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Hybrid propulsive engine including at least one independently rotatable turbine stator

  • US 20100126178A1
  • Filed: 10/30/2009
  • Published: 05/27/2010
  • Est. Priority Date: 10/08/2008
  • Status: Abandoned Application
First Claim
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1. A hybrid propulsive engine, comprising:

  • an at least one jet engine associated with a working fluid passing there through, the at least one jet engine including a turbine section, the turbine section including an at least one turbine rotor and an at least one independently rotatable turbine stator;

    an at least one energy extraction mechanism configured to extract energy from the working fluid, and at least partially convert the that energy to electrical power; and

    an at least one torque conversion mechanism configured to convert at least a portion of the electrical power to torque, wherein the at least one independently rotatable turbine stator of the turbine section is rotatably driven at least partially responsively to the at least one torque conversion mechanism configured to convert the at least the portion of the electrical power to torque.

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