US1921059A - Fuel burner - Google Patents

Fuel burner Download PDF

Info

Publication number
US1921059A
US1921059A US548846A US54884631A US1921059A US 1921059 A US1921059 A US 1921059A US 548846 A US548846 A US 548846A US 54884631 A US54884631 A US 54884631A US 1921059 A US1921059 A US 1921059A
Authority
US
United States
Prior art keywords
fuel
valve
nozzle
sleeve
chamber
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
US548846A
Inventor
Joseph M Weil
Wilson Levi
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.)
Ingersoll Rand Co
Original Assignee
Ingersoll Rand 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 Ingersoll Rand Co filed Critical Ingersoll Rand Co
Priority to US548846A priority Critical patent/US1921059A/en
Application granted granted Critical
Publication of US1921059A publication Critical patent/US1921059A/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
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour

Definitions

  • This invention relates to burners, but more particularly to burners adapted to properly proportion and mix the constituent elements, such as fuel and air which, when combined form the 5 fuel charge for furnaces and the like.
  • One object of the invention is to effectively oxygenize and atomize the fuel.
  • Another object is to effect such mixture of elements forming the fuel charge at a point exteriorly of the burner.
  • Oil burners in common use convey oil through a tube and discharge it through a small opening intended to break the stream of fuel up into a fine spray. It is customary to arrange for a current of air to envelop the spray and mix with it to make complete combustion possible.
  • Such devices invariably introduce the air stream to the fuel stream at the instant the latter emerges from its nozzle, and the air current is con- 2 ducted to the opening of the fuel nozzle by a stream lined nozzle cover or equivalent means.
  • This form of construction has a serious disadvantage for the stream of liquid and the stream of air make such gentle contact that the latter simply surrounds the former and prevents its proper atomization.
  • the present invention arranges the fuel'jet somewhat to the rear of the annular air jet, so that the movement of fuel and the movement of air exert an ejector action upon the space between the two jets, thereby creating an area of low pressure adapted to assist diffusion of the oil spray.
  • the two jets actively intersect each other at a distance from the nozzles in an annulus of mingled air and oil spray which insures thorough mixing of the elements resulting in rapid and complete combustion of the oil.
  • Still another object is to enable the burner to be readily adjusted to vary the proportions of the elements forming the fuel charge.
  • FIG. 1 is a sectional elevation of a fuel burner constructed in accordance with the practice of the invention
  • Figure 2 is a sectional plan view taken through Figure l on the line 2-2 looking in the direction indicated by the arrows, and
  • Figure 3 is a transverse view taken through V Figure 2 on the line 33 looking in the direction indicated by the arrows.
  • the burner which is designated generally by A, is shown secured to a hollow pedestal or supply pipe B through which pressure fluid, such as air,
  • . may flow from a source into a chamber C within shown) wherewith burners of this character are usually employed.
  • a tubular nozzle H Disposed within the chamber C and prefer- 7o ably coaxial with the outlet opening F is a tubular nozzle H in the form of a tube of substantially uniform diameter throughout its length and having one end secured to the head D, as for instance, by a threaded connection and the opposite or free end is rolled or piened over or otherwise restricted and has a port J in the restricted end from which fuel is projected through the outlet opening F.
  • the nozzle H is l of such length that the restricted or outlet end terminates at a point within the chamber C so that, in effect, the fuel issuing therefrom is also projected through a portion of the chamber C adjacent the outlet opening F7
  • the fuel supply for the nozzle H is conveyed 8 thereto by a suitable conduit K which may lead from a source of fuel supply under pressure and may be provided with suitable valve means, such as that designated by L, for controlling the flow of fuel to the nozzle H.
  • means are provided for effecting the oxygenation of the fuel at a point or region ex- 7 teriorly of the burner or casing A.
  • that portion of the casing A wherein the outlet opening F is located is in the form of a wall 0 which converges toward the outlet opening F.
