List of Chinese aircraft engines

Aircraft engines produced by the People's Republic of China.

Abbreviations
AbbreviationsChinesePinyinEnglish Name
HS 活塞Huó SāiPiston engine
WJ 涡桨Wō JiăngTurboprop
WP 涡喷Wō PēnTurbojet
WS 涡扇Wō ShànTurbofan
WZ 涡轴Wō ZhóuTurboshaft

Piston engines
DesignationPower OutputUsed byRemarks
HS-5 Nanchang Y-5A 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-11Licensed 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-5Licensed 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
DesignationPower OutputUsed byRemarks
WJ-5 2,162 kW (2,899 shp)Xian Y-7A 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 AG600Turboprop 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
DesignationPower OutputUsed byRemarks
WZ-5 Harbin/CHDRI Z-6 (cancelled)Turboshaft version of the WJ-5, cancelled.
WZ-6 Harbin Z-8License-built copy of the Turbomeca Turmo.
WZ-8 Harbin Z-9, Harbin Z-19Originally 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-10New turboshaft engine for the Z-10 helicopter.
WZ-10 1,800 kW (2,400 shp)Harbin Z-20Turboshaft 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 AC352New turboshaft engine under development for the Z-10 and Z-15 helicopter based on Turbomeca Ardidan 3.

Turbojet engines
DesignationThrustUsed byRemarks
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-5A 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 kNShenyang JJ-5 trainerProduced by Xi'an (XAE)
WP-6 Shenyang J-6, Nanchang Q-5Based on the Soviet Tumansky R-9BF-811 jet engine
WP-6A 29.42/36.78 kNShenyang J-6 I, Nanchang Q-5Improved WP-6
WP-6Z Nanchang J-12 (cancelled)
WP-7 43.15 kNBased 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 kNXian H-6Based 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 missileSmall turbojet engine made by China National Aero-Engine Corporation (CAREC). Similar to the Turboméca Marboré.
WP-12
WP-13 39.9/63.7 kNChengdu J-7A 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 Shenyang J-8IIProduced by Liming Aircraft Engine Company
WP-13F 44.1/66.7 kNChengdu J-7, JL-9
WP-14 Kunlun ~75 kN with afterburnShenyang J-8IIIIndigenous Chinese turbojet engine developed by Shenyang Aeroengine Research Institute.
WP-14C
Kunlun-3		 Chengdu J-7, Shenyang J-8T, Guizhou JL-9Improved WP-14
WP-15 Shenyang J-13turbojet

Turbofan engines
DesignationThrustUsed byRemarks
WS-5 35 kN (7,900 lbf)Harbin H-5 (testbed)Cancelled; turbofan modification of WP-6
WS-6 Chengdu J-9, Shenyang J-13, Nanchang Q-6Cancelled
WS-6A 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-7ALicensed 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-11Indigenous Thrust/Weight: 7.5 replacement for Saturn AL-31 and AL-31F.
WS-10G Taihang 155 kN (35,000 lbf)Chengdu J-20Modified Taihang with Thrust/Weight: 9.[3]Currently used as interim powerplant for Chengdu J-20 fighters.
WS-11 16.87 kN (3,790 lbf)Hongdu L-11Licensed version of the AI-25TLK
WS-12 Tianshan Not in use.Cancelled
WS-12B Tianshan Not in use.Cancelled. Heavier, improved WS-12. Designed to be used by the Xian JH-7B.
WS-12C Tianshan 80 kN (18,000 lbf)Not in useCancelled. Designed to be used by the Comac ARJ21
WS-13 Taishan 86.37 kN (19,420 lbf)JF-179 ton thrust. Indigenous Thrust/Weight: 7.8 upgrade for RD-93
WS-13E Taishan 100 kN (22,000 lbf)FC-31Upgraded version of WS-13. Currently used as interim powerplant for FC-31 fighters.
WS-15 Emei 180 kN (40,000 lbf)Chengdu J-20Described by Russian sources as the "18-ton" thrust, T/W: 9-10 project.[4] Under development for use by Chengdu J-20.
WS-19 110 kN (25,000 lbf)JF-17, FC-3112 ton thrust. Under development for use by JF-17 and FC-31 fighters.
Minshan 39–49 kN (8,800–11,000 lbf)Hongdu L-15Medium Thrust-Turbofan
Jiuzhai 9.8 kN (2,200 lbf)Medium Thrust-Turbofan[5]

Turbofan engines (High bypass)
DesignationThrustUsed byRemarks
WS-13A Taishan 100 kN (22,000 lbf)Not in useHigh-bypass turbofan.[6] Designed to be used by the Comac ARJ21.
WS-18 120 kN (27,000 lbf)Not in use.Developed as a replacement for the Soloviev D-30KP-2 on Xian H-6K, Xian Y-20. Development suspended.
WS-20 120–140 kN (27,000–31,000 lbf)Xian Y-20, upgraded Il-76 / Il-78A 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 was not successful.
SF-A 120 kN (27,000 lbf)Not in use.A high-bypass turbofan derived from the WS-15 core.[7] 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[8] Designed to be used by the Comac ARJ21.

See also

References
  1. "Lisunov Li-2". 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. pp. 1–1. Retrieved 7 December 2018.
  3. "Archived copy". Archived from the original on 2015-08-13. Retrieved 2010-03-31.CS1 maint: archived copy as title (link)
  4. "Archived copy". Archived from the original on 2015-08-13. Retrieved 2010-04-27.CS1 maint: archived copy as title (link)
  5. 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.
  6. "Archived copy". Archived from the original on 2016-04-19. Retrieved 2015-10-18.CS1 maint: archived copy as title (link)
  7. https://www.ainonline.com/aviation-news/air-transport/2014-01-10/china-flies-first-large-turbofan
  8. "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.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.