Peng-cheng PU, Kai ZHANG, Jin-peng YU, et al. On-line balancing of high-speed magnetic suspended flywheel system under force free control of imbalance[J]. Optics and precision engineering, 2017, 25(7): 1796-1806.
DOI:
Peng-cheng PU, Kai ZHANG, Jin-peng YU, et al. On-line balancing of high-speed magnetic suspended flywheel system under force free control of imbalance[J]. Optics and precision engineering, 2017, 25(7): 1796-1806. DOI: 10.3788/OPE.20172507.1796.
On-line balancing of high-speed magnetic suspended flywheel system under force free control of imbalance
A kind of field dynamic balancing method under force free control is proposed aiming at the unbalance of high-speed magnetic suspended flywheel system. It turns out that the low-speed field balancing in the air environment can replace the high-speed field balancing in the vacuum environment with high-efficiency and high-accuracy. By analyzing the unbalance model of the magnetic suspended rotor system and comparing the correction-masses under different unbalance control mode
it is found that under the free control mode
the synchronous component of control current is zero and the electromagnetic force is a linear function of the rotor displacement within linearization range. Therefore
the correction-masses can be calculated from the synchronous displacement response of the rotor in force free mode. The force free controller of magnetic bearing is designed to make the rotor spinning around its principal axis of inertial
and synchronous displacement response of the rotor is extracted to compute the correction-masses. As there exists some deviation between the theoretical and actual value of the system parameters
a trial weight is completed to correct the convention coefficient matrix. The experimental results show that the conversion coefficient matrix can be re-calibrated after a start-up test. And after the second balancing
the high-accuracy field balancing can be achieved. The orbits of rotor shaft centerline reduce significantly and the synchronous displacement response of the rotor decrease by 77.29% and 94.14% respectively. The rotor operating condition with 500Hz rotation speed in vacuum environment is in close proximity to low-speed condition
and it further validates the proposed method.
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references
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