General Electric GE36

Bypass Ratio

Diameter

1940.56 mm

Dry Weight

2721.554 kg

Thrust To Weight

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 35	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
Boeing 7J7	General Electric GE36	2	43.5864	36.8808
McDonnell Douglas MD-94X	General Electric GE36		36.576		114

All data (13 fields)

Name: General Electric GE36
Aircraft Engine Manufacturer: General Electric Company
Aircraft Engine Type: Turbofan
Dry Weight (kg): 2721.554
Diameter (mm): 1940.56
Wikipedia Article (URL): en.wikipedia.org/wiki/General_Electric_GE36
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 35
Thrust To Weight: 8
Compressor Description: 3-stage low-pressure axial flow compressor @13,270 rpm, 7-stage high-pressure axial compressor @16,810 rpm
Turbine Description: 1-stage low-pressure turbine, 1-stage high-pressure turbine, 6-stage contra-rotating free power turbine