Briefly about JDEC engines:
JDEC is one of the biggest engine producers in Asia, as a part of the giant company CNPC (China National Petroleum Corp.), JDEC has always had the means and facilities to pursue the highest international standards required by the modern world. In the start JDEC had a cooperation with American Waukasha. the new engines are however designed and developed in cooperation with AVL in Austria, an international recognized design and engineering company which has also designed the new engines for both MAN and Wartsila.
Further, as a licensor of German MAN and as a producer of MAN engines, the production facilities, and most important, The QC and material testing procedures guarantee a production and a product of international standard, and as you can see of the below logos, the highest quality of components are used, like Mahler pistons (Germany), Miba bearings (Austria) Woodward Electronic governors (USA) just to mention a few of the components.
Our gas engine 26/32 is highly supercharged, high-power medium-speed engine with low consumption and high reliability. Our company has the 100% intellectual property right. We provide a variety of configurations for the gas engine including 6L26/32, 9L26/32, 12V26/32, and 16V26/32 types. with an output power of 233kW per cylinder,
The gas engine is applicable to projects of natural gas pipeline network, booster pump station, compressor station for the underground natural gas storage, and the marine. It can also meet the power requirement in large gas-fired power station, distributed energy system, and other energy saving and low-emission projects.
Technical Specifications
Type | Four-stroke, water cooled, radial flow turbocharger, intake intercooled, precombustion chamber, multi-point injection, air-fuel ratio control | |||||
Number and arrangement of cylinders | 12-cylinder, V type, 60° | 16-cylinder, V type, 60° | ||||
Cylinder diameter×Stroke | mm | 260×320 | ||||
Displacement of a single cylinder | L | 17 | ||||
Compression ratio | 11:1 | |||||
Continuous power | kW | 2798 | 3730 | |||
Continuous revolution | r/min | 1000 | ||||
Min. operating speed (steady-state) r/min | 350 | |||||
Under the operating condition of continuous power | Fuel thermal efficiency | g/kW.h | 40% | |||
Specific oil consumption | g/kW.h | 0.5 | ||||
Mean effective pressure | MPa | 1.65 | ||||
Mean speed of piston m/s | 10.7 | |||||
Exhaust gas temperature (after the turbo) ℃ | 620 | |||||
Smoke intensity FSU | ≤0.5 | |||||
Noise dB(A) | ≤120 | |||||
Emission g/Nm³ | 0.5g/Nm³ | |||||
Direction of rotation | Counterclockwise (face the flywheel end) | |||||
Type of fuel | Natural gas, marsh gas | |||||
Cooling mode | Forced cooling | |||||
Lubrication mode | Pressure lubrication | |||||
Starting mode | Air motor | |||||
Overall size (l×b×h) mm | 5748×2238×3255 | 6748×2353×3255 |