Liquid fuel supply system for an atomization burner nozzle

Combustion – Combustion bursts or flare-ups in pulses or serial pattern

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239101, 417440, 418 15, 418183, F23C 1100, F04C 2908

Patent

active

043915809

ABSTRACT:
A system for supplying fuel to an atomization fuel oil burner nozzle from a fuel pump at a rate less than that rated for the nozzle for burning of less fuel while achieving good combustion. The fuel is delivered to the nozzle at a pulsing frequency which is dynamically matched to intermittent pressure pulses within the fuel pump to create resonant pressure peaks at the nozzle. The fuel pump creates a pressure pulse each time a tooth of one gear of the pump makes full penetration into the space between a pair of teeth of a coacting rotatable ring gear. Rotatable valving structure, including gear ports in the rotatable ring gear pulses fluid flow to the nozzle by alternately connecting a fluid outlet of the pump to either a pressure port within the pump at the time of a pressure pulse or to the fuel pump inlet with the pressure peak of the pulsed flow being phased together with said pressure pulse.

REFERENCES:
patent: 2464698 (1949-03-01), Logan
patent: 4255093 (1981-03-01), Erikson

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