  • a valve P having a sleeve Q threaded thereto, and said sleeve Q is in engagement with the exterior surface of the nozzle H to prevent leakage of pressure fluid through the sleeve.
  • a bearing member R shown in this instance as being in the form of a bar, having an aperture S to receive the sleeve Q, and a set screw T is threaded into the bar R to seat against the sleeve Q for securing the said bar fixedly to the sleeve.
  • the bar R extends transversely of the chamber C and is provided in its ends with notches U for engagement with guide ribs V which are disposed on opposite sides of the chamber C and may, as illustrated, form integral portions of the casing A.
  • a bar W which, like the bar R, is also provided with suitable notches U to receive the ribs V.
  • Means are provided for conveniently actuating the valve P to determine the area of a space or annular passage X which may exist between the valve and the adjacent surface of the converging wall 0 and through which passage pressure fluid from the chamber C is adapted to flow through the outlet opening F.
  • a screw Y is threaded into the head D and is provided at one end with a plain cylindrical stem Z which is journalled in a bore 2) in the bar W.
  • the free end of the stem Z preferably extends beyond the bar W and has secured thereon a collar or nut c which may be held against accidental displacement by a pin (1.
  • a knob or hand wheel f On the projecting end e of the screw Y is arranged a knob or hand wheel f whereby the screw Y may be 1'0- tated for shifting the valve P with respect to the wall 0.
  • the valve P is of parabolic shape and is truncated to form a flat surface g at that end of the valve for convenience in forming the threaded aperture it into which the sleeve Q is threaded.
  • a concavity 7' In the anterior side of the valve P is a concavity 7' through which fuel issuing from the nozzle H flows to and through the outlet opening F.
  • the rim or outer edge k of the base thus remaining is preferably rounded and is adapted toseat against the adjacent surface of the converging wall 0 to seal the chamber C at will and thus prevent the flow of pressure fluid from the chamber through the outlet opening F.
  • the ejector action of the streams of air and fuel create an area of low pressure within the concavity a' thereby assisting in the diffusion of spray from the fuel nozzle H.
  • the point of convergence of the air jet is substantially coincident with the axis of the fuel projected from the nozzle H and lies exteriorly of the casing A.
  • the hollow jet of air issuing from the passage X encircles the fuel flowing from the port J there is no ,free commingling of fuel and pressure fluid within the casing A.
  • the process of mixing of these elements takes place outside of the burner as does also that of thoroughly atomizing the fuel due to the cross currents of the pressure fluid through the fuel stream, thus assuring a readily combustible mixture.
  • valve P may be readily adjusted by means of the screw Y, either to increase or decrease the width of the annular passage X.
  • the valve P By adjusting the valve P in this manner the conoid jet of pressure fluid directed into the fuel will, of course, be either elongated or shortened but, irrespective of its length, the vertex of such jet will be directed into the fuel stream.
  • the screw Y may be manipulated to seat the rim is of the valve P against the wall 0. In this way the flow of pressure fluid from the chamber C may be cut off.
  • the valve P may be closed to cut off the flow of fuel from the nozzle H. With the valve P closed any fuel, such as oil, which may leak or dribble from the port J will merely flow along the wall of the recess 7' and through the outlet opening F to the exterior of the burner, thus assuring against leakage of fuel into the chamber C and the possible formationof a combustible mixture within the casing.
  • a fuel burner comprising a casing having a chamber, a converging wall on the casing having an outlet opening, a fuel nozzle afiixed at one end to the casing and extending longitudinally into the chamber, a sleeve slidable upon the fuel nozzle and in fluid tight engagement therewith, guide ribs upon the inner side of the casing wall, bearing members slidable upon said guide ribs and affixed in spaced relationship to the sleeve, a valve member on the sleeve adapted to coact with the outlet opening of the casing, and means acting upon one of the bearing members to control the pressure fluid outlet by movement of the valve carrying sleeve.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Description

