US3003548A - Liquid fuel burner - Google Patents

Liquid fuel burner Download PDF

Info

Publication number
US3003548A
US3003548A US682448A US68244857A US3003548A US 3003548 A US3003548 A US 3003548A US 682448 A US682448 A US 682448A US 68244857 A US68244857 A US 68244857A US 3003548 A US3003548 A US 3003548A
Authority
US
United States
Prior art keywords
insert member
end portion
air
cone
blast tube
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US682448A
Inventor
Guy J Sanders
Edward G Grimsal
William E Lawrie
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Crane Co
Original Assignee
Crane Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Crane Co filed Critical Crane Co
Priority to US682448A priority Critical patent/US3003548A/en
Application granted granted Critical
Publication of US3003548A publication Critical patent/US3003548A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F23D11/001Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space spraying nozzle combined with forced draft fan in one unit
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/0075Nozzle arrangements in gas streams

Definitions

  • This invention relates generally to oil burners, and more particularly it is concerned with a novel mechanism therefor having for its purpose the production of an eflicient and quiet oil burning assembly.
  • noise is an objectionable characteristic of many presently known domestic burner constructions, and here the term noise means the relatively loud reverberations or pulsations resulting from interruptions and fluctuations in the oil combustion process. Such pulsations frequently arise from spasmodic alternations of the fuel air mixture ratio, say, between adequate and inadequate oxygen supply, and there may also be other causes related to flame instability.
  • Another object is to provide a mechanism in which the mixture of fuel and air takes place in such a manner that a minimum of noise would be produced by the turbulence of the mixing process itself.
  • a further object of the invention is to reduce low frequency air turbulence prior to said fuel and air mixing and thereby reducing the amount of noise which would be produced by the combustion.
  • a still further object is to provide a liquid fuel burner construction in which a venturi-shaped burner head assembly is employed and in which a cone structure serves as a guide for the air.
  • Another important object is to provide an oil burner construction or the like in which the air delivered to the burner for combustion takes place in the form of a hollow cone and that the fuel is delivered in a second hollow cone inside the air cone preferably having a slightly greater included angle than the air cone. It has been discovered that such structural arrangement causes the fuel and air to mix gradually and in a relatively laminar manner, thereby producing an eflicient and quiet burning flame.
  • a further object is to provide an oil burner construction in which the mixing of the fuel and air may be conveniently controlled and changed by varying the relative position of the air distributing cone with respect to the outlet side of the venturi.
  • our invention consists in the construction, arrangement and combination of the various parts of my oil burner whereby the objects contemplated are obtained as hereinafter more fully set forth, pointed out in our claims and illustrated in the accompanying drawing, wherein:
  • FIG. 1 is a sectional assembly view of an oil burner assembly embodying our invention.
  • FIG. 2 is an end elevational view, looking in the direction of the nozzle and throat shown in FIG. 1.
  • the numeral 1 is used to designate generally a gun-type oil burner constructed in accordance with the present invention, having a casing 2, to which is attached in any suitable manner the blast tube 3,
  • the casing 2 includes a lower portion thereof 3,003,548 Patented Oct. 10, 1961 for receiving an air blower 4 attached in the well known manner and supplying air thereto as indicated by the arrows.
  • the upper portion of the casing 2. is provided with the air outlet port which is in communication with the outer end of the blast tube as illustrated.
  • the longitudinally extending electrode wires 6 and 8 are mounted in the respective insulated supports 5 and 7.
  • the cylindrical insert member generally designated 10 Suitably carrying the said insulated supports and lining the inner peripheral surface of the blast tube 3 for substantially its entire length is the cylindrical insert member generally designated 10 having an annular recessed or chamber portion 9 for a substantial part of the length of the said insert member.
  • the length of the chamber portion 9 is defined by the space between the respective end disposed protruded portions 18 and 19, the latter portions being of annular configuration and snugly received within the blast tube 3 at outer and inner ends of said tube as indicated.
  • the respective connections are made at 11 and 12 to a source (not shown) of electrical ignition for the said electrode wires.
  • the fixed spider having the radially extending spokes 13 as illustrated and with the central apertured hub portion provided to carry the feed piping to the fuel spray nozzle 15.
