Progress D-436

Turbofan · Ivchenko-Progress ZMKB
Reaction Turbines
Bypass Ratio
4.95
Diameter
1373 mm
Length
3030 mm
Dry Weight
1450 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 4.95 Overall Pressure Ratio — Afterburner No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Max Seating
Antonov An-178 Progress D-436 2 32.23 30.57 70
Tupolev Tu-334 Progress D-436 2 31.26 29.77 102
All data (13 fields)
Name
Progress D-436
Aircraft Engine Manufacturer
Ivchenko-Progress ZMKB
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1450
Diameter (mm)
1373
Length (mm)
3030
Wikipedia Article (URL)
en.wikipedia.org/wiki/Progress_D-436
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.95
Compressor Description
Axial flow, 1-stage fan, 6-stage IP, 7-stage HP
Turbine Description
1-stage HP, 1-stage IP, 3-stage LP