Power gas burner system

Combustion – Discrete means transmitting flame between separate flame...

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Details

431183, 431354, 126110R, 126110C, F23D 1458

Patent

active

054414059

ABSTRACT:
A gas burner system in which a turbulator disk is arranged between a burner and an opening in a combustion chamber aligned with the burner. The turbulator disk defines a central port and a plurality of peripheral voids adjacent to the central port. A burner flame, produced by ignition of a gas-primary air mixture, together with a quantity of secondary air, may be directed through the central port of the turbulator disk into the combustion chamber. A additional quantity of secondary air may be directed through the voids into the combustion chamber for combustion of the uncombusted gas from the gas-primary air mixture.

REFERENCES:
patent: 3285316 (1966-11-01), Gustafson et al.
patent: 3301308 (1967-01-01), Briggs
patent: 3720496 (1973-03-01), Briggs
patent: 4115050 (1978-09-01), Gerwin
patent: 4473349 (1984-09-01), Kumatsu
patent: 5316470 (1994-05-01), Sigler

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