Misplaced Pages

Shenyang WS-10

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.

This is an old revision of this page, as edited by 2602:306:b8bf:c0:a17b:1dc4:f754:7974 (talk) at 00:04, 8 August 2015 (The source did not even mention AL-31FM1, where did you get the idea that the latest WS-10 has less thrust than AL-31FM1? You troll !!!!). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Revision as of 00:04, 8 August 2015 by 2602:306:b8bf:c0:a17b:1dc4:f754:7974 (talk) (The source did not even mention AL-31FM1, where did you get the idea that the latest WS-10 has less thrust than AL-31FM1? You troll !!!!)(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)
This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed.
Find sources: "Shenyang WS-10" – news · newspapers · books · scholar · JSTOR (April 2010) (Learn how and when to remove this message)

WS-10
Type Turbofan
National origin People's Republic of China
Manufacturer Shenyang Liming Aircraft Engine Company
First run 1990s
Major applications Shenyang J-11B
Shenyang J-16
Status In production
Number built 300+
Developed into WS-20

The Shenyang WS-10 (Chinese: 涡扇-10; pinyin: woshan-10; lit. 'turbofan-10'), codename Taihang, is a turbofan engine designed and built by the People's Republic of China.

The WS-10A reportedly powers the J-11B and the J-16. Unconfirmed reports claim the WS-10A powers some J-10Bs. Unconfirmed reports also claim an improved WS-10A powers the J-11D.

Chinese media claimed 266 engines were manufactured from 2010 to 2012 for the J-11 program. Unofficial estimates placed production at more than 300 units by May 2015.

Description

The WS-10A is advertised as 120–140 kilonewtons (27,000–31,000 lbf) thrust engine. It has Full Authority Digital Engine Control.

Development

The WS-10 was derived from the WS-6 turbofan, which was abandoned at the start of the 1980s. The WS-10 project was reportedly started by Deng Xiaoping in 1986 to produce an engine comparable to the AL-31. The work was given to the Shenyang Aeroengine Research Institute (606 Institute) of Aviation Industry Corporation of China (AVIC). The WS-10 may have been based on the core of the CFM-56II (itself based on the General Electric F101); China purchased two CFM-56IIs in the 1980s. China may have spent nearly 20 years developing source code, after being unable to purchase code from Salyut.

The WS-10A, targeted for 130 kilonewtons (29,000 lbf) of thrust, was already in development in 2002. An early version was flown on an J-8II in 2002. In 2004, Russian sources familiar with project reported problems meeting the thrust target; in 2005, they reported problems reducing the weight of the primary and secondary compressors, in addition to problems meeting thrust requirements. Engine testing on the J-11 had already started by 2004, and testing using one engine on the J-11 may have occurred as early as 2002.

A full-scale WS-10A engine was first seen at the 2008. China International Aviation & Aerospace Exhibition.

In 2009, Western media reported that the WS-10A approached the performance of the Saturn AL-31, but took much longer than the AL-31 to develop thrust. Furthermore, reportedly the engine only generated 110–125 kilonewtons (25,000–28,000 lbf) of thrust. In April 2009, Lin Zuoming, head of AVIC, reported that the engine's quality was unsatisfactory. In 2010, it was reported that reliability was also poor; the WS-10A lasted only 30 hours, while the AL-31 needed refurbishing after 400 hours. The quality problems encountered with the WS-10A reflected the state of the Chinese aerospace industry; AVIC initiated a general effort to improve quality control throughout its production chain in 2011.

The WS-10A reportedly matured enough after 2009 to power the J-11B Block 02 aircraft. A WS-10A-powered J-10B was seen in July 2011, but the engine did not power the initial J-10B production batch, possibly because of production or performance issues.

Unconfirmed reports claimed the first flight of the J-11D was powered by a new WS-10 variant; the variant reportedly had improved reliability, and a thrust of more than 137 kilonewtons (31,000 lbf). The flight was revealed in early May 2015.

WS-20

The WS-20 is a high-bypass engine reportedly producing 14 tons of thrust. It is believed to be based on the core of the WS-10A.

The WS-20 was first seen in January 2014 while being tested on an Il-76, and is believed to be intended for the Y-20 strategic airlifter.

