Superconducting ultra power efficient radial fan augmented nano-aerodrive (superfan)

A gas turbine engine comprising:

• an outer casing;
• a central longitudinal hollow shaft with a forward air inlet;
• a three stage rotating superconducting electric bypass fan with front and rear fan blades and a diffuser blade interposed between said front and rear fan blades wherein the diffuser blade rotates in an opposite direction to the front and rear fan blades;
• a variable speed multiple stage superconducting axial compressor positioned aft of the three stage rotating superconducting electric bypass fan;
• and
• a multiple stage superconducting electric turbine core positioned aft of the multiple stage variable speed superconducting axial compressor,
• wherein the front fan blade, the diffuser fan blade, and the rear fan blade are incorporated respectively into a first blisk, a second blisk, and a third blisk each positioned radially outwardly from the longitudinal hollow shaft and said blisks respectively have first, second, and third integral superconducting rotor electromagnetic coils.

A gas turbine engine comprising:

• an outer casing;
• a central longitudinal hollow shaft with a forward air inlet;
• a three stage rotating superconducting electric bypass fan with front and rear fan blades and a diffuser blade interposed between said front and rear fan blades wherein the diffuser blade rotates in an opposite direction to the front and rear fan blades;
• a variable speed multiple stage superconducting axial compressor positioned aft of the three stage rotating superconducting electric bypass fan;
• a multiple stage superconducting electric turbine core positioned aft of the multiple stage variable speed superconducting axial compressor,
• wherein the front fan blade, the diffuser fan blade, and the rear fan blade are incorporated respectively into a first blisk, a second blisk, and a third blisk each positioned radially outwardly from the longitudinal hollow shaft and said blisks respectively have first, second, and third integral superconducting rotor electromagnetic coils, and the first, second, and third cryogenic copper field stator coils are fixed to the outer casing in proximate opposed relation respectively to the first, second, and third integral superconducting rotor electromagnetic coils, and an exhaust flow is established by the combustor impinging on the three stage turbine rotor blades generating electricity in the superconducting electric core and rotates the superconducting electric bypass fan adding kinetic energy to the mass air flow as bypass air and is driven by an electrical current in the fixed first, second, and third stator coils.