Updated: 05-Apr-2020
This is the Liming Eng. Manufacturing Corp. Important Chinese industry with extensive experience in the manufacture of aviation engines. They started to build engines in 1954-7 with the WP-5 (VK-1F), licensed by Klimov.
-Thereafter they made the WP-5A (VK-1A).
-Based on the WP-5, the indigenous PF-1A engine developed at the Shengyang Design Office, or (SADO) was made.
-Since 1996 it builds the Turbomeca Arriel under license, as WP-8D.
“WP-5 (VK-1-)”
-The WP-6 is the Tumanskii RD-9BF, and is built since 1958, later they made the WP-6A and WP-6B versions, the latter with 9,290 lbf of maximum thrust with afterburner.
“WP-6”
-The WP-7 is the Tumanskii R-11F, manufactured under license and capable of reaching Mach 2.
“WP-7”
-In the illustration there is no afterburner. The first WP-7 came out in 1965 at 8,600 lbf. dry and 12,600 lbf with afterburner.
-WP-7A was somewhat overpowered.
-The latest version of this LM engine is the 14,300 lbf WP-7F. maximum with afterburner.
“WS-6”
-WS-6 is a more powerful, self-designed turbofan for 27,500 lbf of thrust.
-Although it was put on the board in the mid-1960s, it was not approved until 1980, due to the fact that there was a halt in all China of at least 10 years due to the Cultural Revolution.
Engines of LM
Model: PF-1
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: WP-5, -5A
Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"WP-5 (VK-1-)"
Model: WP-6, -6A, -6B
Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 9290
Weight:
WP-6B, 9,290 lbf max thrust with afterburner.
"LM, WP-6"
Model: WP-7, -7A, -7F
Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
Tumanskii R-11F under license.
The first WP-7 delivered 8,600 lbf dry and 12,600 lbf with afterburner.
The latest version (WP-7F) delivered 14,300 lbf maximum with afterburner.
"LM, WP-7"
Model: WP-8D
Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
Model: WS-6, -6A
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 27500 Lbf
Weight:
"LM, WS-6"