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Aircraft engines produced by the People's Republic of China.
[edit] Abbreviations
[edit] 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 |
[edit] 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 |
[edit] 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 |
[edit] See also
[edit] External links
