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List of Chinese aircraft engines

April 06, 2023

Aircraft engines produced by the People's Republic of China. Most of the engines listed are produced by the Aero Engine Corporation of China (AECC).

WJ 涡桨 Wō Jiăng Turboprop
WP 涡喷 Wō Pēn Turbojet
WS 涡扇 Wō Shàn Turbofan
WZ 涡轴 Wō Zhóu Turboshaft

Piston engines

Designation Thrust Used by Remarks
HS-5 Nanchang Y-5 A version of the Shvetsov ASh-62, which itself was a modified version of the Wright R-1820. Built by the Zhuzhou Aeroengine Factory (ZEF), which is now the South Motive Power and Machinery Complex (SMPMC).[1]
HS-6 Nanchang CJ-6, Harbin Y-11 Licensed copy of the Soviet Ivchenko AI-14R engine. Built by the Zhuzhou Aeroengine Factory (ZEF). Chinese development resulted in many variants (-6A, -6B, -6C, -6D, -6E, -6K).
HS-7 1,268 kW (1,700 hp) Harbin Z-5 Licensed copy of the Soviet Shvetsov ASh-82V engine, which originated in the Wright R-1820. Built by Dongan Engine Manufacturing Company (aka Harbin Engine Factory).
HS-8 1,380 kW (1,850 hp) A modified version of the Dongan HS-7 which "combined the main body and supercharger of the HS-7 with the reduction gear and propeller drive of the Shvetsov ASh-82T". Built by Dongan Engine Manufacturing Company (aka Harbin Engine Factory).

Turboprop engines

Designation Thrust Used by Remarks
WJ-5 2,162 kW (2,899 shp) Xian Y-7 A Turboprop engine based on the Ivchenko AI-24, built by the Dongan Engine Manufacturing Company (Harbin Engine Factory) in several variants.
WJ-6 3,170 kW (4,250 shp) Shaanxi Y-8, AVIC AG600 Turboprop engine; a license-built copy of the Ivchenko AI-20.
WJ-9 turboprop derived from the Turbomeca Arriel and WZ-8 turboshaft engines

Turboshaft engines

Designation Thrust Used by Remarks
WZ-5 Harbin/CHDRI Z-6 (cancelled) Turboshaft version of the WJ-5, cancelled.
WZ-6 Harbin Z-8 License-built copy of the Turbomeca Turmo.
WZ-8 Harbin Z-9, Harbin Z-19 Originally license-built copies of the Turbomeca Arriel turboshaft, many modified variants of this engine were made.
WZ-9 1,000 kW (1,300 shp) CAIC Z-10 New turboshaft engine for the Z-10 helicopter.
WZ-10 1,800 kW (2,400 shp) Harbin Z-20 Turboshaft engine. May power Z-10.
WZ-16 1,243 kW (1,667 shp) take-off
1,137 kW (1,525 shp) continuous		 CAIC Z-10, Avicopter AC352 New turboshaft engine under development for the Z-10 and Z-15 helicopter based on Turbomeca Ardidan 3.

Turbojet engines

Designation Thrust Used by Remarks
PF-1 Shenyang JJ-1 (cancelled) A small turbojet engine based on the WP-5, which was a copy of the Soviet Klimov VK-1F.
WP-5 Shenyang J-5, Harbin H-5 A licensed copy of Soviet Klimov VK-1 turbojet, which was derived from the Rolls-Royce Nene engine. Built at the Shenyang Liming Aircraft Engine Company.
WP-5D 26.5 kN Shenyang JJ-5 trainer Produced by Xi'an (XAE)
WP-6 Shenyang J-6, Nanchang Q-5 Based on the Soviet Tumansky R-9BF-811 jet engine
WP-6A 29.42/36.78 kN Shenyang J-6 I, Nanchang Q-5 Improved WP-6
WP-6Z Nanchang J-12 (cancelled)
WP-7 43.15 kN Based on the Soviet Tumansky R-11-300 afterburning turbojet. Many upgrades and new variants have been developed from the basic engine.
WP-8 93.2 kN Xian H-6 Based on the Mikulin AM-3M-500 turbojet.[2]
WP-9 Shanghai Y-10 (cancelled) Based on the Pratt & Whitney JT3C, cancelled
WP-10
WP-11 Beijing WZ-5, HY-4 anti-ship missile Small turbojet engine made by China National Aero-Engine Corporation (CAREC). Similar to the Turboméca Marboré.
WP-12
WP-13 39.9/63.7 kN Chengdu J-7 A Chinese engine based on the Tumansky R-13-300 turbojet. Several variants were made.
WP-13A 44.1/66.7 kN
WP-13A-II 42.7/65.9 kN [1][2] Shenyang J-8II Produced by Liming Aircraft Engine Company
WP-13F 44.1/66.7 kN Chengdu J-7, JL-9 Produced by CHINA NATIONAL AERO TECHNOLOGY IMPORT AND EXPORT CORPORATION
WP-14
Kunlun 		~75 kN with afterburn Shenyang J-8III Indigenous Chinese turbojet engine developed by Shenyang Aeroengine Research Institute.
WP-14C
Kunlun-3 		Chengdu J-7, Shenyang J-8T, Guizhou JL-9 Improved WP-14
WP-15 81.4 kN/122.58 kN[3] Shenyang J-13 (cancelled) Based on the Soviet Tumansky R-29-300 turbojet engine.