  • the location of the latter member is in proximity to the end portion of the blast tube and has the hollow cone 14 extending to the inner end of the blast tube 3.
  • the latter construction is a significant feature of this invention and particularly so when considered with the frusto-conical inner surface 17, the latter surface being substantially of the same length as the hollow cone 14. It will be now appreciated that the air is thus delivered in the form of a hollow cone and that the fuel is delivered in a second hollow cone inside the air cone and preferably having a slightly greater included angle than the air cone.
  • the frustoconical surface 16 is provided.
  • a liquid fuel burner comprising an elongated air blast tube having inner and outer peripheral end portions and with its outer end portion ported to receive inlet air flow, the other end portion thereof being adapted to discharge into a combustion chamber, a hollow sleeve-like insert member of substantially elongated cylindrical configuration cooperating with the inner peripheral surface .of said air blast tube to bear against the inner and the outer peripheral end portions of the tube, the said insert member having at least the inner end portion thereof with an annular surface of outwardly flaring form, the remaining portion of the insert member merging with the outwardly flaring inner end portion of the insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the outwardly flaring inner end portion with the remaining portion of the said insert member, ported means mounted within the hollow insert member cooperating with said fuel nozzle to centrally position the latter memher in spaced relation to the inner wall of the said insert member, a substantially frusto-conical hollow outwardly flaring cone member cooperating with said nozzle
  • a liquid fuel burner comprising anelongated air blast tube with inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the opposite end portion thereof being adapted to discharge into a combustion chamber, a hollow insert member in the tube with an inner wall surface of substantially cylindrical configuration and with the outer peripheral end portions thereof cooperating with the inner and the outer peripheral end portions of the said air blast tube to line the inner peripheral wall surface of the latter member, the said insert member having at least the inner end portion thereof of outwardly flaring form merging with the remaining inner peripheral wall surface of said hollow insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the outwardly flaring inner end portion with the remaining portion of the said insert member, ported means adjacent the outer end portion of the said blast tube cooperatin with said fuel nozzle to position the latter member in spaced relation to the said inner peripheral wall surface of the said insert member, a substantially hollow cone member fitted over an inner end portion of said nozzle, the said cone member being of a length to extend to thein
  • a liquid fuel burner comprising an elongated cylindrical air blast tube having inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the opposite end portion thereof being adapted to project into a combustion chamber, a hollow insert member of substantially cylindrical configuration fitted over the inner peripheral wall surface of said air blast tube, the said insert member having at least the inner end portion thereof outwardly flared to merge with the remaining portion of the insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the out- 'wardly flaring inner end portion with the remaining portion of the said insert member, ported means within said insert member axially spaced from the said outwardly flared portion of said insert member and cooperating with said fuel nozzle to position the latter member in spaced relation to the inner end portion of the said insert member, a frusto-conical hollow cone mounted over said nozzle with its reduced end connected to said nozzle and being in substantially the same transverse plane as the said point of merger of said insert member and having an included angle approximating that
  • a liquid fuel burner comprising an elongated air blast tube having inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the inner end portion thereof being adapted to discharge into a combustion chamber, a hollow insert member of substantially cylindrical configuration cooperating with the inner peripheral wall of said air blast tube, the said insert member having at least the inner end portion thereof of outwardly flaring form with a curved annular surface merging with a wall inner surface defining an elongated substantially cylindrical cham her in said insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation to said outwardly flaring inner end portion of the said insert mem ber, fixed means engaging the insert member and cooperating with said fuel nozzle to position the latter member in spaced relation to the inner wall of the said insert member and being axially removed from the outwardly flaring portion of the insert member, a substantially hollow outwardly flaring cone mounted over an end portion of said nozzle and cooperating with the outwardly flaring portion of the insert member to form a passage around the outer

