Mixed fuel vacuum burner-reactor

摘要

A mixed-fuel vacuum burner-reactor includes a primary combustion chamber having a conical interior and a first set of directing blades. The conical interior is connected to an intake manifold on one end and a reduction nozzle on the other end. Injectors are mounted perpendicularly to the reduction nozzle to inject a second fuel into the primary combustion chamber. The reduction nozzle is connected to a cylindrical secondary combustion chamber having a second set of directing blades configured to direct air into the secondary combustion chamber. Methods of efficiently burning mixed fuels in a triple-vortex vacuum burner-reactor are also disclosed. Vacuum conditions are created and fuels are introduced into a conical primary combustion chamber. The fuels are passed over a first set of directing blades to form three vortices before additional fuels are injected in a direction opposite to a direction of rotation of the first set of fuels.

主权项

1. A mixed-fuel vacuum burner-reactor comprising:
a primary combustion chamber having a conical interior and a first set of directing blades, an intake connected to a first end of the conical interior; a reduction nozzle connected to a second end of the conical interior; said primary combustion chamber being configured to operate under vacuum to create two vortices of a first fuel entering and exiting the primary combustion chamber due to pressure differences, and said first set of directing blades is configured to create a third vortex sustaining rotation of the first fuel to the exterior of the burner-reactor; a first end of said reduction nozzle connected to the conical interior of the primary combustion chamber and a second end of said reduction nozzle connected to a cylindrical secondary combustion chamber; injectors mounted substantially perpendicularly to the reduction nozzle and configured to inject a second fuel into the primary combustion chamber; and said cylindrical secondary combustion chamber comprising a second set of directing blades configured to direct air into the secondary combustion chamber.