List of Chinese aircraft engines
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "List_of_Chinese_aircraft_engines"
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Aircraft engines produced by the People's Republic of China.

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Contents

Abbreviations

Abbreviations Chinese Pinyin English Name
HS HuoSai Piston engine
WJ WoJiang Turboprop
WP WoPen Turbojet
WS WoShan Turbofan
WZ WoZhou Turboshaft

Propeller engines

Designation Power Output Used by Remarks
HS-6 CJ-6, Y-11 A copy of the Soviet Ivchenko AI-14R engine.
WJ-5 Y-7
WJ-5A-1 SH-5
WJ-6 3170kW Y-8
WZ-5
WZ-8A Z-9 A licensed copy of Turbomeca Arriel-1C1

Turbojet engines

Designation Thrust Used by Remarks
PF-1 JJ-1 jet trainer (cancelled) A copy of the Soviet Klimov VK-1F
WP-5 J-5, H-5 A licensed copy of Soviet Klimov VK-1 turbojet, which was derived from British Rolls-Royce Derwent & Nene Engines.
WP-5D JJ-5 trainer Produced by Xi'an (XAE)
WP-6 J-6(MiG 19), Q-5 A copy of the Soviet Tumanskii R-9BF-811 jet engine
WP-6A 29.42/36.78kN J-6I(MiG 19), Q-5 Improved WP-6
WP-6Z J-12 Lightweight fighter (cancelled)
WP-7 Chinese copy of the Soviet Tumansky R-11-300 afternurning turbojet, produced by LMC
WP-7A J-7, J-8 WP-7A is a copy of the Tumanskii R-11-F-300 turbojet engine, produced by Liyang (LMC)
WP-7B/BM J-7M, JJ-7 trainer
WP-8 93.2kN H-6 A copy of Soviet Milkulin AM-3M-500 turbojet
WP-9 Y-10 (cancelled) A copy of Pratt & Whitney JT3C, cancelled
WP-10
WP-11 WZ-5 UAV & drone, HY-4 anti-ship missiles
WP-12
WP-13 J-7C/D A Chinese copy of the Tumansky R-13-300 turbojet engine
WP-13A 44.1/66.7kN
WP-13A-II J-8-II Produced by Liming Aircraft Engine Company
WP-13F 44.1/66.7kN J-7E/G
WP-14 Kunlun ~75kN with afterburn J-8-II Produced by Liming Aircraft Engine Company

Turbofan engines

Designation Thrust Used by Remarks
WS-5 Modified from WP-5 engine by adding a rear fan, cancelled
WS-6 J-9(cancelled), Q-6(cancelled) Cancelled in 1980s
WS-6A Cancelled
WS-8 Cancelled
WS-9 QinLing JH-7 A Chinese licensed copy of the Rolls-Royce Spey 202
WS-10 Developed by AVIC I Aviation Engine Institute in 1987[1]
WS-10A TaiHang 13,200kg J-10, J-11 Developed as possible replacement for AL-31/AL-31F
WS-11 JL-8
WS-13 TianShan JF-17 Developed as possible replacement for RD-93

See also

External links

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