Guizhou WS-13

Last updated • 2 min readFrom Wikipedia, The Free Encyclopedia

WS-13
Type Turbofan
National originChina
Manufacturer Guizhou Aircraft Industry Corporation
First run2006
Major applications CAC/PAC JF-17 Thunder
Shenyang FC-31

The WS-13 (Chinese :涡扇-13), codename Taishan, is a turbofan engine designed and manufactured by Guizhou Aircraft Industry Corporation to power the CAC/PAC JF-17 Thunder lightweight multirole fighter jointly developed by China and Pakistan, and in the near future the Shenyang FC-31 fifth-generation stealth fighter currently under development.

Contents

Design and development

China began development of the Taishan in 2000 to create a domestic engine for replacing the Klimov RD-93 turbofan, which had been selected in the 1990s to power the JF-17 lightweight fighter. It is designed to produce 86 kN (19,000 lb) of thrust with afterburner and have a life span of 2,200 hours; an improved version providing up to 93 kN (21,000 lb) of thrust with afterburner was also developed. [1] [2]

The WS-13 Taishan was certified in 2007 and serial production began in 2009.[ citation needed ] The 18 March 2010 edition of the HKB Report stated that a JF-17 equipped with the WS-13 completed its first successful runway taxi test. [3]

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. [4] In November 2012, Aviation Week & Space Technology reported that flight testing on the JF-17 was underway in China. [5] It was reported at the 2015 Paris Air Show that testing was continuing. [6]

Guizhou is developing a new engine, designated the WS-19 that fits in the same footprint as the WS-13 but is a wholly new design that incorporates the same technology as the Xian WS-15. The WS-19 is the intended engine for production versions of the Shenyang FC-31 medium-size stealth fighter such as the J-35 for aircraft carriers. [2]

Variants

Applications

Specifications (WS-13)

Data from China Times [11]

General characteristics

Components

Performance

See also

Comparable engines

Related lists

Related Research Articles

<span class="mw-page-title-main">Eurojet EJ200</span> Military low bypass turbofan

The Eurojet EJ200 is a military low-bypass turbofan used as the powerplant of the Eurofighter Typhoon. The engine is largely based on the Rolls-Royce XG-40 technology demonstrator, which was developed in the 1980s. The EJ200 is built by the EuroJet Turbo GmbH consortium. The EJ200 is also used in the Bloodhound LSR supersonic land speed record attempting car.

<span class="mw-page-title-main">General Electric F110</span> Aircraft engine

The General Electric F110 is an afterburning turbofan jet engine produced by GE Aerospace. It was derived from the General Electric F101 as an alternative engine to the Pratt & Whitney F100 for powering tactical fighter aircraft, with the F-16C Fighting Falcon and F-14A+/B Tomcat being the initial platforms; the F110 would eventually power new F-15 Eagle variants as well. The engine is also built by IHI Corporation in Japan, TUSAŞ Engine Industries (TEI) in Turkey, and Samsung Techwin in South Korea as part of licensing agreements.

<span class="mw-page-title-main">General Electric F101</span> Turbofan aircraft engine

The General Electric F101 is an afterburning turbofan jet engine. It powers the Rockwell B-1 Lancer strategic bomber fleet of the USAF. In full afterburner it produces a thrust of more than 30,000 pounds-force (130 kN). The F101 was GE's first turbofan with an afterburner.

<span class="mw-page-title-main">General Electric F404</span> Turbofan aircraft engine family

The General Electric F404 and F412 are a family of afterburning turbofan engines in the 10,500–19,000 lbf (47–85 kN) class. The series is produced by GE Aerospace. Partners include Volvo Aero, which builds the RM12 variant. The F404 was developed into the larger F414 turbofan, as well as the experimental GE36 civil propfan.

<span class="mw-page-title-main">Snecma M88</span> French afterburning turbofan engine

The Snecma M88 is a French afterburning turbofan engine developed by Snecma for the Dassault Rafale fighter.

<span class="mw-page-title-main">General Electric F414</span> American afterburning turbofan engine

The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound thrust class produced by GE Aerospace. The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet. The engine was developed from the F412 non-afterburning turbofan planned for the A-12 Avenger II, before it was canceled.

<span class="mw-page-title-main">Volvo RM12</span> Jet engine

Reaktionsmotor 12 (RM12) is a low-bypass afterburning turbofan jet engine developed for the Saab JAS 39 Gripen fighter. A version of the General Electric F404, the RM12 was produced by Volvo Aero. The last of the 254 engines was produced on 24 May 2011, at which time it had reached 160,000 flight hours without any serious incidents.

<span class="mw-page-title-main">Tumansky RD-9</span> Turbojet aircraft engine

The Tumansky RD-9 was an early Soviet turbojet engine, not based on pre-existing German or British designs. The AM-5, developed by scaling down the AM-3, was available in 1952 and completed testing in 1953; it produced 25.5 kN (5,700 lbf) thrust without afterburner. The AM-5 engine is notable for making possible the first mass-produced supersonic interceptors such as the MiG-19, and the first Soviet all-weather area interceptor, the Yak-25. When Sergei Tumansky replaced Alexander Mikulin as the OKB-24's chief designer in 1956, the engine was renamed RD-9. The engine was later built under license in China as the WP-6.

<span class="mw-page-title-main">Klimov RD-33</span> Russian fighter aircraft engine

The Klimov RD-33 is a turbofan jet engine for a lightweight fighter jet and which is the primary engine for the Mikoyan MiG-29 and CAC/PAC JF-17 Thunder. It was developed in OKB-117 led by S. P. Izotov from 1968 with production starting in 1981. Previous generations of Russian supersonic fighters such as the MiG-21 and MiG-23 used turbojets, but western fighters such as the F-111 and F-4K introduced the use of afterburning turbofans in the 1960s which were more efficient.

