轮毂及隔板型式对旋转冲压压缩转子性能的影响研究
[Abstract]:In order to improve the performance of gas turbine, the development of supersonic / transonic compressor is very important. Rotary press compression rotor is a new type of supersonic compressor rotor which compresses the incoming flow by shock wave. It has the advantages of high single-stage pressure ratio, simple structure, light weight, small volume and so on. In order to improve the overall performance of rotary press compression rotor and obtain the influence mechanism of different wheel hub and partition type on the flow inside the runner, different modification schemes are obtained by changing the wheel hub and partition type. Numerical method is used to study the modification scheme with different wheel hub and partition type. Firstly, different modification schemes are obtained by changing the compression surface, changing the shape of the diffuser along the flow direction and synthetically changing the hub type. The results show that changing the shape of compression surface along the direction of flow can change the shape of shock wave and reduce the loss of shock wave, but it can not obviously improve the overall performance of rotary press compression rotor. The shape of the flow direction of the diffuser surface has a certain influence on the performance of the rotary press compression rotor. When the length is the same, with the decrease of the initial expansion angle, the overall performance of the rotor, such as the booster ratio, the efficiency and so on, will be improved to a certain extent. But the whole ascension is not obvious; Under the condition of the same initial expansion angle, increasing the length of the bearing section can increase the booster ratio of the rotary stamping compression rotor, while increasing the length of the diffuser surface can improve the efficiency and the total pressure recovery coefficient. Local modification of hub type can not obviously improve the overall performance of rotary press compression rotor. Secondly, different modification schemes are obtained by changing the front and back segments of the baffle and synthetically changing the type of the diaphragm of the rotary press compression rotor, and the numerical study is carried out on them. It is found that changing the type of the front section of the baffle can change the shock wave of the front edge of the diaphragm, and then change the inlet air flow rate and the incoming flow quality of the rotary punching compression rotor, enhance the pressurization capacity of the rotary punching compression rotor and reduce the flow loss inside the channel. It has a positive effect on the overall performance of rotary press compression rotor. The separation condition at the outlet of the left septum of the rotary press compression rotor can be changed by changing the type of the posterior section of the partition, and the separation condition of each scheme is gradually improved with the moving back of the starting point of the tail edge. However, there is a maximum supercharging capacity point in the process of moving backward at the starting point of the tail edge, beyond which the airflow will inflate at the outlet of the right diaphragm, which will seriously affect the turbocharging capacity of the rotary press compression rotor. A good modification can also be obtained by folding the left partition into the inner of the runner. Under the condition of considering the influence of the front and back section of the diaphragm on the rotary press compression rotor and ensuring the strength of the partition board, a better modification scheme can be obtained by comprehensive modification of the partition plate.
【学位授予单位】:大连海事大学
【学位级别】:硕士
【学位授予年份】:2016
【分类号】:TK473
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