美国GE模块IS420ESWBH3A涡轮燃机工业Mark VI控制器

美国GE模块IS420ESWBH3A涡轮燃机工业Mark VI控制器

By using cooling technology, GE turbine gas turbine improves the efficiency of the air compressor by increasing the clearance between the air compressor blades. The compressor blades are made of aluminum.

In the combustion chamber, air is blown into the combustion chamber from more than two different positions to obtain high pressure. The high pressure gas generated when it is blown in will generate eddy current and high pressure. Using compressor in the air above the vortex can make the turbine run with higher air temperature.

 This helps to reduce combustion chamber temperature and improve airflow uniformity. The compressor monitors the air temperature and flow outside the combustion chamber and improves the clearance between the blades of the air compressor (i.e. compressor unit) (for example, outside the combustion chamber) to improve efficiency and reduce carbon emissions.

This improvement makes the gas turbine combustion chamber cleaner and more efficient. The increase of surface temperature caused by the contact between swirl and gas can reduce the turbine temperature and cool the combustion chamber. As the compressor improves the gas flow uniformity and increases the combustion chamber pressure, the fuel efficiency and emissions are improved to 0.2 mg/m3). In addition, the air intake can be more smooth by using the clearance between compressor blades.