Turbofan engines

Designation Thrust Used by Remarks
WS-5 35 kN (7,900 lbf) Harbin H-5 (testbed) Cancelled; turbofan modification of WP-6
WS-6 122.2 kN (27,500 lbf) Chengdu J-9, Shenyang J-13, Nanchang Q-6 Cancelled
WS-6A 101.69 kN (22,860 lbf) Cancelled
WS-8 80 kN (18,000 lbf) Shanghai Y-10 (cancelled) Cancelled
WS-9 Qinling 91.2 kN (20,500 lbf) Xian JH-7, JH-7A Licensed version of Rolls-Royce Spey RB.168 Mk 202
WS-9A Qinling 97 kN (22,000 lbf) Improved WS-9; comparable to the French SNECMA M53-P2
WS-10A Taihang 120–140 kN (27,000–31,000 lbf) Chengdu J-10, Shenyang J-11 Indigenous Thrust/Weight: 7.5 replacement for Saturn AL-31 and AL-31F.
WS-10G Taihang 155 kN (35,000 lbf) Chengdu J-20 Modified Taihang with Thrust/Weight: 9.[4] Currently used as interim powerplant for Chengdu J-20 fighters.
WS-11 16.87 kN (3,790 lbf) Hongdu L-11 Licensed version of the AI-25TLK
WS-12 Tianshan 85.3 kN (19,200 lbf) Not in use. Cancelled
WS-13 Taishan 86.37 kN (19,420 lbf) CAC/PAC JF-17, Hongdu GJ-11, CASC CH-7 9 ton thrust. Indigenous Thrust/Weight: 7.8 upgrade for RD-93
WS-15 Emei 181.37 kN (40,770 lbf)[5] Chengdu J-20 Described by Russian sources as the "18-ton" thrust, T/W: 9-10 project.[6] Under development for use by Chengdu J-20.
WS-17 Minshan 39–49 kN (8,800–11,000 lbf) Hongdu L-15 Medium Thrust-Turbofan
WS-19 98.1 kN (22,100 lbf)[7] J-35 10 ton thrust. Under development for use by J-35 fighters.
WS-21 93.2 kN (21,000 lbf) J-35 Currently used as interim powerplant for J-35 fighters.[8]
Jiuzhai 9.8 kN (2,200 lbf) Medium Thrust-Turbofan[9]

Turbofan engines (High bypass)

Designation Thrust Used by Remarks
WS-13A Taishan 100 kN (22,000 lbf) Not in use High-bypass turbofan.[10] Designed to be used by the Comac ARJ21.
WS-18 120 kN (27,000 lbf)[11] Derivative[11] or copy of Soloviev D-30KP-2[12] for Xian H-6K and Xian Y-20.[11] May be superseded by WS-20.[12]
WS-20 120–140 kN (27,000–31,000 lbf) Xian Y-20,[13] Il-76 test bed[14] A high-bypass turbofan based on the core of the low-bypass turbofan WS-10A. Undergoing flight test on Y-20 and Il-76. Designed to be used by Comac C919 and CRAIC CR929 but still currently in testing.[15]
SF-A 120 kN (27,000 lbf) Not in use. A high-bypass turbofan derived from the WS-15 core.[16] Designed to be used by the Comac C919.
CJ-1000A 98–196 kN (22,000–44,000 lbf) Not in use. A high-bypass turbofan derived from the WS-20. Designed to be used by the Comac C919.
CJ-2000 340 kN (76,000 lbf) Not in use. A high-bypass turbofan. Designed to be used by the Chengdu P80, CRAIC CR929.
CJ-500 78 kN (18,000 lbf) Not in use. Medium Thrust-Turbofan[17] Designed to be used by the Comac ARJ21.

