aircraft Engine Manufacturer: General Electric Company
Aircraft Engine Type: Turbofan
Dry Weight (kg): 333.3904
Diameter (mm): 838.2
Length (mm): 1917.7
Wikipedia Article (URL): en.wikipedia.org/wiki/General_Electric_CF700
Fuel: Aviation kerosene
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 2
Thrust To Weight: 6.6
Specific Fuel Consumption (g/(kN·s)): 18.978
Compressor Description: 8 stage high pressure compressor + 1 stage fan directly driven by the free LP turbine
Turbine Description: 2 stage high pressure turbine, 1 stage low pressure turbine