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Description

Oct. 10, 1961 G. J. SANDERS ET AL 3,003,543
LIQUID FUEL BURNER Filed Sept. 6, 1957 United States Patent M 3,003,548 LIQUID FUEL BURNER Guy J. Sanders, Hinsdale, Edward G. Grimsal, Chicago,
and William E. Lawrie, Park Forest, 11]., assignors, by
mesne assignments, to Crane Company, Chicago, Ill., a
corporation of Illinois Filed Sept. 6, 1957, Ser. No. 682,448 4 Claims. (Cl. 158-76) This invention relates generally to oil burners, and more particularly it is concerned with a novel mechanism therefor having for its purpose the production of an eflicient and quiet oil burning assembly.
At the outset, in order to acquire a better appreciation of the accomplishment of this invention, it should be understood that a major cause of noise in oil burners is the fluctuating and poorly distributed air patterns around and adjacent to the oil burner nozzle resulting in an oscillating or unstable flame. Noise is an objectionable characteristic of many presently known domestic burner constructions, and here the term noise means the relatively loud reverberations or pulsations resulting from interruptions and fluctuations in the oil combustion process. Such pulsations frequently arise from spasmodic alternations of the fuel air mixture ratio, say, between adequate and inadequate oxygen supply, and there may also be other causes related to flame instability.
Therefore, it is one of the more important objects of this invention to provide greater stability in the burner flame and more eflicient and quiet combustion.
Another object is to provide a mechanism in which the mixture of fuel and air takes place in such a manner that a minimum of noise would be produced by the turbulence of the mixing process itself.
A further object of the invention is to reduce low frequency air turbulence prior to said fuel and air mixing and thereby reducing the amount of noise which would be produced by the combustion.
A still further object is to provide a liquid fuel burner construction in which a venturi-shaped burner head assembly is employed and in which a cone structure serves as a guide for the air.
Another important object is to provide an oil burner construction or the like in which the air delivered to the burner for combustion takes place in the form of a hollow cone and that the fuel is delivered in a second hollow cone inside the air cone preferably having a slightly greater included angle than the air cone. It has been discovered that such structural arrangement causes the fuel and air to mix gradually and in a relatively laminar manner, thereby producing an eflicient and quiet burning flame.
A further object is to provide an oil burner construction in which the mixing of the fuel and air may be conveniently controlled and changed by varying the relative position of the air distributing cone with respect to the outlet side of the venturi.
With these and other objects in view, our invention consists in the construction, arrangement and combination of the various parts of my oil burner whereby the objects contemplated are obtained as hereinafter more fully set forth, pointed out in our claims and illustrated in the accompanying drawing, wherein:
FIG. 1 is a sectional assembly view of an oil burner assembly embodying our invention.
FIG. 2 is an end elevational view, looking in the direction of the nozzle and throat shown in FIG. 1.
Referring now to the drawing, the numeral 1 is used to designate generally a gun-type oil burner constructed in accordance with the present invention, having a casing 2, to which is attached in any suitable manner the blast tube 3, The casing 2 includes a lower portion thereof 3,003,548 Patented Oct. 10, 1961 for receiving an air blower 4 attached in the well known manner and supplying air thereto as indicated by the arrows. The upper portion of the casing 2. is provided with the air outlet port which is in communication with the outer end of the blast tube as illustrated.
Upon the inside of the said blast tube and at an upper annular portion the longitudinally extending electrode wires 6 and 8 are mounted in the respective insulated supports 5 and 7.