See also

References

  1. ^ . DC-3/Dakota Historical Society, Inc. Archived from the original on 23 February 2010. Retrieved 7 December 2018.
  2. ^ Kopp, Carlo (7 July 2007). "The PLA-AF's Aerial Refuelling Programs". Air Power Australia. p. 1. Retrieved 7 December 2018.
  3. ^ (in Chinese). Afwing.com. Archived from the original on 2016-03-09. Retrieved 2021-07-12.
  4. ^ . Archived from the original on 2015-08-13. Retrieved 2010-03-31.
  5. ^ "聚焦航发控制系统主业，增长提速巩固龙头地位" (PDF) (in Simplified Chinese). 中泰证券. 2021-10-08. p. 25. Retrieved 2021-12-01.
  6. ^ . Archived from the original on 2015-08-13. Retrieved 2010-04-27.
  7. ^ 曾品潔 (2023-02-09). "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 2023-02-26.
  8. ^ Joseph Trevithick (2022-07-22). "Our Best Look Yet At China's J-35 Carrier-Capable Stealth Fighter". The Drive. Retrieved 2023-02-26.
  9. ^ Lei, Zhao (15 November 2012). "Aviation industry flies into future|Economy|chinadaily.com.cn". europe.chinadaily.com.cn. China Daily Information Co. China Daily Europe. Retrieved 7 December 2018.
  10. ^ . Archived from the original on 2016-04-19. Retrieved 2015-10-18.
  11. ^ a b c Fisher, Richard (27 May 2015). "ANALYSIS: Can China break the military aircraft engine bottleneck?". FlightGlobal. Retrieved 2 November 2021.
  12. ^ a b Wood, Peter; Wahlstrom, Alden; Cliff, Roger (March 2020). China's Aeroengine Industry (PDF). United States Air Force Air University China Aerospace Studies Institute. p. 32. ISBN 9798637786664.
  13. ^ "Chinese WS20 engine likely entering operational service". Janes.com. Retrieved 2023-03-24.
  14. ^ Donald, David. "China Flies First Large Turbofan". Aviation International News. Retrieved 2023-03-24.
  15. ^ "Indigenous engines for Y-20 proceeding well: aircraft designer".
  16. ^ "China Flies First Large Turbofan".
  17. ^ "中國商用發動機公司曝中國正研窄體飛機ARJ-21發動機及未來發動機計劃". Retrieved 7 December 2018.

