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Publication numberUS3339613 A
Publication typeGrant
Publication dateSep 5, 1967
Filing dateJan 4, 1965
Priority dateJan 4, 1965
Also published asDE1501801A1
Publication numberUS 3339613 A, US 3339613A, US-A-3339613, US3339613 A, US3339613A
InventorsAatto P Saha
Original AssigneeCarrier Corp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Flame stabilization
US 3339613 A
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Description  (OCR text may contain errors)

p 1967 A. P. SAHA FLAME STABILIZATION Filed Jan." 4, 1965 INVENTOR AATTO P. SAHA BY ATTORNEY.

United States Patent 3,339,613 FLAME STABILIZATION Aatto P. Saha, Jamesville, N.Y., assignor to Carrier Corporation, Syracuse, N.Y., a corporation of Delaware Filed Jan. 4, 1965, Ser. No. 423,251 5 Claims. (Cl. 158--1.5)

This invention relates to combustion of dispersible fuels and, more particularly, to stabilizing and effectively preventing lifting of the flame from a dispersible fuel burner.

The term dispersible fuel includes fuels such as solid fuels in powdered or pulverized form such as powdered coal, and fluid fuels such as gaseous, vaporous or liquid fuels, for example, combustible gases and vapors as well as combustible liquids such as fuel oils, capable of being atomized as by spraying and the like.

Pulsations of the flame produced by dispersible fuel burners cause uneven transfer of heat and intermittent periods or cycles of incomplete combustion, as is more fully discussed in my prior United States Patent 2,539,165, and the present invention is an improvement thereon.

The present invention is directed to improved combustion in a dispersible fuel burner by provision of a pocket extending from a fuel nozzle to an air inlet through which a vortex of air is introduced into a furnace.The pocket is an improvement on the sleeve-like flame stabilizer which is the subject of my aforementioned patent..

It is a primary object of this invention to provide a new and improved apparatus and method for the combustion of dispersible fuel and, more particularly, for stabilizing and effectively preventing lifting of the flame at a dispersible fuel nozzle.

Another object is provision of new and improved apparatus for burning dispersible fuel including a furnace and a nozzle at one end of the furnace for passing dispersible fuel into the furnace to generate a flame, with an air inlet axially spaced from the nozzle for passing a vortex into the furnace to combine with the fuel and move axially through the furnace, and a pocket extending about the nozzle to the air inlet for holding a portion of the vortex to stabilize and effectively prevent lifting of the flame at the nozzle.

Still another object is provision of a new and improved method of stabilizing and effectively preventing lifting of a flame from a dispersible fuel nozzle by establishing about the nozzle a vortex substantially devoid of axial velocity and generally coaxial with the nozzle.

Additional objects and advantages of the invention will be apparent from the following description and drawing in which:

FIGURE 1 is a fragmentary, longitudinal sectional view of a furnace and a burner for dispersible fuel; and

FIGURE 2 is a vertical sectional view, taken generally along the line IIII in FIGURE 1.

Referring to the drawing, a furnace 11 is illustrated in generally cylindrical form within a boiler shell 12. The furnace 11 has a dispersible fuel burner 13 at one end and at an opposite end opening into a flue gas header 14. From the header flue gas may pass through return fire tubes 14a to a flue 14b, or alternatively, directly to a flue.

The burner 13 includes a fuel dispersing nozzle 15, here in the form of a flat perforated plate facing into the furnace 11 on its front side and on its rear side facing a fuel chamber 16 communicating with a suitable fuel line 17 for passage of dispersible fuel through the perforations and into the combustion chamber of the furnace.

Vortex forming means includes an air inlet 18 for providing substantially a rapidly rotating, annular combustion air stream 18a moving along the inner surface of the combustion chamber and about a relatively slowly rotating core 18b delimited from the stream 18a by a 3,339,613 Patented Sept. 5, 1967 flame front and all moving axially along the longitudinal axis of the furnace 11. The inlet 18 opens into the end of the furnace adjacent the nozzle 15 and may be of any suitable type, for example, as shown in my Patent 2,097,255, and in FIGURE 2 wherein the inlet includes a plurality of vanes 19 having inner ends defining an imaginary circle with a diameter D which may be the same as or suitably larger or smaller than the cylindrical vortex confining furnace wall diameter D The vanes 19 receive air through an air plenum 20 from a suitable blower (not shown) and discharge the air through open areas A, between the inner ends of the vanes which are generally tangent to the imaginary circle.

In order to stabilize the flame and for effectively preventing lifting of the flame at the nozzle 15, a ceramic end Wall 20a forms a pocket 21 with the furnace and extends to the air inlet 18 so that a portion of the tvortex created at the air inlet is established rearwardly of the inlet and is substantially static in an axial direction to provide a quiescent zone about the nozzle to hold and stabilize the flame at the nozzle. The pocket 21 should have a diameter greater than the diameter of the core of the vortex at the inlet so that the vortex may be established and maintained in the pocket.

