Hybrid propulsive engine including at least one independently rotatable compressor stator

A hybrid propulsive method, comprising:

• providing a flow of a working fluid through at least a portion of an at least one jet engine, wherein the at least one jet engine includes an at least one compressor section having an at least one independently rotatable compressor stator that rotates about a central axis of the jet engine;
• extracting energy at least partially in the form of electrical power from the working fluid;
• converting at least a portion of the electrical power to torque;
• and
• rotating the at least one independently rotatable compressor stator at least partially responsive to the converting the at least a portion of the electrical power to torque.

A hybrid propulsive method, comprising:

• providing a flow of a working fluid through at least a portion of an at least one jet engine;
• extracting energy from the working fluid that is at least partially converted into an electrical power;
• converting at least a portion of the electrical power to a torque;
• and
• rotating an at least one independently rotatable compressor stator about a central axis of the jet engine at least partially responsive to the converting the at least a portion of the electrical power to the torque.

A hybrid propulsive method, comprising:

• providing a flow of a working fluid through at least a portion of an at least one jet engine, wherein the at least one jet engine includes an at least one compressor section, wherein the at least one compressor section includes at least one compressor stage, and wherein the at least one compressor stage includes an at least one compressor rotor and an at least one independently rotatable compressor stator;
• extracting energy at least partially in the form of electrical power from the working fluid;
• converting at least a portion of the electrical power to torque;
• and
• rotating the at least one independently rotatable compressor stator about a central axis of the jet engine at least partially responsive to the converting the at least a portion of the electrical power to torque.

A hybrid propulsive method, comprising:

• providing a flow of a working fluid through at least a portion of an at least one jet engine;
• extracting electrical energy from a working fluid passing through a portion of a jet engine that is at least partially converted into an electrical power;
• and
• rotating at least one independently rotatable compressor stator about a central of the jet engine at least partially responsive to the extracted electrical energy.