Importance

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Abstract

A hybrid jet engine, including a front cowling having a tubular shape, a rear cowling having a tubular shape and connected to the front cowling, such that the rear cowling is smaller than the front cowling, a central core disposed within the front cowling and the rear cowling, a shaft disposed longitudinally within the central core, a plurality of main fan blades disposed at a first end of the shaft at the front cowling, a plurality of auxiliary fan blades disposed at a second end of the shaft at the rear cowling, at least one aerodynamic stabilizer disposed on a surface of the central core to extend therefrom, to provide connected between the central core and the front cowling, and at least one modified Tesla one way valve disposed on the surface of the central core to receive the ram air and to provide the ram air to the plurality of auxiliary fan blades, such that the air is recycled through the shaft of the central core to power the plurality of main fan blades.

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First Claim