US2659427A - Oil burner nozzle head element - Google Patents

Oil burner nozzle head element Download PDF

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Publication number
US2659427A
US2659427A US197978A US19797850A US2659427A US 2659427 A US2659427 A US 2659427A US 197978 A US197978 A US 197978A US 19797850 A US19797850 A US 19797850A US 2659427 A US2659427 A US 2659427A
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Prior art keywords
head element
oil burner
burner nozzle
oil
nozzle head
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Expired - Lifetime
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US197978A
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Isaiah M Bither
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/40Mixing tubes or chambers; Burner heads
    • F23D11/408Flow influencing devices in the air tube

Definitions

  • the present invention relates to oil burner installations, and has particular reference to a novel head element for an oil burner nozzle.
  • the principal object of the invention is to pro vide a head element for an oil burner nozzle which increases the efficiency of combustion.
  • Another object of the invention is to provide an oil burner nozzle head element which produces a thorough combustion mixture of air and atomized oil.
  • a further object of the invention is to divide the burner air supply into a primary and a secondary air stream for progressively atomizing and mixing with the oil from the burner nozzle.
  • An additional object of the invention is to impart a whirling rotation to a primary and a secondary air stream, whereby the streams impact the oil spray and produce a uniform dispersion of the oil in the combustion air.
  • Fig, 1 is a, perspective view of an oil burner, partly broken away;
  • Fig. 2 is a front elevation of the novel oil burner nozzle head element
  • Fig. 3 is a rear view of Fig. 2;
  • Fig. 4 is a transverse section on the line 44 of Fig. 2.
  • an oil burner nozzle with a head element which is interposed in the path of the combustion air and which divides the combustion air into two whirling conical streams, one whirling air stream being compressed to build up a static pressure differential and to impact into the oil stream to disperse and vaporize the oil and to provide a primary mixture, and the other whirling air stream flowing across the primary mixture to further disperse and atomize the oil and thus produce a resulting uniform air-oil combustible mixture.
  • the resulting combustion is hotter, and has a higher CO2 content, whereby less oil is required for a given heating demand and a lower stock temperature and greater heating efflciency results.
  • the nozzle pipe 0 is centrally mounted in the draft tube II which receives air from the usual blower housmg, not shown.
  • the electrode assembly I2 is mounted in an insulating support [3, the elec-
  • the draft tube has a turbulator [1 novel construction is mounted on the nozzle pipe Hl adjacent the nozzle tip. as illustrated.
  • the head element I8 includes an outer annular shell 19 of tapered shape, which has a central support ring 20 secured thereto, as by legs 2!, 22 which are positioned adjacent the lower portion of the shell, and have set screw bosses 23, M for receiving set screws for locking the head element support ring to the nozzle pipe, the lower positioning of the legs 2
  • the inner surface 25 of the shell I9 has a number of spiral air flow guide vanes 26 which taper down in contact overlapping block relation as illustrated tional embodiment of my invention, it is obvious that changes in the size, shape and arrangement of the parts may be made to accord with different oil burner nozzle shapes and requirements. without departing from the spirit and the scope of the invention as defined in the appended claim.
  • a head element for an oil burner nozzle comprising an outer annular tapered shell, a central support ring, and legs extended from said rin and secured to said shell, the inner surface of the shell having converging spiral air flow guide vanes in contact overlapping block relation. the outer surface of said shell having converging spiral flow guide vanes separated by arcuate troughs.

