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The Guizhou WS-19 (Chinese: 涡扇-19), code name Huangshan, is an afterburner turbofan engine designed by the Guizhou Aeroengine Design Institute. It has a reported thrust-to-weight ratio of 10 and a thrust of 10 metric tons or 22,000 lbs.[1][2]
| WS-19 | |
|---|---|
| Type | Turbofan |
| National origin | China |
| Major applications | Shenyang FC-31 |
The WS-19 fits in the same footprint as the earlier Guizhou WS-13, but is of an entirely new design that incorporates the same technology as found on the Xian WS-15. The WS-19 is intended for the production versions of the Shenyang FC-31 medium-size stealth fighter such as the Shenyang J-35.[2][3]
The reported maximum thrust of the WS-19 is 116 kN (26,000 lbf).[4]
Data from China Aerospace Propulsion Technology Forum 2022[1]
General characteristics
- Type: afterburning turbofan
- Length:
- Diameter:
- Dry weight:
Components
- Compressor: axial
- Combustors: annular
Performance
- Maximum thrust: 26,000 lbf (116 kN; 11,793 kgf) with afterburner[4]
- Thrust-to-weight ratio: ~10
Comparable engines
Related lists
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