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A design method of impeller inlet of supercritical carbon dioxide centrifugal compressor

The invention discloses a design method for an impeller inlet of a supercritical carbon dioxide centrifugal compressor, and aims to provide a design method capable of restricting the condensation phenomenon at the impeller inlet, maintaining geometric compactness and high thermal cycle efficiency. It includes the following steps: the total temperature at the inlet of the impeller, the total pressure at the inlet of the impeller, the target flow function, the Mach number of the machine and the inlet angle of the pre-rotation are given; the total enthalpy of the inlet of the impeller is calculated; Accept the acceleration margin empirical coefficient and steam fraction value; calculate the maximum expansion Mach number, determine the acceptable expansion Mach number according to the obtained maximum expansion Mach number; determine the impeller inlet absolute Mach number according to the obtained acceptable expansion Mach number; according to the obtained impeller inlet absolute Mach number Calculate the static parameters of the impeller inlet under actual conditions; calculate the average isentropy index, calculate the relative axial airflow angle of the optimal impeller inlet cover, calculate the relative Mach number of the impeller inlet cover, and calculate the impeller inlet shape coefficient.
Owner:TIANJIN UNIV
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