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

Description

Nov. 17, 1953 l M. BITHER OIL BURNER NOZZLE HEAD ELEMENT Filed Nov. 28, 1950 IN VEN TOR.
By Mmm ATTURNEY Patented Nov. 17, 1953 UNITED STATES PATENT OFFICE 2,659,427 OIL BURNER NOZZLE HEAD ELEMENT Isaiah M. Bither, Providence, R. I. Application November 28, 1950, Serial N 0. 197,978
1 Claim.
The present invention relates to oil burner installations, and has particular reference to a novel head element for an oil burner nozzle.
The principal object of the invention is to pro vide a head element for an oil burner nozzle which increases the efficiency of combustion.
Another object of the invention is to provide an oil burner nozzle head element which produces a thorough combustion mixture of air and atomized oil.
A further object of the invention is to divide the burner air supply into a primary and a secondary air stream for progressively atomizing and mixing with the oil from the burner nozzle.
An additional object of the invention is to impart a whirling rotation to a primary and a secondary air stream, whereby the streams impact the oil spray and produce a uniform dispersion of the oil in the combustion air.
With the above and other objects and advantageous features in view, the invention consists of a novel arrangement of parts more fully disclosed in the detailed description following, in conjunction with the accompanying drawings, and more specifically defined in the claim appended thereto.
In the drawings,
Fig, 1 is a, perspective view of an oil burner, partly broken away;
Fig. 2 is a front elevation of the novel oil burner nozzle head element;
Fig. 3 is a rear view of Fig. 2; and
Fig. 4 is a transverse section on the line 44 of Fig. 2.
It has been found desirable to provide an oil burner nozzle with a head element which is interposed in the path of the combustion air and which divides the combustion air into two whirling conical streams, one whirling air stream being compressed to build up a static pressure differential and to impact into the oil stream to disperse and vaporize the oil and to provide a primary mixture, and the other whirling air stream flowing across the primary mixture to further disperse and atomize the oil and thus produce a resulting uniform air-oil combustible mixture. The resulting combustion is hotter, and has a higher CO2 content, whereby less oil is required for a given heating demand and a lower stock temperature and greater heating efflciency results.
Referring to the drawings, which illustrate the novel head element as applied to a conventional nozzle with turbulator, the nozzle pipe 0 is centrally mounted in the draft tube II which receives air from the usual blower housmg, not shown. The electrode assembly I2 is mounted in an insulating support [3, the elec- |5 being positioned adjacent the noz- The draft tube has a turbulator [1 novel construction is mounted on the nozzle pipe Hl adjacent the nozzle tip. as illustrated.
The head element I8 includes an outer annular shell 19 of tapered shape, which has a central support ring 20 secured thereto, as by legs 2!, 22 which are positioned adjacent the lower portion of the shell, and have set screw bosses 23, M for receiving set screws for locking the head element support ring to the nozzle pipe, the lower positioning of the legs 2|, 22 providing an ample open annular space greater than a half-circle for the electrodes l4, I5. The inner surface 25 of the shell I9 has a number of spiral air flow guide vanes 26 which taper down in contact overlapping block relation as illustrated tional embodiment of my invention, it is obvious that changes in the size, shape and arrangement of the parts may be made to accord with different oil burner nozzle shapes and requirements. without departing from the spirit and the scope of the invention as defined in the appended claim.
I claim:
A head element for an oil burner nozzle, comprising an outer annular tapered shell, a central support ring, and legs extended from said rin and secured to said shell, the inner surface of the shell having converging spiral air flow guide vanes in contact overlapping block relation. the outer surface of said shell having converging spiral flow guide vanes separated by arcuate troughs.
I. MORRIS EITHER.
4 References Cited in the file of this patent UNITED STATES PATENTS Number Name Date Bierstadt Aug. 25, 1896 Reid Aug. 1'7, 1920 Berryman Dec. 22, 1936 Smith Jan. 5, 1937 Carroll Jan. 12, 1943 Cadella Feb. '1, 1950 Goddard Oct. 1'7, 1950 Smith Nov. 28, 1950 Cadella May 15, 1951
US197978A 1950-11-28 1950-11-28 Oil burner nozzle head element Expired - Lifetime US2659427A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982348A (en) * 1957-05-15 1961-05-02 Antonios G Samothrakis Oil burner for cooking range
DE1169070B (en) * 1961-10-05 1964-04-30 Wagner Hochdruck Dampfturbinen Oil burner with pressure atomizer
US20070125883A1 (en) * 2005-12-01 2007-06-07 Cotler Elliot M Lubricator nozzle and emitter element
CZ306669B6 (en) * 2016-04-28 2017-04-26 Vysoké Učení Technické V Brně An oil burner for incineration of hardly combustible substances
EP3242083A1 (en) 2016-05-06 2017-11-08 Vysoké Ucení Technické V Brne Oil burner for combustion of uneasy combustible stuff

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US566292A (en) * 1896-08-25 Screw-propeller
US1350037A (en) * 1919-04-19 1920-08-17 Reid John Furnace-front
US2065042A (en) * 1935-04-29 1936-12-22 Harry H Berryman Air control for oil burners
US2066806A (en) * 1935-12-02 1937-01-05 Gilbert & Barker Mfg Co Oil burner
US2308439A (en) * 1940-10-31 1943-01-12 Monarch Mfg Works Inc Means for stabilizing air
US2496775A (en) * 1946-06-20 1950-02-07 Cadella Anthony Gun type oil burner
US2526220A (en) * 1947-07-18 1950-10-17 Daniel And Florence Guggenheim Spray nozzle
US2531538A (en) * 1948-05-06 1950-11-28 Cecil W Smith Air control unit for oil burners
US2553130A (en) * 1946-06-20 1951-05-15 Cadella Anthony Air directing means for gun type oil burners

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US566292A (en) * 1896-08-25 Screw-propeller
US1350037A (en) * 1919-04-19 1920-08-17 Reid John Furnace-front
US2065042A (en) * 1935-04-29 1936-12-22 Harry H Berryman Air control for oil burners
US2066806A (en) * 1935-12-02 1937-01-05 Gilbert & Barker Mfg Co Oil burner
US2308439A (en) * 1940-10-31 1943-01-12 Monarch Mfg Works Inc Means for stabilizing air
US2496775A (en) * 1946-06-20 1950-02-07 Cadella Anthony Gun type oil burner
US2553130A (en) * 1946-06-20 1951-05-15 Cadella Anthony Air directing means for gun type oil burners
US2526220A (en) * 1947-07-18 1950-10-17 Daniel And Florence Guggenheim Spray nozzle
US2531538A (en) * 1948-05-06 1950-11-28 Cecil W Smith Air control unit for oil burners

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982348A (en) * 1957-05-15 1961-05-02 Antonios G Samothrakis Oil burner for cooking range
DE1169070B (en) * 1961-10-05 1964-04-30 Wagner Hochdruck Dampfturbinen Oil burner with pressure atomizer
US20070125883A1 (en) * 2005-12-01 2007-06-07 Cotler Elliot M Lubricator nozzle and emitter element
US8074901B2 (en) * 2005-12-01 2011-12-13 Uniwave, Inc. Lubricator nozzle and emitter element
CZ306669B6 (en) * 2016-04-28 2017-04-26 Vysoké Učení Technické V Brně An oil burner for incineration of hardly combustible substances
EP3242083A1 (en) 2016-05-06 2017-11-08 Vysoké Ucení Technické V Brne Oil burner for combustion of uneasy combustible stuff

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