General Electric J47

Turbojet · General Electric Company
Reaction Turbines
Diameter
933.45 mm
Length
3683 mm
Dry Weight
1158.475 kg
Thrust To Weight
2.34

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 1 Bypass Ratio — Overall Pressure Ratio — Afterburner No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Chase XC-123A General Electric J47 4 23.4696 33.528
Convair NB-36H General Electric J47 4 49.38 70.1
North American F-86D Sabre General Electric J47 1 12.27 11.31
All data (14 fields)
Name
General Electric J47
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1158.475
Diameter (mm)
933.45
Length (mm)
3683
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_J47
Fuel
JP-1, JP-2, JP-3, JP-4 or MIL-F-5572 gasoline
Geared Fan
No
Afterburner
No
Streams
1
Thrust To Weight
2.34
Compressor Description
12-stage axial compressor
Turbine Description
single-stage axial