Suitably carrying the said insulated supports and lining the inner peripheral surface of the blast tube 3 for substantially its entire length is the cylindrical insert member generally designated 10 having an annular recessed or chamber portion 9 for a substantial part of the length of the said insert member. Thus the length of the chamber portion 9 is defined by the space between the respective end disposed protruded portions 18 and 19, the latter portions being of annular configuration and snugly received within the blast tube 3 at outer and inner ends of said tube as indicated.
At the inner end of the electrode wires 11 and 12, the respective connections are made at 11 and 12 to a source (not shown) of electrical ignition for the said electrode wires.
Within the liner or insert member 10 and mounted in transverse relation thereto is the fixed spider having the radially extending spokes 13 as illustrated and with the central apertured hub portion provided to carry the feed piping to the fuel spray nozzle 15. The location of the latter member is in proximity to the end portion of the blast tube and has the hollow cone 14 extending to the inner end of the blast tube 3. The latter construction is a significant feature of this invention and particularly so when considered with the frusto-conical inner surface 17, the latter surface being substantially of the same length as the hollow cone 14. It will be now appreciated that the air is thus delivered in the form of a hollow cone and that the fuel is delivered in a second hollow cone inside the air cone and preferably having a slightly greater included angle than the air cone.
At the outer end of the cylindrical insert 10, the frustoconical surface 16 is provided.
It will of course be appreciated that the drawing is largely diagrammatic in character, and therefore changes may be made in the construction and arrangement of the parts of our oil burner without departing from the real spirit and purpose of our invention. It is therefore our intention to cover by our claims any modified forms of structure or use of mechanical improvements which may be reasonably included in their scope.
What we claim as new and desire to obtain by Letters Patent of the United States is:
We claim:
1. A liquid fuel burner comprising an elongated air blast tube having inner and outer peripheral end portions and with its outer end portion ported to receive inlet air flow, the other end portion thereof being adapted to discharge into a combustion chamber, a hollow sleeve-like insert member of substantially elongated cylindrical configuration cooperating with the inner peripheral surface .of said air blast tube to bear against the inner and the outer peripheral end portions of the tube, the said insert member having at least the inner end portion thereof with an annular surface of outwardly flaring form, the remaining portion of the insert member merging with the outwardly flaring inner end portion of the insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the outwardly flaring inner end portion with the remaining portion of the said insert member, ported means mounted within the hollow insert member cooperating with said fuel nozzle to centrally position the latter memher in spaced relation to the inner wall of the said insert member, a substantially frusto-conical hollow outwardly flaring cone member cooperating with said nozzle and being of a length approximating the said outwardly flaring inner end portion of the insert member, the included angle of said frusto-conical cone member being approximately equal to the included angle formed by the outwardly flaring annular surface of the inner end portion of the said insert member whereby to form a ring-like continuously outwardly flaring passage between said hollow cone member and the outwardly flaring annular surface of the inner end portion of the insert member.
2. A liquid fuel burner comprising anelongated air blast tube with inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the opposite end portion thereof being adapted to discharge into a combustion chamber, a hollow insert member in the tube with an inner wall surface of substantially cylindrical configuration and with the outer peripheral end portions thereof cooperating with the inner and the outer peripheral end portions of the said air blast tube to line the inner peripheral wall surface of the latter member, the said insert member having at least the inner end portion thereof of outwardly flaring form merging with the remaining inner peripheral wall surface of said hollow insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the outwardly flaring inner end portion with the remaining portion of the said insert