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US2494991A - Perforated combustion tube oil burner having atmospheric air draft inducing means - Google Patents

Perforated combustion tube oil burner having atmospheric air draft inducing means Download PDF

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Publication number
US2494991A
US2494991A US718822A US71882246A US2494991A US 2494991 A US2494991 A US 2494991A US 718822 A US718822 A US 718822A US 71882246 A US71882246 A US 71882246A US 2494991 A US2494991 A US 2494991A
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Prior art keywords
oil burner
atmospheric air
air draft
combustion tube
inducing means
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US718822A
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Francois U Dumas
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D5/00Burners in which liquid fuel evaporates in the combustion space, with or without chemical conversion of evaporated fuel

Definitions

  • This invention relates to improvements in oil burners and the principal object of the invention is to provide a novel oil burner having new and improved means for inducing a draft of atmospheric air upwardly into the region of the flame for improved economy in burning fuel.
  • FIG. 1 is a vertical section through an oil burner according to the invention.
  • Fig. 2 is a section on line 2-2 of Fig. 1.
  • the reference l indicates an oil feed line from a reservoir, this feed line being in the form of a pipe and being secured to a cup-shaped reservoir
  • 2 is generally circular and extends upwardly as at I4 and flares outwardly as at IS in circular form.
  • the element l2, l4, I6 is provided with an upstanding circular flange
  • the ring-like portion 20 is provided with a series of apertures 24 arranged in circular form, see Fig. 2.
  • the downturned flange 22 has secured thereto a depending imperforate skirt 26 which is circular and provides a shield completely around the device, this shield, however, being open at the bottom.
  • Flange 22 is also recessed to receive and support in upright condition a perforated cylinder 28 which is also circular and supports a top cover plate or the like 30 as clearly shown in Fig. 1.
  • the top cover or plate 30 is provided with a central opening 32 and surrounding the opening underneath plate 3
  • Plate 36 is connected to three spaced perforated cylinders 40, 4
  • the interior circular plate generally indicated at 44 is supported on elements I4 and I6, by leg brackets 46, in spaced relation thereto and forming an oil fuel passage therebetween.
  • Plate 44 is provided with a circular peripheral upstanding flange 46 which curves upwardly and outwardly terminating in a shoulder as shown at 48, supporting cylinders 40 and 4
  • This part of element 44 is provided with a circular series of holes 5
  • a circular wick may be provided in a channel formed between members I8 and 46, as clearly shown in Fig. 1.
  • An oil burner comprising a base element of circular form having a series of holes adjacent the periphery thereof, said base element being of depressed cup-shape form, centrally thereof to form a fuel reservoir, an oil feed pipe to the reservoir, a perforated cylinder mounted on the base element at the periphery thereof, said cylinder surrounding the holes, a plate mounted in spaced relation above the base element and forming therewith a fuel passage radially from the reservoir to the edge of the plate, an annular flange about the periphery of the plate extending upwardly and outwardly and located radially inwardly of and adjacent to the said holes, said annular flange having a series of holes located about the periphery thereof, means forming a shoulder on the flange outwardly of the series of holes therein, a second perforated cylinder supported on the shoulder and positioned thereby coaxially with respect to the first cylinder, the

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Evaporation-Type Combustion Burners (AREA)