Aug. 8, 1933. J. M w ET AL 1,921,059
FUEL BURNER Filed July 6, 1931 Fig -1.
I N V EN TOR. tl'osqphflmzlilg pd can H15 ATTORNEY.
Patented Aug. 8, 1933 UNITED STATES 1,921,059 FUEL BURNER Joseph M. Weil, Phillipshurg, N. J and Levi Wilson, Easton, Pa., assignors to Ingersoll-Rand Company, Jersey City, N. J., a Corporation of New Jersey Application July 6, 1931.
1 Claim.
This invention relates to burners, but more particularly to burners adapted to properly proportion and mix the constituent elements, such as fuel and air which, when combined form the 5 fuel charge for furnaces and the like.
One object of the invention is to effectively oxygenize and atomize the fuel.
Another object is to effect such mixture of elements forming the fuel charge at a point exteriorly of the burner. Oil burners in common use convey oil through a tube and discharge it through a small opening intended to break the stream of fuel up into a fine spray. It is customary to arrange for a current of air to envelop the spray and mix with it to make complete combustion possible. Such devices invariably introduce the air stream to the fuel stream at the instant the latter emerges from its nozzle, and the air current is con- 2 ducted to the opening of the fuel nozzle by a stream lined nozzle cover or equivalent means. This form of construction has a serious disadvantage for the stream of liquid and the stream of air make such gentle contact that the latter simply surrounds the former and prevents its proper atomization.
To overcome this disadvantage the present invention arranges the fuel'jet somewhat to the rear of the annular air jet, so that the movement of fuel and the movement of air exert an ejector action upon the space between the two jets, thereby creating an area of low pressure adapted to assist diffusion of the oil spray. The two jets actively intersect each other at a distance from the nozzles in an annulus of mingled air and oil spray which insures thorough mixing of the elements resulting in rapid and complete combustion of the oil.
Still another object is to enable the burner to be readily adjusted to vary the proportions of the elements forming the fuel charge.
Other objects will be in part obvious and in part pointed out hereinafter.
In the accompanying drawing forming part of the specification and in which similar reference characters refer to similar parts,
Figure 1 is a sectional elevation of a fuel burner constructed in accordance with the practice of the invention,
5 Figure 2 is a sectional plan view taken through Figure l on the line 2-2 looking in the direction indicated by the arrows, and
Figure 3 is a transverse view taken through V Figure 2 on the line 33 looking in the direction indicated by the arrows.
Serial No. 548,846
Referring more particularly to the drawing, the burner, which is designated generally by A, is shown secured to a hollow pedestal or supply pipe B through which pressure fluid, such as air,
. may flow from a source into a chamber C within shown) wherewith burners of this character are usually employed.
Disposed within the chamber C and prefer- 7o ably coaxial with the outlet opening F is a tubular nozzle H in the form of a tube of substantially uniform diameter throughout its length and having one end secured to the head D, as for instance, by a threaded connection and the opposite or free end is rolled or piened over or otherwise restricted and has a port J in the restricted end from which fuel is projected through the outlet opening F. The nozzle H is l of such length that the restricted or outlet end terminates at a point within the chamber C so that, in effect, the fuel issuing therefrom is also projected through a portion of the chamber C adjacent the outlet opening F7 The fuel supply for the nozzle H is conveyed 8 thereto by a suitable conduit K which may lead from a source of fuel supply under pressure and may be provided with suitable valve means, such as that designated by L, for controlling the flow of fuel to the nozzle H.
i In accordance with the practice of the invention, means are provided for effecting the oxygenation of the fuel at a point or region ex- 7 teriorly of the burner or casing A. To this end that portion of the casing A wherein the outlet opening F is located is in the form of a wall 0 which converges toward the outlet opening F. Within the chamber C is a valve P having a sleeve Q threaded thereto, and said sleeve Q is in engagement with the exterior surface of the nozzle H to prevent leakage of pressure fluid through the sleeve. At a point intermediate the ends of the sleeve Q is a bearing member R, shown in this instance as being in the form of a bar, having an aperture S to receive the sleeve Q, and a set screw T is threaded into the bar R to seat against the sleeve Q for securing the said bar fixedly to the sleeve. i