Variants

  • WS-10
  • WS-10A – improved variant; advertised to have 120–140 kilonewtons (27,000–31,000 lbf) of thrust
  • WS-10Gthust vectoring variant for the J-20 fighter; 152–155 kilonewtons (34,000–35,000 lbf) of thrust
  • WS-20 – high-bypass derivative for the Y-20 transport; 138 kilonewtons (31,000 lbf) of thrust

Specifications (WS-10A)

General characteristics

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

Components

  • Compressor:

Performance

See also

Comparable engines

Related development

Related lists

References

  1. ^ Fisher, Richard (27 May 2015). "ANALYSIS: Can China break the military aircraft engine bottleneck?". flightglobal.com. Retrieved 5 August 2015.
  2. Fisher, Richard D. Jr. (26 August 2014). "Chinese J-11BH 'aggressive' with USN P-8A, says DoD". janes.com. Retrieved 25 May 2015.
  3. Weening, Alexander; Hardy, James (9 October 2014). "New pictures of J-10B revealed". janes.com. Retrieved 25 May 2015.
  4. ^ Fisher, Richard D. Jr. (5 May 2015). "Images show J-11D variant with possible new radar". janes.com. Retrieved 25 May 2015. Cite error: The named reference "janes_2015-05-05" was defined multiple times with different content (see the help page).
  5. "美称中国近三年内共生产约266台太行发动机". mil.news.sina.com.cn (in Chinese). 20 December 2012. Retrieved 25 May 2015.
  6. ^ Fisher, Richard, Jr. (30 December 2009). "October Surprises In Chinese Aerospace". International Assessment and Strategy Center. Retrieved 25 May 2015.{{cite web}}: CS1 maint: multiple names: authors list (link)
  7. "LM WS10A Tai Hang (China), Aero-engines - Turbofan". janes.com. 26 January 2010. Archived from the original on 18 February 2010. Retrieved 25 May 2015.
  8. "Liming WS10A Taihang Engine". globalsecurity.org. 28 September 2014. Retrieved 25 May 2015.
  9. ^ Fisher, Richard D., Jr. (7 October 2003). "New Developments In Russia-China Military Relations: A Report On The August 19-23 2003 Moscow Aerospace Salon (MAKS)". uscc.gov. United States-China Economic and Security Review Commission. Archived from the original on 12 January 2005. Retrieved 25 May 2015.{{cite web}}: CS1 maint: multiple names: authors list (link)
  10. ^ Fisher, Richard, Jr. (13 December 2004). "Report on the 5th Airshow China: Zhuhai, PRC, November 1-7, 2004". International Assessment and Strategy Center. Retrieved 25 May 2015.{{cite web}}: CS1 maint: multiple names: authors list (link)
  11. Fisher, Richard, Jr. (12 September 2005). "Chinese Dimensions of the 2005 Moscow Aerospace Show". United States: International Assessment and Strategy Center. Retrieved 25 May 2015.{{cite web}}: CS1 maint: multiple names: authors list (link)
  12. Saunders et. al: p.37
  13. Saunders et. al: p.44
  14. Pomfret, John. "Military strength is eluding China." Washington Post, 25 December 2010.
  15. Collins, Gabe; Erickson, Andrew (27 June 2011). "Jet Engine Development in China: Indigenous high-performance turbofans are a final step toward fully independent fighter production". chinasignpost.com. Retrieved 25 May 2015.
  16. Rupprecht, Andreas (December 2011). "China's 'Flanker' gains momentum. Shenyang J-11 update". Combat Aircraft Monthly. 12 (12): 40–42.
  17. ^ Fisher, Richard D. Jr. (4 September 2014). "China's Y-20 'enters second phase of testing'". janes.com. Retrieved 25 May 2015.
  18. Lin, Jeffrey; Singer, P.W. (20 February 2015). "China's most powerful aircraft engine ever takes to the sky: Presenting the WS-20". popsci.com. Retrieved 25 May 2015.
  19. Saunders et. al: p.45
Bibliography
AVIC aircraft and aero engines
Fighter and attack aircraft
Bombers
Trainers
Transport aircraft
Commercial aircraft
Civilian airshipAS700
Helicopters
  • Advanced Heavy Lifter
  • AC313
  • AC332
  • AC352
  • CA-109
  • HC-120
  • WZ-10
  • WZ-19
  • Z-5
  • Z-8
  • Z-9
  • Z-11
  • Z-18
  • Z-20
  • Ultralight aircraft
    UAVs and UCAVs
    Engines
    Missiles
    Miscellaneous
    People's Republic of China military aircraft engines
    Piston Engines
    Turbojets
    Turboprops/Turboshafts
    Turbofans
    Categories: