Patent US4194874A successfully refreshed from Google Patents.
US4194874A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Variable flame shape oil burner
Assignee: John Zink Co LLC
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Filing: 1978-01-03
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Granted: 1980-03-25
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Expires: 1998-01-03
Abstract
Abstract An oil fired burner adapted to produce a variable asymmetrical flame shape. The burner includes a tip head carrying a plurality of tips disposed in at least two orientations, i.e., axial and off-axis. The relative rates of fuel supply to the tips is controlled to afford asymmetric flame shaping. In a typical application in a rotary cement kiln, the flame is biased to increase the heat transferred to the load in the front end of the kiln and to decrease the heat transferred to the top and sides of the kiln.
Inventors
- 👤 Temple S. Voorheis
- 👤 Louis D. Siegert
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 18:19
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/36; F23D11/38
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
280 words
A liquid fuel fired burner assembly for producing a single variable shaped asymmetric flame, said assembly comprising: a tip head for receiving and carrying tip means in relatively fixed, spaced-apart relation, said tip head including means defining a hollow core for receiving a first fuel supply and means defining a hollow annulus about said hollow core for receiving a second fuel supply; a first fuel supply means for controllably supplying liquid fuel to a first tip means through said core; a second fuel supply means for controllably supplying liquid fuel to a second tip means through said annulus; first liquid fuel spray tip means mounted to said tip head and disposed parallel to a central axis of said burner assembly for forming a first dispersed liquid fuel spray cone having its axis parallel to said central axis of said burner; second liquid fuel spray tip means mountable to said tip head for forming a second dispersed liquid fuel spray cone, said second tip means being disposed divergent of said central axis on one side of a plane through said axis, and wherein the spray cone angle of said second tip means is substantially wider than the spray cone angle of said first tip means such that said second spray cone substantially intersects said first spray cone to form a single composite liquid fuel spray cone of asymmetric cross-section relative to said plane; and means for controlling the relative rates at which said first fuel supply means and said second fuel supply means provide liquid fuel to said core and to said annulus, respectively, such that the asymmetric shape of said single composite liquid fuel spray cone may be continuously varied.
Claim 2
Dependent Claim
280 words
A liquid fuel fired burner assembly for producing a single variable shaped asymmetric flame, said assembly comprising: a tip head for receiving and carrying tip means in relatively fixed, spaced-apart relation, said tip head including means defining a hollow core for receiving a first fuel supply and means defining a hollow annulus about said hollow core for receiving a second fuel supply; a first fuel supply means for controllably supplying liquid fuel to a first tip means through said core; a second fuel supply means for controllably supplying liquid fuel to a second tip means through said annulus; first liquid fuel spray tip means mounted to said tip head and disposed parallel to a central axis of said burner assembly for forming a first dispersed liquid fuel spray cone having its axis parallel to said central axis of said burner; second liquid fuel spray tip means mountable to said tip head for forming a second dispersed liquid fuel spray cone, said second tip means being disposed divergent of said central axis on one side of a plane through said axis, and wherein the spray cone angle of said second tip means is substantially wider than the spray cone angle of said first tip means such that said second spray cone substantially intersects said first spray cone to form a single composite liquid fuel spray cone of asymmetric cross-section relative to said plane; and means for controlling the relative rates at which said first fuel supply means and said second fuel supply means provide liquid fuel to said core and to said annulus, respectively, such that the asymmetric shape of said single composite liquid fuel spray cone may be continuously varied.
Claim 3
Dependent Claim
42 words
Apparatus according to claim 1 wherein said second liquid fuel spray tip means define a spray cone angle of at least about 60° and less than about 100° to produce liquid fuel droplets of a minimum size for producing localized head "polishing".
Claim 4
Dependent Claim
52 words
Apparatus according to claim 1 wherein said second tip means is oriented at an angle of between about 40° and 70° to said central axis for supplying a maximum concentration of liquid fuel droplets along a path transverse of the central axis to a lateral target area forward of said tip head.
Claim 5
Dependent Claim
42 words
Apparatus according to claim 1 wherein said tip head is bilaterally symmetric along a plane through said central axis, said tip head further comprising at least two means for receiving said second tip means disposed at spaced locations equidistant from said plane.
Claim 6
Dependent Claim
31 words
Apparatus according to claim 4 wherein said tip head further comprises means for receiving and carrying at least three first tip means disposed at spaced locations equidistant from said central axis.
Claim 7
Dependent Claim
73 words
Apparatus according to claim 1 wherein said first and second fuel supply means comprises a pair of concentric tubular conduits defining a first fuel path interior of the inner of said conduits and a second fuel path in the annular region between said pair of conduits, and a plurality of conduits interior of said tip head communicating from the first and second fuel paths to the first and second fuel tip means respectively.
Claim 8
Independent Claim
209 words
A method for producing a single asymmetric liquid fuel flame from a burner assembly having first and second independently controllable supply means and first and second fixed, divergent fuel injection tip means spaced equidistant from a central axis through said burner assembly, said method comprising the steps of: (a) injecting at least one stream of liquid fuel from said first supply means through said first tip means as a first combustible spray cone along an axis parallel to said central axis; (b) injecting at least another stream of liquid fuel from said second supply means through said second tip means as a second combustible spray cone divergent of said central axis and on one side of a plane through said central axis, the cone angle of said second combustible spray being substantially greater than the cone angle of said first combustible spray such that a substantial portion of said second spray intercepts said first spray cone to form a single composite asymmetric fuel spray cone; and (c) independently controlling the relative rate of fuel supply of said first and second fuel supply means to said first and second tip means, respectively, so that the shape of the composite fuel spray cone can be continuously varied in an asymmetric pattern.
Claim 9
Independent Claim
209 words
A method for producing a single asymmetric liquid fuel flame from a burner assembly having first and second independently controllable supply means and first and second fixed, divergent fuel injection tip means spaced equidistant from a central axis through said burner assembly, said method comprising the steps of: (a) injecting at least one stream of liquid fuel from said first supply means through said first tip means as a first combustible spray cone along an axis parallel to said central axis; (b) injecting at least another stream of liquid fuel from said second supply means through said second tip means as a second combustible spray cone divergent of said central axis and on one side of a plane through said central axis, the cone angle of said second combustible spray being substantially greater than the cone angle of said first combustible spray such that a substantial portion of said second spray intercepts said first spray cone to form a single composite asymmetric fuel spray cone; and (c) independently controlling the relative rate of fuel supply of said first and second fuel supply means to said first and second tip means, respectively, so that the shape of the composite fuel spray cone can be continuously varied in an asymmetric pattern.
Claim 10
Dependent Claim
29 words
The method according to claim 7 wherein said second injecting step comprises injecting at least two off axis streams laterally symmetrical relative to a plane parallel to said axis.
Claim 11
Dependent Claim
63 words
The method according to claim 7 wherein the cone angle of said second sprays is between about 60° and 100° and the transverse angle of said second spray with said central axis is between about 40° and 70° for supplying a maximum concentration of droplets along a path transverse of said central axis to a lateral target area forward of said tip means.
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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) | 1983-03-25 | 1983-09-24 | 1984-03-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-03-25 | 1987-09-24 | 1988-03-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-03-25 | 1991-09-24 | 1992-03-25 | $7700.00 | Window Closed / Lapsed |