The bar R extends transversely of the chamber C and is provided in its ends with notches U for engagement with guide ribs V which are disposed on opposite sides of the chamber C and may, as illustrated, form integral portions of the casing A. Similarly, on that end of the sleeve Q opposite to the end to which the valve P is aflixed is threaded a bar W which, like the bar R, is also provided with suitable notches U to receive the ribs V. The bars R and W and the sleeve Q thus form an adequate bearing for the free end or portion of the nozzle H.
Means are provided for conveniently actuating the valve P to determine the area of a space or annular passage X which may exist between the valve and the adjacent surface of the converging wall 0 and through which passage pressure fluid from the chamber C is adapted to flow through the outlet opening F. To this end a screw Y is threaded into the head D and is provided at one end with a plain cylindrical stem Z which is journalled in a bore 2) in the bar W.
The free end of the stem Z preferably extends beyond the bar W and has secured thereon a collar or nut c which may be held against accidental displacement by a pin (1. On the projecting end e of the screw Y is arranged a knob or hand wheel f whereby the screw Y may be 1'0- tated for shifting the valve P with respect to the wall 0.
Posteriorly, the valve P is of parabolic shape and is truncated to form a flat surface g at that end of the valve for convenience in forming the threaded aperture it into which the sleeve Q is threaded. In the anterior side of the valve P is a concavity 7' through which fuel issuing from the nozzle H flows to and through the outlet opening F. The rim or outer edge k of the base thus remaining is preferably rounded and is adapted toseat against the adjacent surface of the converging wall 0 to seal the chamber C at will and thus prevent the flow of pressure fluid from the chamber through the outlet opening F. The ejector action of the streams of air and fuel create an area of low pressure within the concavity a' thereby assisting in the diffusion of spray from the fuel nozzle H.
In practice the fuel flowing through the conduit K and the nozzle H under pressure issues from the port J and is projected as spray through the outlet opening F. With the valve P adjusted so that an annular passage X of suitable area may exist between the rim k of the valve and the adjacent wall 0 to assure an adequate amount of pressure fluid for oxygenizing the fuel, such pressure fluid will, due to the shape of the wall 0 and the curvature of the rim is, flow through the outlet opening F in the form of a hollow converging jet.
With the passage X and the port J in coaxial relationship the point of convergence of the air jet is substantially coincident with the axis of the fuel projected from the nozzle H and lies exteriorly of the casing A. Although the hollow jet of air issuing from the passage X encircles the fuel flowing from the port J there is no ,free commingling of fuel and pressure fluid within the casing A. The process of mixing of these elements takes place outside of the burner as does also that of thoroughly atomizing the fuel due to the cross currents of the pressure fluid through the fuel stream, thus assuring a readily combustible mixture.
Whenever it is desired to vary the quantitative relation of pressure fluid and fuel the valve P may be readily adjusted by means of the screw Y, either to increase or decrease the width of the annular passage X. By adjusting the valve P in this manner the conoid jet of pressure fluid directed into the fuel will, of course, be either elongated or shortened but, irrespective of its length, the vertex of such jet will be directed into the fuel stream.
In order to discontinue the operation of the burner the screw Y may be manipulated to seat the rim is of the valve P against the wall 0. In this way the flow of pressure fluid from the chamber C may be cut off. At the same time the valve P may be closed to cut off the flow of fuel from the nozzle H. With the valve P closed any fuel, such as oil, which may leak or dribble from the port J will merely flow along the wall of the recess 7' and through the outlet opening F to the exterior of the burner, thus assuring against leakage of fuel into the chamber C and the possible formationof a combustible mixture within the casing.
We claim:
A fuel burner comprising a casing having a chamber, a converging wall on the casing having an outlet opening, a fuel nozzle afiixed at one end to the casing and extending longitudinally into the chamber, a sleeve slidable upon the fuel nozzle and in fluid tight engagement therewith, guide ribs upon the inner side of the casing wall, bearing members slidable upon said guide ribs and affixed in spaced relationship to the sleeve, a valve member on the sleeve adapted to coact with the outlet opening of the casing, and means acting upon one of the bearing members to control the pressure fluid outlet by movement of the valve carrying sleeve.
JOSEPH M. WEIL. LEVI WILSON.
US548846A 1931-07-06 1931-07-06 Fuel burner Expired - Lifetime US1921059A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US548846A US1921059A (en) 1931-07-06 1931-07-06 Fuel burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US548846A US1921059A (en) 1931-07-06 1931-07-06 Fuel burner

