Device for Producing a Gaseous Fuel Composite and System of Production Thereof

A vortex generator for producing a gaseous fuel composite, comprising an axial channel opening, a flange defining a ring channel, and a plurality of apertures in the ring channel, each with an associated tangential channel, for the creation of a passageway from the ring channel through the apertures and the associated tangential channel into the axial channel opening, and wherein at least a connection between one of the apertures and the associated tangential channel includes a first curved aerodynamic channel amplifier having a first curvature.

A system for the production of a gaseous fuel composite, comprising the process of transforming a gas fuel into a gaseous fuel composite by successive steps of:

• connecting a device for the production of a gaseous fuel composite to an inlet connected a source of gas fuel having a plurality of vortex generators each with an axial channel, the generators being in a stacked configuration in relation to the other vortex generators in a housing between the inlet and an outlet, wherein each of the vortex generators including a flange defining a ring channel and a plurality of apertures and associated tangential channels, wherein at least a connection between one of the apertures and the associated tangential channel includes a first curved aerodynamic channel amplifier having a first curvature, and
• aerating the gas fuel with a stream of air traveling from the ring channel via at least one of the plurality of apertures and associated tangential channel into the axial channel for mixture of a first quantity of air with the gas fuel using one of the plurality of vortex generators, and wherein the stream of air includes an upward motion created by the first curvature and a circular motion to form a gaseous fuel composite.

A gaseous fuel composite made of a first gas fuel traveling linearly and aerated by a series of at least two streams at different staggered distances along a linear axial chamber, where each stream includes kinetic energy in the form of a circular motion and kinetic energy in the form of an upward motion, and where the stream is further compressed and accelerated in the axial chamber by a conical reduction of the axial chamber and a nozzle release.