Fault detection and location method for rotary rectifier of aviation brushless electric excitation synchronous motor
A technology of rotating rectifiers and synchronous motors, which is applied in the direction of motor generator testing, instruments, and measuring electronics. It can solve the problems of insufficient reflection speed, large number of data samples, and processing speed to be improved, and achieve the effect of fault diagnosis and positioning.
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[0033] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0034] (1) For aviation brushless electric excitation synchronous motors (see figure 1 ), use Simulink offline simulation to obtain the stator side voltage and current of the main exciter under various states of the rotating rectifier (a diode D1-D6 is faulty and normal respectively), and estimate the rotor current of the main exciter through the stator flux linkage, and estimate the formula (1 )as follows;
[0035]
[0036] In the formula:
[0037]
[0038] Among them: u eαs , u eβs is the exciter stator voltage; i eαs i eβs is the exciter stator current; R es , L es is the stator resistance and inductance of the exciter; M esr is the stator-rotor mutual inductance; θ er is the rotor position; i ear i ebr i ecr is the exciter rotor current;
[0039] (2) Perform FFT analysis on the estimated rotor current to obtain the waveform amplitude of 1-5...
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