基于結(jié)構(gòu)適應(yīng)的離心壓縮機(jī)自愈調(diào)控方法研究
[Abstract]:Centrifugal compressor as the core equipment is widely used in oil and gas, large-scale coal chemical industry, deep-sea oil and gas mining and other fields. The performance of centrifugal compressor directly affects the economic benefit, safe operation and reliability of the whole unit. At present, with the rapid development of economy, resources consumption, environmental deterioration and other problems are becoming more and more serious. Therefore, how to keep compressor safe, stable and efficient operation, improve its design, operation efficiency and self-healing ability, broaden the scope of working conditions has been more and more widely concerned. In this paper, an efficient and accurate analysis and prediction model is developed by using the numerical analysis method in view of the above difficulties and hot spots. First, the unsteady coherent phenomenon between the inlet guide vane and the impeller is deeply studied by unsteady numerical simulation of the centrifugal compressor. The influence of this phenomenon on the strength of impeller structure is analyzed. It is concluded that the main reason for the failure of impeller blade is the airflow exciting force caused by this phenomenon. Secondly, the influence of the side curvature and axial length of the impeller cover on the overall performance of the compressor is discussed. The aerodynamic, mechanical and vibration modes of four kinds of impellers with different cover and side curvature were analyzed. The results show that reducing the lateral curvature of the impeller cover can obviously improve the aerodynamic performance and improve the mechanical properties of the impeller and the natural frequency of vibration. But at the same time, the rotor dynamics caused by the impeller must be considered. Finally, CFD technology is used to study the optimization design method of centrifugal compressor integral performance. The effect of blade parameters of impeller diffuser and reflux on compressor performance was analyzed by using the method of full-3D flow field analysis. On this basis, the main geometric parameters are optimized and the corresponding relationship between aerodynamic parameters and structural parameters is established. The results show that the maximum efficiency and working range of the compressor can be improved by adjusting the angle of the diffuser blade during the operation of the compressor. For the compressor of this model, the efficiency can be increased by more than 2%. After the optimization design, the overall aerodynamic performance of the compressor is obviously improved. The research results of this paper can provide an effective method for improving the design efficiency, working condition range and self-healing regulation of compressor.
【學(xué)位授予單位】:北京化工大學(xué)
【學(xué)位級(jí)別】:碩士
【學(xué)位授予年份】:2012
【分類號(hào)】:TH452
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