Mixed fuel vacuum burner-reactor

A triple-vortex burner-reactor comprising:

• an intake manifold, including a vacuum chamber, a compressed air nozzle inlet into the vacuum chamber, a compressed air nozzle for injecting compressed air into the vacuum chamber through the compressed air nozzle inlet, and an ejector outlet, wherein the intake manifold is configured to supply a gaseous fuel to a primary combustion chamber;
• a primary combustion chamber having a cylindrical exterior and having a conical interior, the conical interior having a first end with a smaller diameter and a second end with a larger diameter, the first end of the conical interior being connected to the intake manifold, the conical interior further including a first set of directing blades;
• a reduction nozzle connected to the second end of the conical interior of the primary combustion chamber, the reduction nozzle having a frustoconical first portion with a larger diameter connected to the primary combustion chamber and having a cylindrical second portion that extends from a smaller diameter of the frustoconical first portion;
• injectors perpendicular to the frustoconical first portion of the reduction nozzle configured to inject liquid fuel into the primary combustion chamber;
• and
• a cylindrical secondary combustion chamber having a second set of directing blades configured to direct air into the secondary combustion chamber,
• wherein the primary combustion chamber is configured to operate under vacuum to form three vortices of fuel in order to sustain rotation of the fuel to the exterior of the burner-reactor and configured to slow transit of the fuels to allow for complete combustion.

A method of efficiently burning mixed fuels in a triple-vortex vacuum burner-reactor, the method comprising:

• creating vacuum conditions in a conical primary combustion chamber by ejecting air through an intake manifold connected to the conical primary combustion chamber;
• introducing fuels into the conical primary combustion chamber through the intake manifold, such that two vortices of a first set of fuels and outlet gases are formed due to pressure differences caused by the vacuum conditions;
• passing the first set of fuels over a first set of directing blades in the conical primary combustion chamber to form a third vortex, the three vortices sustaining rotation through the conical combustion chamber and a secondary combustion chamber to the exterior of the burner-reactor;
• and
• injecting a second set of fuels into the conical primary combustion chamber in a direction opposite to a direction of rotation of the first set of fuels.