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Guizhou WS-13

From Wikipedia, the free encyclopedia

WS-13
Type Turbofan
National origin China
Manufacturer Guizhou Aircraft Industry Corporation
First run 2006
Major applications CAC/PAC JF-17 Thunder
Shenyang FC-31

TheWS-13(Chinese:Oa phiến -13), codenameTaishan,is aturbofanengine designed and manufactured byGuizhou Aircraft Industry Corporationto power theCAC/PAC JF-17 Thunderlightweightmultirole fighterjointly developed by China and Pakistan, and in the near future theShenyang FC-31fifth-generationstealth fightercurrently under development.

Design and development

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China began development of the Taishan in 2000 to create a domestic engine for replacing theKlimov RD-93turbofan, 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 withafterburnerand 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 theHKB Reportstated that a JF-17 equipped with the WS-13 completed its first successful runway taxi test.[3]

Officials at theFarnborough International Airshowin 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 Technologyreported that flight testing on the JF-17 was underway in China.[5]It was reported at the 2015Paris Air Showthat testing was continuing.[6]

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

Variants

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  • WS-13– 86 kilonewtons (19,000 lbf) thrust withafterburner[1]
  • WS-13A– high bypass[7]
  • WS-13E/WS-21– 93 kilonewtons (21,000 lbf) thrust with afterburner

Specifications (WS-13)

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Data fromChina Times[8]

General characteristics

  • Type:afterburningturbofan
  • Length:4.14 m (163 in)
  • Diameter:1.02 m (40 in)
  • Dry weight:1,135 kg (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

See also

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Comparable engines

Related lists

References

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  1. ^abFisher, Richard Jr. (30 December 2009)."October Surprises In Chinese Aerospace".International Assessment and Strategy Center.Archived fromthe originalon 13 August 2015.Retrieved27 April2010.
  2. ^abTừng phẩm khiết (9 February 2023)."Trung Quốc tua bin -19 động cơ tiến độ trước tiên! Hàng phát tổng sư phơi: Tương lai tiêm -35 sẽ so tiêm -20 sớm hơn đổi trang"(in Traditional Chinese). Newtalk tin tức.Retrieved26 February2023.
  3. ^Coatepeque (30 May 2010)."FC-1 equipped with WS-13 completed first successful runway taxi test".China Defense Blog.Retrieved11 February2023– viaBlogger.
  4. ^Pocock, Chris (6 August 2010)."China and Pakistan Push Chengdu JF-17 Fighter for Export".AINonline.Archived fromthe originalon 15 August 2010.Retrieved8 August2010.
  5. ^Sweetman, Bill(5 November 2012)."China's Warplane Industry Expands".Aviation Week & Space Technology.Archived fromthe originalon 10 May 2013.Retrieved5 September2013.
  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 fromthe originalon 17 June 2015.Retrieved13 June2021.
  7. ^"Trung Quốc oa phiến hệ liệt WS13"(in Chinese).Northwestern Polytechnical University.19 April 2016. Archived fromthe originalon 19 April 2016.Retrieved11 February2023.
  8. ^Chiang, Fei-yu (10 February 2021)."Đại lục oa phiến 13 động cơ sinh sản tuyến ổn thoả nhưng trở thành tiêm 31 trái tim".China Times(in Chinese).Retrieved11 February2023.
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