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).
Piston engines [ edit ] 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 [ edit ] Turboshaft engines [ edit ] 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 [ edit ] 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-1 F. 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-14CKunlun-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 [ edit ] 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 152 kN (34,000 lbf ) Modified Taihang with Thrust/Weight: 9.[4] Never been used. 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 156 kN (35,000 lbf )[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 lbf ) Hongdu L-15 Medium Thrust-Turbofan WS-19 Huangshan 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 Upgrade of the WS-13, 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) [ edit ] 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-20 147–156 kN (33,000–35,000 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 132 kN (30,000 lbf ) 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 lbf ) 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 lbf ) 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 lbf ) Not in use. Medium Thrust-Turbofan[17] Designed to be used by the Comac ARJ21 .
See also [ edit ] References [ edit ]