Description

Jan. 17, 1950 F. u. DUMAS 2,494,991
PERFORATED COMBUSTION TUBE OIL BURNER HAVING ATMOSPHERIC AIR DRAFT INDUCING MEANS Filed Dec. 2'7, 1946 A irzumfar: .Efzflcas .Dzzrrzas Patented Jan. 17,1950
PERFORATED COMBUSTION TUBE OIL BURNER HAVING ATMOSPHERIC AIR DRAFT INDUCING MEANS Francois U. Dumas, Spencer, Mass.
Application December 27, 1946, Serial No. 718,822
1 Claim. 1
This invention relates to improvements in oil burners and the principal object of the invention is to provide a novel oil burner having new and improved means for inducing a draft of atmospheric air upwardly into the region of the flame for improved economy in burning fuel.
Other objects and advantages of the invention will appear hereinafter.
Reference is to be had to the accompanying drawings in which Fig. 1 is a vertical section through an oil burner according to the invention; and
Fig. 2 is a section on line 2-2 of Fig. 1.
As shown in the drawings the reference l indicates an oil feed line from a reservoir, this feed line being in the form of a pipe and being secured to a cup-shaped reservoir |2 which it is in communication with. The cup-shaped element |2 is generally circular and extends upwardly as at I4 and flares outwardly as at IS in circular form. The element l2, l4, I6 is provided with an upstanding circular flange |8, the latter extending into a flat horizontal ring-like portion 2|] terminating in a downturned flange 22. The ring-like portion 20 is provided with a series of apertures 24 arranged in circular form, see Fig. 2.
The downturned flange 22 has secured thereto a depending imperforate skirt 26 which is circular and provides a shield completely around the device, this shield, however, being open at the bottom. Flange 22 is also recessed to receive and support in upright condition a perforated cylinder 28 which is also circular and supports a top cover plate or the like 30 as clearly shown in Fig. 1. The top cover or plate 30 is provided with a central opening 32 and surrounding the opening underneath plate 3|] there is located a support 34 carrying a circular plate-like element 36 which also is centrally apertured as at 38.
Plate 36 is connected to three spaced perforated cylinders 40, 4|, and 42, cylinders 40 and 4| being shorter than the cylinder 42 and terminating in ends supported on an element 44 in the form of a circular plate. It is to be noted that all four of the perforated cylinders are concentrically positioned in spaced relation.
The interior circular plate generally indicated at 44 is supported on elements I4 and I6, by leg brackets 46, in spaced relation thereto and forming an oil fuel passage therebetween. Plate 44 is provided with a circular peripheral upstanding flange 46 which curves upwardly and outwardly terminating in a shoulder as shown at 48, supporting cylinders 40 and 4| in spaced relation.
This part of element 44 is provided with a circular series of holes 5|] located interiorly of cylinders 40 and 4|. It is to be noted that the cylinder 42 fits snugly within the upstanding flange 46'.
As the oil in the reservoir member i2 is heated, it will gasify and rise along the passage between members Hi and 44 and continuing upwardly between members I8 and 46 to emerge into the area just under holes 50 where the flame will start. However, it is to be noted that this gas may rise through apertures 50 and between the cylinders 28 and 49. As the gas is thus dispersed, air will be induced from the imperforate skirt 26 through holes 24 and into the same regions described above so that combustion of the gas will be substantially complete and extremely economical and the burner will be maintained in good operating condition with a minimum of cleaning. If desired, a circular wick may be provided in a channel formed between members I8 and 46, as clearly shown in Fig. 1.
Having thus described my invention and the advantages thereof, I do not wish to be limited to the details herein disclosed, otherwise than is set forth in the claim, but what I claim is:
An oil burner comprising a base element of circular form having a series of holes adjacent the periphery thereof, said base element being of depressed cup-shape form, centrally thereof to form a fuel reservoir, an oil feed pipe to the reservoir, a perforated cylinder mounted on the base element at the periphery thereof, said cylinder surrounding the holes, a plate mounted in spaced relation above the base element and forming therewith a fuel passage radially from the reservoir to the edge of the plate, an annular flange about the periphery of the plate extending upwardly and outwardly and located radially inwardly of and adjacent to the said holes, said annular flange having a series of holes located about the periphery thereof, means forming a shoulder on the flange outwardly of the series of holes therein, a second perforated cylinder supported on the shoulder and positioned thereby coaxially with respect to the first cylinder, the
second cylinder having a lesser diameter than the first cylinder so that the two cylinders are spaced, one being within the other, an imperforate skirt depending from the base element at the periphery thereof to create a draft through the holes and between the cylinders when the fuel is under combustion at the edges of the plate, and a third perforated cylinder resting on the plate and located against the flange, the second and third cylinders being spaced and the holes in the flange being located between the second and third cyl- Number inders. 1,660,970 FRANCOIS U. DUMAS. 1,886,667 1,928,201 REFERENCES CITED 5 2 0223 The following references are of record in the 29064381 file of this patent: 2,416,383
UNITED STATES PATENTS Number Name Date 1 Number 625,124 Ruppel May 16, 1899 787,527
Name Date La. Pointe Feb. 28, 1928 Fowler Nov. 8, 1932 Field Sept. 26, 1933 Sherman et a1 Dec. 3, 1935 Quart Dec. 15, 1936 Dumas Feb. 25, 1947 FOREIGN PATENTS Country Date France July 8, 1935
US718822A 1946-12-27 1946-12-27 Perforated combustion tube oil burner having atmospheric air draft inducing means Expired - Lifetime US2494991A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US718822A US2494991A (en) 1946-12-27 1946-12-27 Perforated combustion tube oil burner having atmospheric air draft inducing means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US718822A US2494991A (en) 1946-12-27 1946-12-27 Perforated combustion tube oil burner having atmospheric air draft inducing means

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US625124A (en) * 1899-05-16 E horfhj peters co
US1660970A (en) * 1926-07-27 1928-02-28 Francis J Lapointe Oil burner
US1886667A (en) * 1931-09-01 1932-11-08 Joseph E Fowler Oil burner
US1928201A (en) * 1931-12-07 1933-09-26 Field Bernard Fuel oil burner
FR787527A (en) * 1935-03-19 1935-09-24 Heavy oil burner
US2022871A (en) * 1930-08-04 1935-12-03 Silent Glow Oil Burner Corp Burner
US2064081A (en) * 1932-07-05 1936-12-15 Thure A Quart Oil burner
US2416383A (en) * 1944-03-04 1947-02-25 Dumas Francois Uldege Oil burner

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US625124A (en) * 1899-05-16 E horfhj peters co
US1660970A (en) * 1926-07-27 1928-02-28 Francis J Lapointe Oil burner
US2022871A (en) * 1930-08-04 1935-12-03 Silent Glow Oil Burner Corp Burner
US1886667A (en) * 1931-09-01 1932-11-08 Joseph E Fowler Oil burner
US1928201A (en) * 1931-12-07 1933-09-26 Field Bernard Fuel oil burner
US2064081A (en) * 1932-07-05 1936-12-15 Thure A Quart Oil burner
FR787527A (en) * 1935-03-19 1935-09-24 Heavy oil burner
US2416383A (en) * 1944-03-04 1947-02-25 Dumas Francois Uldege Oil burner

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