Lotarev D-36

Bypass Ratio

6.3

Diameter

1333 mm

Length

3470 mm

Dry Weight

1109 kg

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 6.3	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
Antonov An-72	Lotarev D-36	2	28.07	31.89	52
Antonov An-74	Lotarev D-36	2	28.07	31.89	52
Mikoyan MiG 18-50	Lotarev D-36	2	24.9	23.3	18
Yakovlev Yak-42	Lotarev D-36	3	36.38	34.88	120

All data (13 fields)

Name: Lotarev D-36
Aircraft Engine Manufacturer: Ivchenko-Progress ZMKB
Aircraft Engine Type: Turbofan
Dry Weight (kg): 1109
Diameter (mm): 1333
Length (mm): 3470
Wikipedia Article (URL): en.wikipedia.org/wiki/Lotarev_D-36
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 6.3
Compressor Description: 7-stage high-pressure compressor, 6-stage low-pressure compressor
Turbine Description: 1-stage high-pressure turbine, 1-stage low-pressure turbine, 3-stage free-power turbine