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Aircraft engines produced by the People's Republic of China .
Abbreviations
Piston engines
Designation
Power Output
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).[1]
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 ). [2] [3]
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
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.[1]
WZ-9
1,000 kW (1,300 shp)
CAIC Z-10
New turboshaft engine under development for the Z-10 helicopter.[1]
WZ-10
1,800 kW (2,400 shp)
Harbin Z-20
Turboshaft engine. May power WZ-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.[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-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 .[4]
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 [5]
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.[5]
WP-13A
44.1/66.7 kN
WP-13A-II
42.7/65.9 kN [6] [7]
Shenyang J-8II
Produced by Liming Aircraft Engine Company
WP-13F
44.1/66.7 kN
Chengdu J-7 , JL-9
WP-14 Kunlun
~75 kN with afterburn
Shenyang J-8III
Indigenous Chinese turbojet engine developed by Shenyang Aeroengine Research Institute .[6]
WP-14CKunlun-3
Chengdu J-7 , Shenyang J-8T , Guizhou JL-9
Improved WP-14
WP-15
Shenyang J-13
turbojet
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
Chengdu J-9 , Shenyang J-13 , Nanchang Q-6
Cancelled[7]
WS-6A
Cancelled
WS-8
80 kN (18,000 lbf )
Shanghai Y-10 (cancelled)
Cancelled[8]
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 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
155 kN (35,000 lbf )
Chengdu J-20
Modified Taihang with T/W: 9, possibly used to power new J-20 fighters [10]
WS-11
16.87 kN (3,790 lbf )
Hongdu L-11
Licensed version of the AI-25TLK
WS-12 Tianshan
Cancelled
WS-12B Tianshan
Xian JH-7B
Heavier, improved WS-12
WS-12C Tianshan
80 kN (18,000 lbf )
Comac ARJ21
WS-13 Taishan
86.37 kN (19,420 lbf )
JF-17
Indigenous T/W: 7.8 upgrade for RD-93
WS-13A Taishan
100 kN (22,000 lbf )
Comac ARJ21
High-bypass turbofan.[11]
WS-15 Emei
180 kN (40,000 lbf )
Chengdu 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
120 kN (27,000 lbf )
Xian H-6K , Xian Y-20
Developed as a replacement for the Soloviev D-30KP-2 [13]
SF-A
120 kN (27,000 lbf )
Xian Y-20 , Comac C919
A high-bypass turbofan derived from the WS-10A core.
WS-20
120–140 kN (27,000–31,000 lbf )
Xian Y-20 , Comac C919 , CRAIC CR929 , upgraded Il-76 / Il-78
A high-bypass turbofan based on the core of the low-bypass turbofan WS-10A .
CJ-1000A
98–196 kN (22,000–44,000 lbf )
Comac C919
A high-bypass turbofan derived from the WS-20.
CJ-2000
340 kN (76,000 lbf )
Chengdu P80, CRAIC CR929
A high-bypass turbofan.[14]
CJ-500
78 kN (18,000 lbf )
Comac ARJ21
Medium Thrust-Turbofan[15]
Minshan
39–49 kN (8,800–11,000 lbf )
Hongdu L-15
Medium Thrust-Turbofan[16]
Jiuzhai
9.8 kN (2,200 lbf )
Medium Thrust-Turbofan[17]
See also
Aero Engine Corporation of China
References