Guizhou WS-19

Afterburner turbofan engine From Wikipedia, the free encyclopedia

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]

Quick Facts WS-19, Type ...
WS-19
Type Turbofan
National origin China
Major applications Shenyang FC-31
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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]

Design

The reported maximum thrust of the WS-19 is 116 kN (26,000 lbf).[4]

Specifications (WS-19)

Data from China Aerospace Propulsion Technology Forum 2022[1]

General characteristics

  • Type: afterburning turbofan
  • Length:
  • Diameter:
  • Dry weight:

Components

Performance

See also

Comparable engines

Related lists

References

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