Research Article

Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm

Table 8

The mass parameters of the 4-stage rotors.

ComponentRadial datumRadial measuring surface
Unbalanced mass (g)Coordinates of unbalance mass point (mm)Unbalanced mass (g)Coordinates of unbalance mass point (mm)

Front shaft0.17(24.9657, −1.3084, 0)0.1(23.1796, 9.3652, 96.5)
LPC1.97(8.1392, 23.6380, 0)1.41(33.4590, 38.4902, 138)
HPC1.10(−50.7206, −5.3310, 0)2.34(−8.7266, 15.7432, 115)
Back shaft0.08(2.5051, −17.8248, 0)0.16(17.9835, 17.3665, 80)