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METHOD AND SYSTEM FOR IMPROVING PEAK POWER CAPABILITY OF AN AIRCRAFT

  • US 20100066165A1
  • Filed: 09/16/2008
  • Published: 03/18/2010
  • Est. Priority Date: 09/16/2008
  • Status: Active Grant
First Claim
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1. An electrical system, comprising:

  • a first main engine generator for providing steady state and transient power;

    a first inverter/converter controller connected to the first main engine generator for converting power from the first main engine generator;

    a first load for receiving the first main engine generator power;

    an auxiliary generator activated for parallel operation in connection with the first main engine generator during transient power demands from the electrical system, the auxiliary generator providing a supplemental power to the electrical system; and

    a supplemental inverter/converter controller connected to the auxiliary generator for converting the supplemental power into a supplemental current and for supplying the supplemental current to augment the first main engine generator power.

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