Shenyang WS-10

Turbofan · Shenyang
Reaction Turbines
Maximum Takeoff Thrust
135 kN
Dry Weight
1795 kg
Thrust To Weight
8.8

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 annular
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 — Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Chengdu J-20 Shenyang WS-10 2 21.2 13.01
Shenyang J-16 Shenyang WS-10 2 21.9 14.7

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
V2531-E5 International Aero Engines 134.8 4.52 32.3 Compare
V2531-E5 International Aero Engines 134.8 4.52 32.3 Compare
PW1130G-JM Pratt & Whitney 134 11.7 35.52 Compare
CFM56-5B1/2P CFM56-5B CFM International 133.5 5.7 30.5 Compare
V2530-A5 International Aero Engines 133.4 4.54 32.1 Compare
V2530-A5 SelectOne™ Upgrade Package International Aero Engines 133 4.6 32 Compare
All data (11 fields)
Name
Shenyang WS-10
Aircraft Engine Manufacturer
Shenyang
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1795
Wikipedia Article (URL)
en.wikipedia.org/wiki/Shenyang_WS-10
Geared Fan
No
Combustion Chamber
annular
Afterburner
Yes
Streams
2
Maximum Takeoff Thrust (kN)
135
Thrust To Weight
8.8