The diameter of the core of the vortex is a function of the vortex forming means and is related to a Vortex Constant C which is the sum of the tangential area or areas A, of the discharge passage at the outlets between the vanes divided by the product of the inlet or inner diameter across the vane circle of the vortex forming means D times the diameter of the furnace D that is i D D; Within normal working limits, for a given Vortex Constant the pocket diameter must be more than the potential core diameter D at the flame front 21a and may be stated as a percent of the diameter of the furnace or other confining surface as follows:

crete jets, the centrifugal force imparted to the jets by the core cause better dispersal of the fuel and more even combustion than occurs with a single, large jet normally injected into the center of the core where centrifugal force is negligible. The quiescent zone of the vortex in the pocket 21 provides for slow combustion of the entering fuel from the nozzle through interdiffusion of the-fuel and air in the vortex in the pocket, and absence of axial velocity of the air in the pocket effectively prevents the flame from being lifted from the nozzle.

By providing adequate flame holding and stabilization of the flame, higher axially velocity of the flame can be tolerated in the furnace without lifting of the flame, so that for a given furnace area or volume the heat release is greater while facilitating uniform heating without peaking and permitting a reduction in the diameter of the combustion chamber for a given heat output.

While a preferred embodiment of the invention has been described and illustrated, it will be understood the invention is not limited thereto since it may be otherwise embodied within the scope of the following claims.

I claim.

1. An apparatus for burning dispersible fuel comprising a furnace having a combustion chamber, a nozzle at an end of said furnace for passing dispersible fuel into said combustion chamber of the furnace to mix with air and generate a flame, means including an air inlet between said nozzle and said combustion chamber for providing in said combustion chamber a vortex of air moving axially therethrough and generally along the wall thereof and mixing with said fuel, and means for receiving said vortex and providing a quiescent zone stabilizing and eflectively preventing lifting of the flame at the nozzle including a pocket about said nozzle extending from said nozzle to the annular origin of said air stream at said air inlet.

2. An apparatus for burning dispersible fuel comprising means defining a furnace having a combustion chamher for the passage of a vortex having an annular portion rotating relatively rapidly along the wall thereof and about a relatively nonrotating core with the vortex moving axially through said combustion chamber, means including a nozzle at an end of said furnace for passing dispersible fuel into said combustion chamber to mix with the air in said vortex and generate a flame, means including an air inlet between said nozzle and said combustion chamber and spaced axially of said furnace from said nozzle for providing said vortex in said combustion chamber, and means for receiving said vortex and providing a quiescent zone stabilizing and effectively preventing lifting of the flame at the nozzle including a pocket about said nozzle and extending substantially from said nozzle to said air inlet and having a diameter at said inlet greater thn the diameter of the vortex core.

3. An apparatus for burning dispersible fuel comprising a nozzle for passing dispersible fuel to mix with air and generate a flame, means including an air inlet downstream of said nozzle for providing a vortex including a rotating, annular air stream about a core for mixing with said fuel, and means for stabilizing and effectively preventing lifting of the flame at the nozzle including a pocket about said nozzle and extending to the annular origin of said air stream, said pocket having a diameter at said inlet greater than the diameter of said core.

4. A method of stabilizing and effectively preventing lifting of a flame from a dispersible fuel nozzle comprising the steps of passing dispersible fuel through said nozzle, and establishing aboutsaid nozzle a substantially axially static vortex of combustion air generally axially aligned with said nozzle.

5. A method of stabilizing and effectively preventing lifting of a flame from a dispersible fuel nozzle comprising the steps of passing dispersible fuel through said nozzle, downstream of said nozzle generating a vortex of combustion air generally axially aligned with said nozzle, and establishing about said nozzle a portion of said vortex substantially devoid of axial velocity.

References Cited UNITED STATES PATENTS 1,795,347 3/1931 Reese 11028 2,097,255 10/1937 Saha 1581 2,678,615 5/1954 Soderlund et a1 1l0-28 FOREIGN PATENTS 270,295 1/ 1928 Great Britain. 705,447 3/ 1954 Great Britain.

30 FREDERICK L. MATTESON, ]R., Primary Examiner.

E. G. FAVORS, Assistant Examiner.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1795347 *Jul 18, 1927Mar 10, 1931Erie City Iron WorksFurnace
US2097255 *Mar 15, 1935Oct 26, 1937 Method of and apparatus fob burn
US2678615 *Jan 25, 1950May 18, 1954Rosenblad CorpMethod for burning sticky, watercontaining liquid fuel
GB270295A * Title not available
GB705447A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3677532 *Jul 6, 1970Jul 18, 1972Wolfersperger John JTwo chamber fuel burner
US3718122 *Mar 15, 1971Feb 27, 1973Agrest JFiring chamber for the combustion of gaseous, liquid or fine-granular fuel
US4120640 *Feb 18, 1977Oct 17, 1978Infern-O-Therm CorporationBurner for liquid fuel
Classifications
U.S. Classification431/173, 431/190, 431/349
International ClassificationF23C7/02, F23D11/00, F23D14/00
Cooperative ClassificationF23C7/02, F23D14/00, F23D11/00
European ClassificationF23D11/00, F23D14/00, F23C7/02