Guizhou WS-13
The WS-13 (Chinese: 涡扇-13), codename Taishan, is a turbofan engine designed and manufactured by Guizhou Aircraft Industry Corporation to power the Pakistan-China jointly developed CAC/PAC JF-17 Thunder light-weight multi-role fighter, and in the near future the Shenyang J-31 fifth generation stealth fighter currently under development.
WS-13 | |
---|---|
Type | Turbofan |
National origin | People's Republic of China |
Manufacturer | Guizhou Aircraft Industry Corporation |
First run | 2006 |
Major applications | JF-17 Thunder J-31 |
Design and development
China began development of the Taishan in 2000 to replace the Klimov RD-93 turbofan, which had been selected in the 1990s to power the JF-17 light-weight fighter. It is designed to have a life span of 2,200 hours and an improved version, providing around 100 kN (22,450 lb) of thrust with afterburner, is under development.[1]
The WS-13 Taishan was certified in 2007 and serial production began in 2009. The 18 March 2010 edition of the HKB report stated that a FC-1 equipped with the WS-13 completed its first successful runway taxi test.[2]
Officials at the Farnborough International Airshow in August 2010 stated that a JF-17 was being test flown with a Chinese engine, likely the WS-13.[3] In November 2012, Aviation Week reported that flight testing on the JF-17 was underway in China.[4] It was reported at the 2015 Paris Air Show that testing was continuing.[5]
Variants
- WS-13 - 86 kilonewtons (19,000 lbf) thrust with afterburner.[1]
- WS-13A - High bypass.[6]
- WS-13E - 100 kilonewtons (22,000 lbf) thrust with afterburner
Specifications (WS-13)[7]
General characteristics
- Type: Afterburning turbofan
- Length: 4.14 metres (13.6 ft)
- Diameter: 1.02 metres (3 ft 4 in)
- Dry weight: 1,135 kilograms (2,502 lb)
Components
- Compressor: axial, 4-stage low pressure, 8-stage high pressure compressor
- Combustors: annular
- Turbine: counter-rotating 1-stage high pressure, 1-stage low pressure
Performance
- Maximum thrust: 56.75 kilonewtons (12,760 lbf) dry; 86.37 kilonewtons (19,420 lbf) with afterburner
- Bypass ratio: 0.57:1
- Turbine inlet temperature: 1650 K (1,377 °C (2,511 °F))
- Thrust-to-weight ratio: 7.8
See also
Comparable engines
- Eurojet EJ200 (EJ2x0 Standard)
- Snecma M88 (M88-2 Standard)
- Klimov RD-93 (RD-33MK Standard)
- General Electric F414 (F414-EPE Standard)
Related lists
References
- Fisher, Jr., Richard (2009-12-30). "October Surprises In Chinese Aerospace". International Assessment and Strategy Center. Archived from the original on 2015-08-13. Retrieved 2010-04-27.
- "China Defense Blog: FC-1 equipped with WS-13 completed first successful runway taxi test". 30 May 2010.
- Pocock, Chris (August 6, 2010). "China and Pakistan Push Chengdu JF-17 Fighter for Export". AIN Online (ainonline.com). AIN Online (ainonline.com). Archived from the original on 15 August 2010. Retrieved 8 August 2010.
- Sweetman, Bill (5 November 2012). "China's Warplane Industry Expands". Aviation Week. Retrieved 5 September 2013.
- Fisher, Richard D., Jr (15 June 2015). "Paris Air Show 2015: JF-17 fighter flying with indigenous Chinese turbofan". Archived from the original on 17 June 2015. Retrieved 13 June 2021.
- 中国涡扇系列 WS13 Archived 2016-04-19 at the Wayback Machine
- 大陸渦扇13引擎生產線就緒 可成為殲31心臟