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AC/DC converter for aeronautics

  • US 7,813,147 B2
  • Filed: 09/05/2005
  • Issued: 10/12/2010
  • Est. Priority Date: 09/24/2004
  • Status: Active Grant
First Claim
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1. An AC-DC converter, comprising:

  • an autotransformer having three main inputs configured to be optionally connected to a first three-phase AC supply voltage and more than three outputs and a rectifier bridge with more than three phases connected to the outputs of the autotransformer, the autotransformer comprising a magnetic core with three branches and on each branch a main winding and auxiliary windings, the auxiliary windings of one branch being electrically connected, at one end, to taps of the main windings of this branch or of another branch and, at the other end, to a respective output of the autotransformer, all of the connections exhibiting a circular permutational symmetry allowing a balanced three-phase operation; and

    three auxiliary input terminals configured to be optionally connected to a second three-phase AC supply voltage, each one tapped on a respective winding according to a three-phase permutational symmetry, at a location where the amplitude of the voltage is Va/g when the first three-phase AC supply voltage present on the main inputs having an amplitude Va, where g is a number different from 1, and wherein these three auxiliary input terminals are connected to a three-phase connector in order to form an auxiliary three-phase input for the second three-phase AC supply voltage having an amplitude Va/g to be optionally received in replacement for said first three-phase AC supply voltage having the amplitude Va at the main inputs of the AC-DC converter with the same effect as if said first three-phase AC supply voltage were applied to said main inputs.

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