DS215DMCBG1AZZ03A DS200DMCBG1AED DS200DMCBG1AKG | GE | Static interaction configuration

Description

DS215DMCBG1AZZ03A DS200DMCBG1AED DS200DMCBG1AKG | GE | Static interaction configuration

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The function of the compressor is to do work on the airflow, DS215DMCBG1AZZ03A to increase the pressure of the airflow. Generally, there are two types of compressors for gas turbines: axial and centrifugal.
Axial compressors have many blades, similar in shape to propeller blades, but are divided into two types: stator and rotor. The DS215DMCBG1AZZ03A rotor rotates like a propeller, pushing the airflow backwards during rotation. At this time, the pressure of the airflow will increase, and the temperature will also rise. The function of the stator is to guide the rotating airflow generated by the rotor back to the axial direction and enter the next set of rotors at the correct angle. Usually, it is an interaction configuration between a set of rotors and a set of stators, and a set of rotors and stators is called a stage.

The DS200DMCBG1AED centrifugal compressor utilizes the centrifugal force generated during impeller rotation to push the airflow outward, resulting in a pressurization effect. The DS200DMCBG1AKG first stage centrifugal compressor can have a compression ratio of several stages of axial flow compressors, which is a good choice for smaller gas turbines. However, due to the outward radiation of the airflow, it must be folded back into the interior through a significantly curved channel, resulting in significant energy consumption.
Compression ratio is the main performance indicator of compressors, and DS200DMCBG1AED refers to the ratio of air pressure after pressurization to before pressurization. Generally, gas turbines with higher compression ratios have higher efficiency, but the temperature of the air flow will rise during the compression process. Considering that the temperature that the turbine can withstand has a certain limit, a too high compression ratio is not good. The ideal compression process should be an isentropic process, but in reality, the temperature and entropy of the compressed airflow will be greater than the ideal value, while the pressure will be lower than the ideal value. The efficiency of the compressor is defined as:
DS200DMCBG1AKG, where η C represents the efficiency of the compressor, h1 represents the enthalpy before the airflow enters the compressor, h2i represents the enthalpy when the airflow leaves the compressor under ideal conditions, and h2a represents the enthalpy when the airflow leaves the compressor under actual conditions. According to the laws of thermodynamics, the efficiency of a compressor cannot exceed 1.

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