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US3308870A - Oil burner air cone - Google Patents

Oil burner air cone Download PDF

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Publication number
US3308870A
US3308870A US400516A US40051664A US3308870A US 3308870 A US3308870 A US 3308870A US 400516 A US400516 A US 400516A US 40051664 A US40051664 A US 40051664A US 3308870 A US3308870 A US 3308870A
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Prior art keywords
air
oil burner
nozzle
cone
oil
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Expired - Lifetime
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US400516A
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Jr John P Rex
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Rex Roto Corp
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Rex Roto Corp
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Priority to US400516A priority Critical patent/US3308870A/en
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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B28/00Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
    • C04B28/24Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing alkyl, ammonium or metal silicates; containing silica sols
    • C04B28/26Silicates of the alkali metals
    • 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
    • F23D11/40Mixing tubes; Burner heads
    • F23D11/408Flow influencing devices in the air tube

Definitions

  • an air cone as hereinafter described in detail is constructed with a refractory insulating material capable of withstanding operating temperatures combined with properties of minimum mass, heat conductivity and storage capacity.
  • FIG. 1 is a side elevation of a gun-type oil burner nozzle partially sectioned to show the nose cone installation
  • FIG. 2 is an enlarged rear elevation of the nose cone per se as seen along the line 22 of FIG. 1;
  • FIG. 3 is a side elevation of the nose cone per se shown in FIG. 2 partially sectioned to show interior air passage construction
  • FIG. 4 is a fragmentary sectional view taken along the line 4-4 of FIG. 3;
  • FIG. 5 is a fragmentary sectional view taken along the line 5-5 of FIG. 3.
  • the gun-type burner housing encloses an oil nozzle 11 fed by tube 12 and discharging oil spray into a furnace combustion chamber through air cone 13, mounted within the housing 10.
  • air cone frequently referred to as a nose cone or stabilizer, includes a plurality of fluted passages 14 around the internal wall thereof adapted to induce a swirling action to the air flow surrounding the oil nozzle to assist in atomizing the oil spray for as rapid and complete combustion as possible.
  • a lightweight, fibrous refractory air cone may reduce operating temperatures in the order of 100 to 150 below metal cone operating temperatures, will substantially eleminate heat retention and storage, and solves the problem of nozzle coking substantially if not 3,308,870 Patented Mar. 14, 1967 entirely.
  • the preferred materials employed in manufacturing such air cones are aluminum silicate fibers and a colloidal silica binder.
  • a typical specification for the aluminum silicate fiber is as follows:
  • the fibrous material is preferably molded with an inorganic binder having the following properties:
  • Viscosity at 25 C. cps 3.6.
  • a 20 lb. per cubic foot fiber density bonded with 20 to 50% by weight of binder and resulting in a 25 lb. to 40 lb. per cubic foot density has been found after considerable experimentation to provide a range within which desired balance of durability, lightweight, minimum operating temperature and heat retention characteristics may be obtained.
  • An oil burner nozzle air nose cone comprising a molded fibrous re'fractory ring, said ring being held in a stable nose cone form by an inorganic refractory binder, said ring being adapted for retention in an air tube surrounding an oil burner nozzle, said ring having a plurality of flutes molded in its internal surface adapted to induce a swirling movement of incoming air in order to mix incoming combustion air with an oil spray ejected from said nozzle, and said internal surface forming the most immediate adjacent element surrounding said oil burner nozzle.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)