Publications (1)

Publication Number Publication Date
US1921059A true US1921059A (en) 1933-08-08

Family

ID=24190624

Family Applications (1)

Application Number Title Priority Date Filing Date
US548846A Expired - Lifetime US1921059A (en) 1931-07-06 1931-07-06 Fuel burner

Country Status (1)

Country Link
US (1) US1921059A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5507573A (en) * 1991-04-05 1996-04-16 Hiorth; Hans Method and a means for continuous, static mixing of thin layers
US20110197588A1 (en) * 2010-02-12 2011-08-18 General Electric Company Fuel Injector Nozzle
US20110197589A1 (en) * 2010-02-12 2011-08-18 General Electric Company Fuel Injector Nozzle
US20110197594A1 (en) * 2010-02-12 2011-08-18 General Electric Company Method of Controlling a Combustor for a Gas Turbine
US20140000297A1 (en) * 2012-06-29 2014-01-02 Air Liquide Industrial U.S. L.P. Production of Particles from Liquids or Suspensions with Liquid Cryogens

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5507573A (en) * 1991-04-05 1996-04-16 Hiorth; Hans Method and a means for continuous, static mixing of thin layers
US20110197588A1 (en) * 2010-02-12 2011-08-18 General Electric Company Fuel Injector Nozzle
US20110197589A1 (en) * 2010-02-12 2011-08-18 General Electric Company Fuel Injector Nozzle
US20110197594A1 (en) * 2010-02-12 2011-08-18 General Electric Company Method of Controlling a Combustor for a Gas Turbine
US8468834B2 (en) 2010-02-12 2013-06-25 General Electric Company Fuel injector nozzle
US8555648B2 (en) * 2010-02-12 2013-10-15 General Electric Company Fuel injector nozzle
US8584467B2 (en) 2010-02-12 2013-11-19 General Electric Company Method of controlling a combustor for a gas turbine
US20140000297A1 (en) * 2012-06-29 2014-01-02 Air Liquide Industrial U.S. L.P. Production of Particles from Liquids or Suspensions with Liquid Cryogens

Similar Documents

Publication Publication Date Title
US2120387A (en) Device for burning atomized liquid fuel
US2254123A (en) Oil burner
US1921059A (en) Fuel burner
US1396086A (en) Fuel-oil burner
US2212052A (en) Oil burner
US2047570A (en) Fuel burner
US1474867A (en) Hydrocarbon burner
US2174695A (en) Oil burner
US1712326A (en) Burner
US2660230A (en) Oil burner
US1713259A (en) Apparatus for atomizing and spraying
US1874848A (en) Atomizing oil burner
US1938852A (en) Burner
US1098429A (en) Oil-burner.
US1686213A (en) Liquid-fuel burner
US1063913A (en) Oil-burner.
US1563246A (en) Liquid-fuel burner or atomizer
US1493584A (en) Oil burner
US2667384A (en) Oil burner
US2193270A (en) Combination atomizer and mixer
US1781785A (en) Gas burner
US1592865A (en) Vacuum-feed oil burner
US1643967A (en) Low-pressure oil burner
US1581759A (en) Nebulizer
US1992851A (en) Atomizing device