It will be able to ensure safe operation and timely replacement of the aircraft engines to quantitatively analyses compressor performance deterioration. According to the blade fouling and the increasing of tip clearance caused by compressor long time operation, we introduced deterioration factor and built the quantitatively analyses model of compressor performance deterioration based on the blade fouling and the increasing of tip clearance under different rotation rate. Results showed that with the increase of rotation rate, the pressure ratio and efficiency errors caused by the two kinds of deterioration factors dropped from 16.3%, 19.4% to less than 4%, 5%; and that caused by combined action of the two kinds of deterioration factors dropped from 17.6%, 21.6% to less than 5%, 6%. The agreement between the correlation analysis of the calculation results and the measured results proved that this model can simulate deterioration of compressor well and has a certain guiding significance to the study of multiple rotor turbofan engines.