<span class="mw-page-title-main">GTRE GTX-35VS Kaveri</span> Afterburning turbofan aircraft engine

The GTRE GTX-35VS Kaveri is an afterburning turbofan project under development by the Gas Turbine Research Establishment (GTRE), a lab under the Defence Research and Development Organisation (DRDO) in Bengaluru, India. An Indian design, the Kaveri was originally intended to power production models of the HAL Tejas Light Combat Aircraft (LCA) developed by Hindustan Aeronautics Limited. However, the Kaveri programme failed to satisfy the necessary technical requirements on time and was officially delinked from the Tejas programme in September 2008.

<span class="mw-page-title-main">Saturn AL-31</span> Family of turbofan engines used by the Soviet military

The Saturn AL-31 is a family of axial flow turbofan engines, developed by the Lyulka-Saturn design bureau in the Soviet Union, now NPO Saturn in Russia, originally as a 12.5-tonne powerplant for the Sukhoi Su-27 long range air superiority fighter. The AL-31 currently powers the Su-27 family of combat aircraft and some variants of the Chengdu J-10 multirole jet fighter. Assembly of the engine is also performed under license in India by HAL, for the Sukhoi Su-30MKI. Improved variants power the fifth-generation Sukhoi Su-57 and Chengdu J-20.

<span class="mw-page-title-main">Shenyang WS-10</span> Chinese fighter turbofan engine

The Shenyang WS-10, codename Taihang, is a turbofan engine designed and built by the People's Republic of China.

<span class="mw-page-title-main">General Electric YJ101</span> 1970s American prototype turbojet aircraft engine

The General Electric YJ101 was an afterburning turbofan engine, as signified by its "J" designation, in the 15,000 lbf class. It was designed for the Northrop P-530 Cobra but its initial application was the Northrop YF-17 entry in the Lightweight Fighter (LWF) competition. It was subsequently developed into the widely used General Electric F404.

The Shenyang J-13 was a long-running Chinese project by Shenyang Aircraft Corporation to develop a light-weight, single engine fighter aircraft, which was ultimately cancelled.

<span class="mw-page-title-main">Tumansky R-29</span> Soviet turbojet

The Tumansky R-29 is a Soviet turbojet aircraft engine that was developed in the early 1970s. It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.

The WS-6 was an unsuccessful turbofan development program from the People's Republic of China.

<span class="mw-page-title-main">Shenyang J-35</span> Fifth-generation jet fighter under development by Shenyang Aircraft Corporation

The Shenyang J-35 is a series of Chinese twin-engine, all-weather, stealth multirole combat aircraft manufactured by Shenyang Aircraft Corporation (SAC), designed for air superiority and surface strike missions. The aircraft reportedly has two variants, a land-based variant designed for the People's Liberation Army Air Force (PLAAF), and a carrier-based variant optimized for catapult-assisted launch (CATOBAR) for the People's Liberation Army Naval Air Force (PLANAF).

The Shenyang WS-15, codename Emei, is a Chinese afterburning turbofan engine designed by the Shenyang Aeroengine Research Institute and manufactured by the Shenyang Liming Aircraft Engine Company.

The Shenyang WS-20 is a high-bypass turbofan aircraft engine designed by the Shenyang Aeroengine Research Institute for the PLAAF's Y-20 family of strategic airlifters, it is currently installed in limited numbers. It is based on the core of the low-bypass turbofan Shenyang WS-10A. The thrust range is 138 kilonewtons (31,000 lbf).

The Guizhou WS-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.

References

  1. 1 2 Fisher, Richard Jr. (30 December 2009). "October Surprises In Chinese Aerospace". International Assessment and Strategy Center. Archived from the original on 13 August 2015. Retrieved 27 April 2010.
  2. 1 2 曾品潔 (9 February 2023). "中國渦輪-19發動機進度提前! 航發總師曝 : 未來殲-35會比殲-20更早換裝" (in Traditional Chinese). Newtalk新闻. Retrieved 26 February 2023.
  3. Coatepeque (30 May 2010). "FC-1 equipped with WS-13 completed first successful runway taxi test". China Defense Blog. Retrieved 11 February 2023 via Blogger.
  4. Pocock, Chris (6 August 2010). "China and Pakistan Push Chengdu JF-17 Fighter for Export". AINonline . Archived from the original on 15 August 2010. Retrieved 8 August 2010.
  5. Sweetman, Bill (5 November 2012). "China's Warplane Industry Expands". Aviation Week & Space Technology . Archived from the original on 10 May 2013. Retrieved 5 September 2013.
  6. Fisher, Richard D. Jr. (15 June 2015). "Paris Air Show 2015: JF-17 fighter flying with indigenous Chinese turbofan". Jane's Defence Weekly . Archived from the original on 17 June 2015. Retrieved 13 June 2021.
  7. "中国涡扇系列 WS13" (in Chinese). Northwestern Polytechnical University. 19 April 2016. Archived from the original on 19 April 2016. Retrieved 11 February 2023.
  8. "WS-13IPE engine for FC-31 fighter mass-produced in 2020". China Arms. 26 January 2020.
  9. "Our Best Look Yet At China's J-35 Carrier-Capable Stealth Fighter". 22 July 2022.
  10. Waldron, Greg (1 August 2023). "Future Asia Pacific carrier air wings come into focus". FlightGlobal. Archived from the original on 6 August 2023.
  11. Chiang, Fei-yu (10 February 2021). "大陸渦扇13引擎生產線就緒 可成為殲31心臟". China Times (in Chinese). Retrieved 11 February 2023.