member, ported means adjacent the outer end portion of the said blast tube cooperatin with said fuel nozzle to position the latter member in spaced relation to the said inner peripheral wall surface of the said insert member, a substantially hollow cone member fitted over an inner end portion of said nozzle, the said cone member being of a length to extend to theinner end portion of the air blast tube and forming with the said inner portion of the insert member an annular continuously flaring passage over the said nozzle of substantially frusto-conical configuration, the included angle of the cone member being approximately equal to the included angle of the outwardly flaring portion of the insert member, the said fuel nozzle entering said cone member at the outer reduced end of the latter member.
3. A liquid fuel burner comprising an elongated cylindrical air blast tube having inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the opposite end portion thereof being adapted to project into a combustion chamber, a hollow insert member of substantially cylindrical configuration fitted over the inner peripheral wall surface of said air blast tube, the said insert member having at least the inner end portion thereof outwardly flared to merge with the remaining portion of the insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation adjacent to the point of merger of the out- 'wardly flaring inner end portion with the remaining portion of the said insert member, ported means within said insert member axially spaced from the said outwardly flared portion of said insert member and cooperating with said fuel nozzle to position the latter member in spaced relation to the inner end portion of the said insert member, a frusto-conical hollow cone mounted over said nozzle with its reduced end connected to said nozzle and being in substantially the same transverse plane as the said point of merger of said insert member and having an included angle approximating that of the outwardly flared inner end portion of the said insert member.
4. A liquid fuel burner comprising an elongated air blast tube having inner and outer peripheral end portions and with its outer end portion adapted to receive inlet air flow, the inner end portion thereof being adapted to discharge into a combustion chamber, a hollow insert member of substantially cylindrical configuration cooperating with the inner peripheral wall of said air blast tube, the said insert member having at least the inner end portion thereof of outwardly flaring form with a curved annular surface merging with a wall inner surface defining an elongated substantially cylindrical cham her in said insert member, a fuel nozzle mounted in spaced apart longitudinally coaxial relation to said outwardly flaring inner end portion of the said insert mem ber, fixed means engaging the insert member and cooperating with said fuel nozzle to position the latter member in spaced relation to the inner wall of the said insert member and being axially removed from the outwardly flaring portion of the insert member, a substantially hollow outwardly flaring cone mounted over an end portion of said nozzle and cooperating with the outwardly flaring portion of the insert member to form a passage around the outer sloping surface of the cone adapted to direct a flaring air stream forwardly from the said outer end portion of the blast tube into a combustion chamber, said passage being of continuous outwardly flaring annular configuration, the hollow cone being of a length suflicient to extend inwardly at least to the said inner end portion of the said air blast tube, the included angle of said hollow cone being approximately equal to the included angle of the outwardly flaring portion of the said insert member.
References Cited in the file of this patent UNITED STATES PATENTS 1,130,124 White Mar. 2, 1915 1,676,501 Moors July 10, 1928 1,799,355 Cole Apr. 7, 1931 2,132,521 Voorheis Oct. 11, 1938 2,216,508 Zink Oct. 1, 1940 2,465,712 Clarkson Mar. 29, 1949 2,689,001 Leysen Sept. 14, 1954 FOREIGN PATENTS 377,474 Great Britain July 28, 1932 178,351 Switzerland July 15, 1935
US682448A 1957-09-06 1957-09-06 Liquid fuel burner Expired - Lifetime US3003548A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US682448A US3003548A (en) 1957-09-06 1957-09-06 Liquid fuel burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US682448A US3003548A (en) 1957-09-06 1957-09-06 Liquid fuel burner

