US4035137A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Burner unit
Assignee: Forney International Inc
•
Filing: 1975-02-12
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Granted: 1977-07-12
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Expires: 1995-02-12
Abstract
Abstract A burner unit is provided for receiving gaseous and liquid fuels and generating heat therefrom. The burner unit is formed with a plurality of orifices for introducing combustion air into the burner chamber.
Inventors
- 👤 John K. Arand
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 05:14
CPC Classifications
F; F23; F23C; F23C7/00; F23C9/00; F23C9/006
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
268 words
A fuel burner assembly for the combustion of liquid and gaseous fuels comprising an elongated cylindrical wall defining an internal cylindrical burner chamber, an end plate mounted on said cylindrical wall having an inlet opening at one end for introducing fuel into said burner chamber and an exhaust port at the opposite end for exhausting the products of combustion, said cylindrical wall being positioned along a horizontal axis, oil nozzle means at said inlet opening coaxially positioned along said horizontal axis, said end plate formed with a plurality of gas jet openings equally spaced apart in a plane such that said gas jet openings are positioned parallel with respect to said horizontal axis, gas nozzles mounted in each of said jet openings, said cylindrical wall having a plurality of orifices equal in number to said gas jet openings and medially located between said inlet opening and said exhaust port for introducing combustion air into said burner chamber, said orifices positioned in a plane which is substantially perpendicular to said horizontal axis, means for supplying jets of air at each of said orifices such that said combustion air is within a range below and above the theoretical combustion air required for complete combustion of the fuel in said burner chamber, whereby a portion of said jets of air is circulated towards said inlet opening to mix with a portion of said fuel and thereafter flow along said cylindrical wall towards said exhaust port and the remainder of said jets of air is mixed with said fuel and is conveyed towards said exhaust port for combustion as it is discharged.
Claim 2
Dependent Claim
268 words
A fuel burner assembly for the combustion of liquid and gaseous fuels comprising an elongated cylindrical wall defining an internal cylindrical burner chamber, an end plate mounted on said cylindrical wall having an inlet opening at one end for introducing fuel into said burner chamber and an exhaust port at the opposite end for exhausting the products of combustion, said cylindrical wall being positioned along a horizontal axis, oil nozzle means at said inlet opening coaxially positioned along said horizontal axis, said end plate formed with a plurality of gas jet openings equally spaced apart in a plane such that said gas jet openings are positioned parallel with respect to said horizontal axis, gas nozzles mounted in each of said jet openings, said cylindrical wall having a plurality of orifices equal in number to said gas jet openings and medially located between said inlet opening and said exhaust port for introducing combustion air into said burner chamber, said orifices positioned in a plane which is substantially perpendicular to said horizontal axis, means for supplying jets of air at each of said orifices such that said combustion air is within a range below and above the theoretical combustion air required for complete combustion of the fuel in said burner chamber, whereby a portion of said jets of air is circulated towards said inlet opening to mix with a portion of said fuel and thereafter flow along said cylindrical wall towards said exhaust port and the remainder of said jets of air is mixed with said fuel and is conveyed towards said exhaust port for combustion as it is discharged.
Claim 3
Dependent Claim
42 words
A fuel burner assembly according to claim 1 in which said oil nozzle means is capable of producing an oil spray angle in the range of from 16 to 30 degrees of the total included angle radially subtended from said horizontal axis.
Claim 4
Dependent Claim
70 words
A fuel burner assembly according to claim 1, in which said means for supplying jets of air forms a central flow pattern of combustion air which diverges into a rearward flow pattern and a forward flow pattern, such that the fuel sprayed from said oil nozzle mixes with said combustion air to form stable combustion zones in which said fuel is burned, whereby low levels of nitric oxides are produced.
Claim 5
Dependent Claim
50 words
A fuel burner assembly according to claim 1, in which the end of said burner chamber with said inlet opening is formed with a plurality of through bores for introducing streams of primary air along the internal surface of said cylindrical wall, whereby the formation of coke deposits is prevented.
Claim 6
Dependent Claim
25 words
A fuel burner assembly according to claim 1 in which said gas nozzles are equally spaced apart and coaxially positioned around said oil nozzle means.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-07-11 | 1981-01-10 | 1981-07-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-07-11 | 1985-01-10 | 1985-07-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-07-11 | 1989-01-10 | 1989-07-12 | $7700.00 | Window Closed / Lapsed |