Burner assembly

Combustion – With means attenuating sound or pulsation

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Details

181229, 431265, F23D 1312, F23D 1300

Patent

active

041689488

ABSTRACT:
In a burner assembly connected with a combustion chamber at a fuel inlet of said combustion chamber, the improvement of which comprising a fuel duct which is connected at its one end to said fuel inlet and contains therein a fuel injection nozzle, ignition rod and air-fuel mixture diffuser, a blower means which has an outlet for blowing an air through said outlet of the blower means and said fuel duct into said combustion chamber, and a conduit member coupled to said inlet of the blower means, whereby pneumatic oscillation plane progressive waves are converted into plane stationary waves to thereby reduce progressive energy of said pneumatic oscillation plane progressive waves.

REFERENCES:
patent: 2046193 (1936-06-01), Spicer
patent: 2150782 (1939-03-01), Vollmer
patent: 2670034 (1954-02-01), Thompson
patent: 2942683 (1960-06-01), Moyer
patent: 2955671 (1960-10-01), Leistritz
patent: 3712416 (1973-01-01), Swanson
patent: 3940234 (1976-02-01), Reed

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