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Active turbine combustion parameter control system and method

  • US 20020063479A1
  • Filed: 10/11/2001
  • Published: 05/30/2002
  • Est. Priority Date: 10/11/2000
  • Status: Abandoned Application
First Claim
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1. A turbogenerator, comprising:

  • a compressor configured to compress a fuel oxidizer;

    a combustor connected to an exhaust of the compressor and configured both to receive the fuel oxidizer and a fuel and to combust the fuel and the fuel oxidizer into a combusted gas;

    a fuel supplier configured to control fuel droplet sizes of the fuel supplied into the combustor to prevent flameout of the turbogenerator;

    a turbine attached to an exhaust of said combustor and configured to convert heat from the combusted gas into rotational energy;

    a motor/generator configured to convert said rotational energy into electrical energy; and

    a common shaft connecting said turbine, said compressor, and said motor/generator, wherein said common shaft is configured to rotate said turbine, said compressor, and said motor/generator.

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