Publications (1)

Publication Number Publication Date
US3003548A true US3003548A (en) 1961-10-10

Family

ID=24739751

Family Applications (1)

Application Number Title Priority Date Filing Date
US682448A Expired - Lifetime US3003548A (en) 1957-09-06 1957-09-06 Liquid fuel burner

Country Status (1)

Country Link
US (1) US3003548A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2552374A1 (en) * 1974-11-18 1976-05-20 Mitsubishi Heavy Ind Ltd BURNERS FOR LIQUID OR GASEOUS FUEL
US4019851A (en) * 1975-09-22 1977-04-26 Combustion Engineering, Inc. High energy arc ignitor for burner
US4110063A (en) * 1975-07-03 1978-08-29 Mitchell Douglas Allison Gas fire
US4171199A (en) * 1977-09-27 1979-10-16 Joseph Henriques Frustoconical burner can assembly
US4313721A (en) * 1979-03-15 1982-02-02 Joseph Henriques Oil burner diffuser

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1130124A (en) * 1914-03-09 1915-03-02 William Albert White Furnace-front.
US1676501A (en) * 1919-11-26 1928-07-10 Recip Roto Engine Company Burner
US1799355A (en) * 1927-12-09 1931-04-07 Timken Detroit Company Oil burner
GB377474A (en) * 1930-12-17 1932-07-28 Hanrez Sa J Atel Improvements in or relating to process and burner for the combustion of powdered coal
CH178351A (en) * 1934-07-02 1935-07-15 Brevo A G Fuer Explosions Und Atomizing burners for liquid fuel.
US2132521A (en) * 1934-12-26 1938-10-11 Joseph T Voorheis Burner construction
US2216508A (en) * 1938-10-26 1940-10-01 John S Zink Combination gas and oil burner
US2465712A (en) * 1944-10-21 1949-03-29 Clarkson Alick Louvered air register for oil burners
US2689001A (en) * 1949-07-12 1954-09-14 Leyle V Leysen Fluid fuel burner

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1130124A (en) * 1914-03-09 1915-03-02 William Albert White Furnace-front.
US1676501A (en) * 1919-11-26 1928-07-10 Recip Roto Engine Company Burner
US1799355A (en) * 1927-12-09 1931-04-07 Timken Detroit Company Oil burner
GB377474A (en) * 1930-12-17 1932-07-28 Hanrez Sa J Atel Improvements in or relating to process and burner for the combustion of powdered coal
CH178351A (en) * 1934-07-02 1935-07-15 Brevo A G Fuer Explosions Und Atomizing burners for liquid fuel.
US2132521A (en) * 1934-12-26 1938-10-11 Joseph T Voorheis Burner construction
US2216508A (en) * 1938-10-26 1940-10-01 John S Zink Combination gas and oil burner
US2465712A (en) * 1944-10-21 1949-03-29 Clarkson Alick Louvered air register for oil burners
US2689001A (en) * 1949-07-12 1954-09-14 Leyle V Leysen Fluid fuel burner

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2552374A1 (en) * 1974-11-18 1976-05-20 Mitsubishi Heavy Ind Ltd BURNERS FOR LIQUID OR GASEOUS FUEL
US4110063A (en) * 1975-07-03 1978-08-29 Mitchell Douglas Allison Gas fire
US4019851A (en) * 1975-09-22 1977-04-26 Combustion Engineering, Inc. High energy arc ignitor for burner
US4171199A (en) * 1977-09-27 1979-10-16 Joseph Henriques Frustoconical burner can assembly
US4313721A (en) * 1979-03-15 1982-02-02 Joseph Henriques Oil burner diffuser

Similar Documents

Publication Publication Date Title
US4872833A (en) Gas burner construction
GB1154098A (en) Multi-Fuel Burner Nozzle.
ES465796A1 (en) Blue-flame oil burner
US3003548A (en) Liquid fuel burner
US3393650A (en) Slurry burner
US1330048A (en) Blue-flame gas-burner
US2525432A (en) Gaseous fuel burner, including flame retainer
US2537542A (en) Flame retention head for gas burners
GB1168064A (en) An Improved Inspirator Assembly for a Gasburner
GB1100889A (en) Burner assembly producing radiant heat
ES406859A2 (en) Burner for liquid fuels
ES453830A1 (en) Coal burner
GB1448924A (en) Atomiser for liquids particularly for use in burning liquid fuels
US2659427A (en) Oil burner nozzle head element
US1934379A (en) Oil burner
GB310555A (en) Improvements in or relating to burners for pulverulent fuel or/and liquid fuel
SU579499A1 (en) Oil-gas combination burner
US1533509A (en) Liquid and gas mixer
GB953277A (en) Improvements in or relating to combined liquid and gaseous fuel burners
GB1358192A (en) Liquid-fuel burner
SU840570A1 (en) Injection nozzle
US1093495A (en) Blowpipe.
SU1672119A1 (en) Mixer of two-phase flows
GB1197998A (en) Improvements in or relating to Fuel Burners
US1576729A (en) Illuminating-gas blowpipe