April 06, 2023
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Aircraft engines produced by the People s Republic of China Most of the engines listed are produced by the Aero Engine Corporation of China AECC WJ 涡桨 Wō Jiăng TurbopropWP 涡喷 Wō Pen TurbojetWS 涡扇 Wō Shan TurbofanWZ 涡轴 Wō Zhou TurboshaftContents 1 Piston engines 2 Turboprop engines 3 Turboshaft engines 4 Turbojet engines 5 Turbofan engines 6 Turbofan engines High bypass 7 See also 8 ReferencesPiston engines EditDesignation Thrust Used by RemarksHS 5 Nanchang Y 5 A version of the Shvetsov ASh 62 which itself was a modified version of the Wright R 1820 Built by the Zhuzhou Aeroengine Factory ZEF which is now the South Motive Power and Machinery Complex SMPMC 1 HS 6 Nanchang CJ 6 Harbin Y 11 Licensed copy of the Soviet Ivchenko AI 14R engine Built by the Zhuzhou Aeroengine Factory ZEF Chinese development resulted in many variants 6A 6B 6C 6D 6E 6K HS 7 1 268 kW 1 700 hp Harbin Z 5 Licensed copy of the Soviet Shvetsov ASh 82V engine which originated in the Wright R 1820 Built by Dongan Engine Manufacturing Company aka Harbin Engine Factory HS 8 1 380 kW 1 850 hp A modified version of the Dongan HS 7 which combined the main body and supercharger of the HS 7 with the reduction gear and propeller drive of the Shvetsov ASh 82T Built by Dongan Engine Manufacturing Company aka Harbin Engine Factory Turboprop engines EditThis section does not cite any sources Please help improve this section by adding citations to reliable sources Unsourced material may be challenged and removed August 2022 Learn how and when to remove this template message Designation Thrust Used by RemarksWJ 5 2 162 kW 2 899 shp Xian Y 7 A Turboprop engine based on the Ivchenko AI 24 built by the Dongan Engine Manufacturing Company Harbin Engine Factory in several variants WJ 6 3 170 kW 4 250 shp Shaanxi Y 8 AVIC AG600 Turboprop engine a license built copy of the Ivchenko AI 20 WJ 9 turboprop derived from the Turbomeca Arriel and WZ 8 turboshaft enginesTurboshaft engines EditThis section does not cite any sources Please help improve this section by adding citations to reliable sources Unsourced material may be challenged and removed August 2022 Learn how and when to remove this template message Designation Thrust Used by RemarksWZ 5 Harbin CHDRI Z 6 cancelled Turboshaft version of the WJ 5 cancelled WZ 6 Harbin Z 8 License built copy of the Turbomeca Turmo WZ 8 Harbin Z 9 Harbin Z 19 Originally license built copies of the Turbomeca Arriel turboshaft many modified variants of this engine were made WZ 9 1 000 kW 1 300 shp CAIC Z 10 New turboshaft engine for the Z 10 helicopter WZ 10 1 800 kW 2 400 shp Harbin Z 20 Turboshaft engine May power Z 10 WZ 16 1 243 kW 1 667 shp take off1 137 kW 1 525 shp continuous CAIC Z 10 Avicopter AC352 New turboshaft engine under development for the Z 10 and Z 15 helicopter based on Turbomeca Ardidan 3 Turbojet engines EditDesignation Thrust Used by RemarksPF 1 Shenyang JJ 1 cancelled A small turbojet engine based on the WP 5 which was a copy of the Soviet Klimov VK 1F WP 5 Shenyang J 5 Harbin H 5 A licensed copy of Soviet Klimov VK 1 turbojet which was derived from the Rolls Royce Nene engine Built at the Shenyang Liming Aircraft Engine Company WP 5D 26 5 kN Shenyang JJ 5 trainer Produced by Xi an XAE WP 6 Shenyang J 6 Nanchang Q 5 Based on the Soviet Tumansky R 9BF 811 jet engineWP 6A 29 42 36 78 kN Shenyang J 6 I Nanchang Q 5 Improved WP 6WP 6Z Nanchang J 12 cancelled WP 7 43 15 kN Based on the Soviet Tumansky R 11 300 afterburning turbojet Many upgrades and new variants have been developed from the basic engine WP 8 93 2 kN Xian H 6 Based on the Mikulin AM 3M 500 turbojet 2 WP 9 Shanghai Y 10 cancelled Based on the Pratt amp Whitney JT3C cancelledWP 10WP 11 Beijing WZ 5 HY 4 anti ship missile Small turbojet engine made by China National Aero Engine Corporation CAREC Similar to the Turbomeca Marbore WP 12WP 13 39 9 63 7 kN Chengdu J 7 A Chinese engine based on the Tumansky R 13 300 turbojet Several variants were made WP 13A 44 1 66 7 kNWP 13A II 42 7 65 9 kN 1 2 Shenyang J 8II Produced by Liming Aircraft Engine CompanyWP 13F 44 1 66 7 kN Chengdu J 7 JL 9 Produced by CHINA NATIONAL AERO TECHNOLOGY IMPORT AND EXPORT CORPORATIONWP 14Kunlun 75 kN with afterburn Shenyang J 8III Indigenous Chinese turbojet engine developed by Shenyang Aeroengine Research Institute WP 14CKunlun 3 Chengdu J 7 Shenyang J 8T Guizhou JL 9 Improved WP 14WP 15 81 4 kN 122 58 kN 3 Shenyang J 13 cancelled Based on the Soviet Tumansky R 29 300 turbojet engine Turbofan engines EditDesignation Thrust