Description

March 14, 1957 J- P. REX, JR 3,308,870
OIL BURNER AIR CONE Filed Sept. 30, 1964 FIG..].
/NVENTO/? JOHN P. REX JR.
ATTORNEYS United States Patent 3,308,870 OIL BURNER AIR CONE John P. Rex, Jr., Fenton, Mich., assignor to Rex Roto Corporation, Walled Lake, Mich., a corporation of Michigan Filed Sept. 30, 1964, Ser. No. 400,516 1 Claim. (Cl. 15876) This invention relates to the discovery that oil burner coking with resultant inefiiciency and smoking result primarily from radiant and convective heat flow into the nozzle after the furnace is off and the cooling oil flow has stopped and that such coking can be entirely or substantially eliminated through the provision of an air cone which minimizes heat absorption and storage during operation of the furnace and insulates the nozzle from heat transfer when the burner shuts off.
In accordance with the present invention an air cone as hereinafter described in detail is constructed with a refractory insulating material capable of withstanding operating temperatures combined with properties of minimum mass, heat conductivity and storage capacity.
The objects of the invention may best be understood from the following detailed description of a preferred embodiment as illustrated in the drawings wherein:
FIG. 1 is a side elevation of a gun-type oil burner nozzle partially sectioned to show the nose cone installation;
FIG. 2 is an enlarged rear elevation of the nose cone per se as seen along the line 22 of FIG. 1;
FIG. 3 is a side elevation of the nose cone per se shown in FIG. 2 partially sectioned to show interior air passage construction;
FIG. 4 is a fragmentary sectional view taken along the line 4-4 of FIG. 3; and
FIG. 5 is a fragmentary sectional view taken along the line 5-5 of FIG. 3.
As shown in FIG. 1 the gun-type burner housing encloses an oil nozzle 11 fed by tube 12 and discharging oil spray into a furnace combustion chamber through air cone 13, mounted within the housing 10. Such air cone, frequently referred to as a nose cone or stabilizer, includes a plurality of fluted passages 14 around the internal wall thereof adapted to induce a swirling action to the air flow surrounding the oil nozzle to assist in atomizing the oil spray for as rapid and complete combustion as possible.
It is conventional practice to construct such air cone as a cast iron or stamped steel element which during operation absorbs a considerable amount of heat from the furnace combustion chamber producing in many cases a radiant temperature reflected onto the nozzle and heating the same to a substantial temperature notwithstanding the internal cooling oil fiow and surrounding air flow. Upon shut-off of the nozzle immediately following firing the stored heat radiating and passing by convection from a cast iron or stamped steel air cone to the nozzle, in the absence of the cooling oil and air flow, may substantially elevate the temperature of the nozzle and oil therein, as well as back somewhat into the feed line 12, to a coking temperature. The progressive build-up of deposit layers within the feed tube and nozzle with successive firings gradually restricts the oil passage to a progressively smaller effective orifice upsetting the proper air fuel mixture ratio, producing a reduction in heat, heat efficiency and eventual smoking of the oil burner from incomplete combustion.
I have discovered that a lightweight, fibrous refractory air cone may reduce operating temperatures in the order of 100 to 150 below metal cone operating temperatures, will substantially eleminate heat retention and storage, and solves the problem of nozzle coking substantially if not 3,308,870 Patented Mar. 14, 1967 entirely. The preferred materials employed in manufacturing such air cones are aluminum silicate fibers and a colloidal silica binder.
A typical specification for the aluminum silicate fiber is as follows:
Color White.
Fiber length Short to 1 /2 inches.
Fiber diameter Submicron to 10 microns,
mean of 2% microns.
Specific gravity 2.73.
Bulk density 20 lbs. per cubic foot.
The approximate chemical analysis of this material in percentage by weight is as follows: A1 0 51.2%; SiO 47.4%; B 0 0.7%; Na O, 0.7%.
The fibrous material is preferably molded with an inorganic binder having the following properties:
Percent colloidal silica as SiO 30.0.
Ratio, wt., SiO /Na O 95.
Chloride as NaCl 0.04%.
Sulfate as Na SO 0.05%.
Viscosity at 25 C., cps 3.6.
pH at 25 C 9.8.
Surface area B.E.T. method m. g. 210.
Approximate particle diameter 15 mu.
Turbidity 21.
Stability Stable, except toward freezing,
. which causes irreversible precipitation. Freezing point 32 F.
A 20 lb. per cubic foot fiber density bonded with 20 to 50% by weight of binder and resulting in a 25 lb. to 40 lb. per cubic foot density has been found after considerable experimentation to provide a range within which desired balance of durability, lightweight, minimum operating temperature and heat retention characteristics may be obtained.
While a preferred embodiment of the present invention has been described in detail it will be understood that certain modifications there-to may be resorted to without departing from the scope of the invention as defined in the following claim.
I claim:
An oil burner nozzle air nose cone comprising a molded fibrous re'fractory ring, said ring being held in a stable nose cone form by an inorganic refractory binder, said ring being adapted for retention in an air tube surrounding an oil burner nozzle, said ring having a plurality of flutes molded in its internal surface adapted to induce a swirling movement of incoming air in order to mix incoming combustion air with an oil spray ejected from said nozzle, and said internal surface forming the most immediate adjacent element surrounding said oil burner nozzle.
References Cited by the Examiner UNITED STATES PATENTS 1,591,679 7/1926 Hawley 28 1,656,711 1/1928 Scott l5876 X 3,202,197 8/1965 Knobloch l581 3,208,502 9/1965 Carlson l5876 X 3,213,917 10/1965 Scheppers 158-1 FREDERICK L. MATTESON, JR., Primary Examiner. E. G. FAVORS, Assistant Examiner.
US400516A 1964-09-30 1964-09-30 Oil burner air cone Expired - Lifetime US3308870A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3556412A (en) * 1968-06-18 1971-01-19 Koppers Co Inc Burner nozzle for hot blast stove
US4479775A (en) * 1981-12-04 1984-10-30 Sivan Development And Implementation Of Technological Systems Ltd. Vane structure burner for improved air-fuel combustion
US4913646A (en) * 1988-05-18 1990-04-03 Kockums Marine Ab Combustion device
US5431343A (en) * 1994-03-15 1995-07-11 Nordson Corporation Fiber jet nozzle for dispensing viscous adhesives

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1591679A (en) * 1921-01-15 1926-07-06 Peoples Savings & Trust Compan Process for the combustion of ash-containing fuels
US1656711A (en) * 1926-03-20 1928-01-17 Lewis L Scott Oil burner
US3202197A (en) * 1963-04-16 1965-08-24 George H Knobloch Furnace including refractory sealing sleeve for the nozzle of an oil burner
US3208502A (en) * 1961-03-08 1965-09-28 Babcock & Wilcox Ltd Fuel burners having air control means
US3213917A (en) * 1963-07-10 1965-10-26 Johns Manville Furnace combustion chambers

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1591679A (en) * 1921-01-15 1926-07-06 Peoples Savings & Trust Compan Process for the combustion of ash-containing fuels
US1656711A (en) * 1926-03-20 1928-01-17 Lewis L Scott Oil burner
US3208502A (en) * 1961-03-08 1965-09-28 Babcock & Wilcox Ltd Fuel burners having air control means
US3202197A (en) * 1963-04-16 1965-08-24 George H Knobloch Furnace including refractory sealing sleeve for the nozzle of an oil burner
US3213917A (en) * 1963-07-10 1965-10-26 Johns Manville Furnace combustion chambers

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3556412A (en) * 1968-06-18 1971-01-19 Koppers Co Inc Burner nozzle for hot blast stove
US4479775A (en) * 1981-12-04 1984-10-30 Sivan Development And Implementation Of Technological Systems Ltd. Vane structure burner for improved air-fuel combustion
US4913646A (en) * 1988-05-18 1990-04-03 Kockums Marine Ab Combustion device
US5431343A (en) * 1994-03-15 1995-07-11 Nordson Corporation Fiber jet nozzle for dispensing viscous adhesives

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