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Aircraft engines produced by the People's Republic of China.
Abbreviations
Piston engines
Designation |
Power Output |
Used by |
Remarks |
Zhuzhou 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] |
Zhuzhou HS-6 |
|
Nanchang CJ-6, Harbin Y-11 |
Originally a 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).[1] |
Dongan HS-7 |
1,268 kW (1,700 hp) |
Harbin Z-5 |
A modified version of the Soviet Shvetsov ASh-82V, which originated in the Wright R-1820. Built by Dongan Engine Manufacturing Company (aka Harbin Engine Factory). [2] [3] |
Dongan 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). [4] |
Turboprop engines
Turboshaft engines
Designation |
Power Output |
Used by |
Remarks |
Dongan WZ-5 |
|
Harbin Z-6 |
Turboshaft version of the Dongan WJ-5, program was cancelled. |
Changzhou WZ-6 |
|
Changhe Z-8 |
Turboshaft engine. License-built copy of the Turbomeca Turmo. |
Zhuzhou WZ-8 |
|
Harbin Z-9 |
Originally license-built copies of the Turbomeca Arriel turboshaft, many modified variants of this engine were made.[1] |
Zhuzhou WZ-9 |
1,000 kW (1,350 shp) |
CAIC WZ-10 |
New turboshaft engine under development for the WZ-10 helicopter.[1] |
WZ-10 |
1,800 kW (2,414 shp) |
Harbin Z-20 |
Turboshaft engine. May power WZ-10. |
WZ-16 |
1,306 kW (1,752 hp) take-off
1,137 kW (1,525 hp) continuous |
CAIC WZ-10, Avicopter Z-15 |
New turboshaft engine under development for the WZ-10 and Z-15 helicopter based on Turbomeca Ardidan 3.[3] |
Turbojet engines
Designation |
Thrust |
Used by |
Remarks |
Shenyang PF-1 |
|
Shenyang JJ-1 |
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.[4] |
WP-5D |
26.5 kN |
Shenyang JJ-5 trainer |
Produced by Xi'an (XAE) |
Shenyang WP-6 |
|
Shenyang J-6, Nanchang Q-5 |
Based on the Soviet Tumansky R-9BF-811 jet engine |
Shenyang WP-6A |
29.42/36.78 kN |
Shenyang J-6 I, Nanchang Q-5 |
Improved WP-6 |
Shenyang WP-6Z |
|
Nanchang J-12 Lightweight fighter (cancelled) |
|
Shenyang 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 [5] |
WP-9 |
|
Shanghai Y-10 (cancelled) |
Based on the Pratt & Whitney JT3C, cancelled |
WP-10 |
|
|
|
CAREC 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 |
|
|
|
Guizhou 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.[5] |
WP-13A |
44.1/66.7 kN |
|
|
WP-13A-II |
42.7/65.9 kN [6][7] |
J-8-II |
Produced by Liming Aircraft Engine Company |
WP-13F |
44.1/66.7 kN |
Chengdu J-7, JL-9 |
|
Shenyang WP-14 Kunlun |
~75 kN with afterburn |
Shenyang J-8III |
Indigenous Chinese turbojet engine developed by Shenyang Aeroengine Research Institute.[6] |
WP-14C Kunlun-3 |
|
Chengdu J-7, Shenyang J-8T, Guizhou JL-9 |
An improved WP-14 Kunlun |
WP-15 |
Shenyang J-13 |
turbojet |
|
Turbofan engines
Designation |
Thrust |
Used by |
Remarks |
Shenyang WS-5 |
|
|
Cancelled |
Shenyang WS-6 |
|
Chengdu J-9, Shenyang J-13, Nanchang Q-6 |
Cancelled[7] |
Shenyang WS-6A |
|
|
Cancelled |
Shanghai WS-8 |
80 kN |
Shanghai Y-10 |
Cancelled[8] |
Xian WS-9 Qinling |
91.2 kN |
Xian JH-7 |
Licensed version of Rolls-Royce Spey RB.168 Mk 202 |
Xian WS-9 Qinling-2 |
9,325+ kg |
|
Improved version of the WS-9; comparable to the French SNECMA M53-P2 |
WS-10A Taihang |
13,200 kg |
Chengdu J-10, Shenyang J-11 |
Indigenous T/W: 7.5 replacement for Saturn AL-31 and AL-31F; possibly used to power new Chengdu J-20 fighters[9] |
WS-10G Taihang |
15,810 kg |
Chengdu J-20 |
Modified Taihang with T/W: 9, possibly used to power new J-20 fighters [10] |
WS-11 |
16.87 kN |
Hongdu L-11 |
Licensed version of the AI-25TLK |
WS-12 Tianshan |
|
|
Canceled |
WS-12B Tianshan |
|
Xian JH-7B |
Heavier, improved WS-12 |
WS-12C Tianshan |
8,000 kg |
Regional narrow-body jetliner ARJ21 |
|
WS-13 Taishan |
86.37 kN |
JF-17 FBC-1 |
Indigenous T/W: 7.8 upgrade for RD-93 |
WS-13A Taishan |
100 kN |
ARJ21, J-31 |
High-bypass turbofan.[11] |
WS-15 Emei |
18,350 kg |
J-20 |
Described by Russian sources as the "18-ton" thrust, T/W: 9-10 project possibly used to power new J-20 fighters.[12] |
WS-17 |
|
JF-17 |
|
WS-18 |
12,000 kg |
H-6K, Y-20 |
Developed as a replacement for the Soloviev D-30KP-2[13] |
WS-20/SF-A |
12,000 kg |
Y-20, C919 |
A high-bypass turbofan derived from the WS-10A core to power the Y-20 strategic airlifter and C919 narrow-body jetliner. |
CJ-1000A |
13,000 kg |
Y-20, C919 |
A high-bypass turbofan derived from the WS-20 to power the Y-20 strategic airlifter and C919 narrow-body jetliner. |
CJ-2000 |
35,000 kg |
Wide-body jetliner C929 |
A high-bypass turbofan.[14] |
CJ-500 |
8,000 kg |
Regional narrow-body jetliner ARJ21 |
Medium Thrust-Turbofan[15] |
References