Used by RemarksWS 5 35 kN 7 900 lbf Harbin H 5 testbed Cancelled turbofan modification of WP 6WS 6 122 2 kN 27 500 lbf Chengdu J 9 Shenyang J 13 Nanchang Q 6 CancelledWS 6A 101 69 kN 22 860 lbf CancelledWS 8 80 kN 18 000 lbf Shanghai Y 10 cancelled CancelledWS 9 Qinling 91 2 kN 20 500 lbf Xian JH 7 JH 7A Licensed version of Rolls Royce Spey RB 168 Mk 202WS 9A Qinling 97 kN 22 000 lbf Improved WS 9 comparable to the French SNECMA M53 P2WS 10A Taihang 120 140 kN 27 000 31 000 lbf Chengdu J 10 Shenyang J 11 Indigenous Thrust Weight 7 5 replacement for Saturn AL 31 and AL 31F WS 10G Taihang 155 kN 35 000 lbf Chengdu J 20 Modified Taihang with Thrust Weight 9 4 Currently used as interim powerplant for Chengdu J 20 fighters WS 11 16 87 kN 3 790 lbf Hongdu L 11 Licensed version of the AI 25TLKWS 12 Tianshan 85 3 kN 19 200 lbf Not in use CancelledWS 13 Taishan 86 37 kN 19 420 lbf CAC PAC JF 17 Hongdu GJ 11 CASC CH 7 9 ton thrust Indigenous Thrust Weight 7 8 upgrade for RD 93WS 15 Emei 181 37 kN 40 770 lbf 5 Chengdu J 20 Described by Russian sources as the 18 ton thrust T W 9 10 project 6 Under development for use by Chengdu J 20 WS 17 Minshan 39 49 kN 8 800 11 000 lbf Hongdu L 15 Medium Thrust TurbofanWS 19 98 1 kN 22 100 lbf 7 J 35 10 ton thrust Under development for use by J 35 fighters WS 21 93 2 kN 21 000 lbf J 35 Currently used as interim powerplant for J 35 fighters 8 Jiuzhai 9 8 kN 2 200 lbf Medium Thrust Turbofan 9 Turbofan engines High bypass EditDesignation Thrust Used by RemarksWS 13A Taishan 100 kN 22 000 lbf Not in use High bypass turbofan 10 Designed to be used by the Comac ARJ21 WS 18 120 kN 27 000 lbf 11 Derivative 11 or copy of Soloviev D 30KP 2 12 for Xian H 6K and Xian Y 20 11 May be superseded by WS 20 12 WS 20 120 140 kN 27 000 31 000 lbf Xian Y 20 13 Il 76 test bed 14 A high bypass turbofan based on the core of the low bypass turbofan WS 10A Undergoing flight test on Y 20 and Il 76 Designed to be used by Comac C919 and CRAIC CR929 but still currently in testing 15 SF A 120 kN 27 000 lbf Not in use A high bypass turbofan derived from the WS 15 core 16 Designed to be used by the Comac C919 CJ 1000A 98 196 kN 22 000 44 000 lbf Not in use A high bypass turbofan derived from the WS 20 Designed to be used by the Comac C919 CJ 2000 340 kN 76 000 lbf Not in use A high bypass turbofan Designed to be used by the Chengdu P80 CRAIC CR929 CJ 500 78 kN 18 000 lbf Not in use Medium Thrust Turbofan 17 Designed to be used by the Comac ARJ21 See also EditAero Engine Corporation of ChinaReferences Edit Lisunov Li 2 DC 3 Dakota Historical Society Inc Archived from the original on 23 February 2010 Retrieved 7 December 2018 Kopp Carlo 7 July 2007 The PLA AF s Aerial Refuelling Programs Air Power Australia p 1 Retrieved 7 December 2018 歼击 13 型飞机 in Chinese Afwing com Archived from the original on 2016 03 09 Retrieved 2021 07 12 International Assessment and Strategy Center gt Research gt October Surprises in Chinese Aerospace Archived from the original on 2015 08 13 Retrieved 2010 03 31 聚焦航发控制系统主业 增长提速巩固龙头地位 PDF in Simplified Chinese 中泰证券 2021 10 08 p 25 Retrieved 2021 12 01 International Assessment and Strategy Center gt Research gt October Surprises in Chinese Aerospace Archived from the original on 2015 08 13 Retrieved 2010 04 27 曾品潔 2023 02 09 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 2023 02 26 Joseph Trevithick 2022 07 22 Our Best Look Yet At China s J 35 Carrier Capable Stealth Fighter The Drive Retrieved 2023 02 26 Lei Zhao 15 November 2012 Aviation industry flies into future Economy chinadaily com cn europe chinadaily com cn China Daily Information Co China Daily Europe Retrieved 7 December 2018 WS13 Archived from the original on 2016 04 19 Retrieved 2015 10 18 a b c Fisher Richard 27 May 2015 ANALYSIS Can China break the military aircraft engine bottleneck FlightGlobal Retrieved 2 November 2021 a b Wood Peter Wahlstrom Alden Cliff Roger March 2020 China s Aeroengine Industry PDF United States Air Force Air University China Aerospace Studies Institute p 32 ISBN 9798637786664 Chinese WS20 engine likely entering operational service Janes com Retrieved 2023 03 24 Donald David China Flies First Large Turbofan Aviation International News Retrieved 2023 03 24 Indigenous engines for Y 20 proceeding well aircraft designer China Flies First Large Turbofan 中國商用發動機公司曝中國正研窄體飛機ARJ 21發動機及未來發動機計劃 Retrieved 7 December 2018 Retrieved from https en wikipedia org w index php title List of Chinese aircraft engines amp oldid 1147657540, wikipedia, wiki, book, books, library,

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