| 摘要 |
In a system for damping of phase shifts and for attenuation of harmonics between at least one energy source and at least one brushless electric motor in aircraft, the object is to connect an active circuit for attenuation of harmonics of the current and of the high-frequency waves of the three-phase current between the at least one energy source ( 1 ) and the at least one electrically commutated brushless motor ( 10 ).
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