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The result of the idea it is obtain a new thermodynamic cycle of an engine with a different mechanical technique, based on the integration of piston and blades movements derived from Otto and jet cycles; providing in a third technology based on the vortex flowing.

The position of “airfoil lift force improvement section” is not necessarily along the wing, and so allocated on relevant coordinates that adds value in order to increase the upward capability of wing, considering yet more than one mechanism could be applying. Otherwise, regarding this mechanism as such auxiliary equipment the same could be deactivating due to a manual or automatic control already settable (i.e. high velocity of airplane becoming unnecessary the use of this mechanism).

The other mechanism named “airfoil trailing edge drag force reduction component” is able to decrease the drag force effects (named “downwash”, also) over airfoil performance, regarding a better airflow escaping due to trailing edge adjacent preventing the turbulence flowing-off related to drag vortex formation. This vortex causing a reduction on aerodynamic performance of airfoil related to low airflow relative velocity after trailing edge of wing

The proposal refers to a new technique that the transmission of an axle powered occurs by a connection bar between two pulleys that are able to change the position of joining of this bar along a length related to the pulleys radius. Thus, considering that the diameters of transmission could be changed from to each pulley, also a torque ratio has established.

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