List_of_Chinese_aircraft_engines

List of Chinese aircraft engines

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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).

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"Lisunov Li-2". DC-3/Dakota Historical Society, Inc. Archived from the original on 23 February 2010. Retrieved 7 December 2018.

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

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).

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

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.

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	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.

List_of_Chinese_aircraft_engines

List of Chinese aircraft engines

Piston engines

Turboprop engines

Turboshaft engines

Turbojet engines

Turbofan engines

Turbofan engines (High bypass)

See also

References

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Designation	Thrust	Used by	Remarks
WS-5	35 kN (7,900 lb_f)	Harbin H-5 (testbed)	Cancelled; turbofan modification of WP-6
WS-6	122.2 kN (27,500 lb_f)	Chengdu J-9, Shenyang J-13, Nanchang Q-6	Cancelled
WS-6A	101.69 kN (22,860 lb_f)		Cancelled
WS-8	80 kN (18,000 lb_f)	Shanghai Y-10 (cancelled)	Cancelled
WS-9 Qinling	91.2 kN (20,500 lb_f)	Xian JH-7, JH-7A	Licensed version of Rolls-Royce Spey RB.168 Mk 202
WS-9A Qinling	97 kN (22,000 lb_f)		Improved WS-9; comparable to the French SNECMA M53-P2
WS-10A Taihang	120–140 kN (27,000–31,000 lb_f)	Chengdu J-10, Shenyang J-11	Indigenous Thrust/Weight: 7.5 replacement for Saturn AL-31 and AL-31F.
WS-10G Taihang	152 kN (34,000 lb_f)		Modified Taihang with Thrust/Weight: 9.^[4] Never been used.
WS-11	16.87 kN (3,790 lb_f)	Hongdu L-11	Licensed version of the AI-25TLK
WS-12 Tianshan	85.3 kN (19,200 lb_f)	Not in use.	Cancelled
WS-13 Taishan	86.37 kN (19,420 lb_f)	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	156 kN (35,000 lb_f)^[5]	Chengdu J-20	Described by Russian sources as the "16-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 lb_f)	Hongdu L-15	Medium Thrust-Turbofan
WS-19 Huangshan	98.1 kN (22,100 lb_f)^[7]	J-35	10 ton thrust. Under development for use by J-35 fighters.
WS-21	93.2 kN (21,000 lb_f)	J-35	Upgrade of the WS-13, currently used as interim powerplant for J-35 fighters.^[8]
Jiuzhai	9.8 kN (2,200 lb_f)		Medium Thrust-Turbofan^[9]

Designation	Thrust	Used by	Remarks
WS-13A Taishan	100 kN (22,000 lb_f)	Not in use	High-bypass turbofan.^[10] Designed to be used by the Comac ARJ21.
WS-18	120 kN (27,000 lb_f)^[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	147–156 kN (33,000–35,000 lb_f)	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	132 kN (30,000 lb_f)	Not in use.	A high-bypass turbofan derived from the WS-10 core.^[16] Designed to be used by the Comac C919.
CJ-1000A	132–147 kN (30,000–33,000 lb_f)	Not in use.	A high-bypass turbofan derived from the WS-20. Designed to be used by the Comac C919.
CJ-2000	347–372 kN (78,000–84,000 lb_f)	Not in use.	A high-bypass turbofan. Designed to be used by the Chengdu P80, CRAIC CR929.
CJ-500	80–98 kN (18,000–22,000 lb_f)	Not in use.	Medium Thrust-Turbofan^[17] Designed to be used by the Comac ARJ21.