US2156121A - Burner - Google Patents

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US2156121A
US2156121A US135426A US13542637A US2156121A US 2156121 A US2156121 A US 2156121A US 135426 A US135426 A US 135426A US 13542637 A US13542637 A US 13542637A US 2156121 A US2156121 A US 2156121A
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sleeve
cup
air
tube
burner
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US135426A
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James N Macrae
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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

  • a further object of the invention is that of constructing a burner in which the air and fuel may be more efficiently mixed than has heretofore been possible, and in which moreover the control and adjustment of this mixture will present no particular problem.
  • a further object is that of furnishing a unit of this type which will embody relatively few parts,
  • FIG. 2 is a transverse sectional view taken along the broken line 2-2 and in the direction of the arrows of Fig. 1;
  • Fig. 3 is a view similar to Fig. 1, but showing a slightly different form of construction
  • Figs. 4 and 5 are transverse sectional views taken along the lines 4-4 and 55 respectively,
  • Fig. 6 is a somewhat schematic partly sectional 10 view showing a modified form of burner constructed in accordance with the teachings of the present invention.
  • reference numeral l0 indicates a tube formed of any desired material such as 15 brass, and which has adjacent its forward end a socket II to receive a nozzle (not shown).
  • the rear end of the tube may have its bore connected to a pipe l2 through which fuel is fed toward the nozzle.
  • cup element l3 there is mounted upon the tube and adjacent the nozzle end of the same a cup element l3 having an outstanding portion M in the form of a truncated cone adjacent its edge and which is formed with slots l5 preferably extending at a tangent to the edge of tube II].
  • the method of attaching the cup i3 to the tube is relatively immaterial.
  • a set screw l6 may be used to lock the parts against movement, it being understood that the cup member is normally not subject to adjustment length- 30 wise of the tube.
  • the base of the cup may be formed with a series of openings H as well as two larger openings through which electrodes i8 may extend the latter being maintained against movement by a bracket I9. 35
  • Tube l0 and cup l3 are positioned within a sleeve 20, the latter preferably having its forward edge inclined as at 2! to provide a reduced end portion against the inner face of which the edge of member 13 may be abutted.
  • Sleeve 20- 40 may be supported adjacent its rear or inner end by the housing 22 which includes a duct 23 connected to a suitable blower or air compresser (not shown). It is also to be understood that while duct 23 in these views as well as in subse- 4 quent views, extends to one side of the center of sleeve 20, this duct or its functional equivalent might be positioned as desired, it being the primary purpose of this unit to supply air at high velocity to the interior of sleeve 20.
  • casing 22 is for ed with an opening through which tube 10 extends and that while the latter is normally secured against movement with respect to the same, as for example by a set screw 24, adjustment is possible and intended.
  • any desired mechanism normally maintaining a locked condition of the parts, but allowing for adjustment of the same, could be utilized. Under the conditions just described, the operator would simply release-bolt 24 and retract the tube It), cup l3, and associated parts within the bore of sleeve 20.
  • Figs. 3, 4 and 5 Substantially the same construction as that aforedescribed occurs in Figs. 3, 4 and 5, in which the same reference numerals have been used to identify the heretofore referred to parts.
  • two factors are additionally present in these views, either one or both of which may be employed if the construction shown in Figs. 1 and 2 wouldfor some reason-not suffice.
  • the outer end of sleeve 20 may be inwardly extended or tapered as at 25 to functionally correspond to flange 2
  • this inwardly extending portion is formed with a plurality of spirally curved or tapered ribs or vanes 26.
  • the inner portion, of these vanes define in aggregate an annular space of constant radius and corresponding substantially to the maximum diameter of cup member l3.
  • the latter has sliding contact with these edges so that it may ride along toward and away from the outer end of sleeve 20.
  • the air adjustment desired is again achieved adjacent the nozzle and not, for example, at the In such flow it will, of course, be given a outlet or intake end of the blower or fan, or by changing the size of the impeller associated with the latter.
  • the cone or cup member I3 is shifted to provide a greater or lesser space between the inner surface of member 25 and the cup or cone; a greater or lesser volume of air passes through this space.
  • the second factor present in this latter group .of figures is embraced within the casing connected to the rear end of sleeve 20.
  • This may include a forward section 21 and a cover plate 29.
  • This forward section carries a series of spirally extending vanes 28.
  • , to this casing assembly may be ofi center as illustrated or otherwise disposed.
  • air will flow around the casing and be distributed between vanes 28 so that as it enters sleeve 20 it will move in a spiral path. This path may again coincide to that imparted to it by slots I5 or vanes 26.
  • any desired path of travel may be imparted to the air, according to the curvature and disposition of the vanes.
  • FIG. 6 discloses the unit comprising the outer cup member I3 and its associated parts as a replacement structure. In any event, again in this type of apparatus the volume of air is controlled adjacent the burner tip or nozzle.
  • a burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, a cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis of said tube and sleeve, the discharge end of said sleeve tially equal to the greatest diameter of the outwardly flared portion, said cup being shiftable toward the reduced end of said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiitable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, and a spray nozzle on said
  • a burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, 9. cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis oi said tube and sleeve, the discharge end 01' said sleeve being reduced and having an opening substantially equal to the greatest diameter of the outwardly flared portion, said cup being shittable toward the reduced end 01' said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiftable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, a spray
  • a burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, a cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis of said tube and sleeve, the discharge and of said sleeve being reduced and having an opening substantially equal to the greatest diameter of the outwardly flared portion, said cup being shiftable toward the reduced end of said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiitable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, a spray nozzle on

Description

A ril 25, 1939. J. N. MACRAE BURNER Filed April 7, 1937 2 Sheets-Sheet l I INVENTOR Jami-5 11. Mac/me ATTORNEYS April 25, 1939- I J. N. MACRAE BURNER Filed April 7, 1937 2 Sheets-Sheet 2 INVENTOR Jami; 1111mm MT 1% I Ka w- Sm'wo C ATTORNEYS Patented Apr. 25, 1939 UNITED STATES PATENT OFFICE 3 Claims.
or combustion apparatus and in its more specific aspects aims to provide a functionally and structurally improved oil burner, capable of use in association with virtually any type of heat exchange apparatus.
It is well appreciated by those skilled in the industry that considerable difficulty has been experienced in providing a burner which might be utilized to efliciently burn different quantities of oil and in which such difference is over a wide range. In other words, it has been perfectly feasible to produce a more or less satisfactory apparatus which would operate to burn from, for
example, one and one-half to three gallons of oil per hour, or from three and one-half to five gallons per hour. However, when one has attempted, in a single apparatus, to burn, for example, one and one-half gallons per hour, or five or six gallons per hour, it has been found necessary, in effect, to reconstruct the unit, or else to be penalized by improper combustion with all the difliculties which naturally ensue therefrom It is an object of the present invention to furnish a burner with which there may be associated, for example, a one and one-half or six gallon per hour nozzle, and which will efficiently burn oil over this entire range, or in fact beyond the same. Thus, a more or less universal type of apparatus is furnished which will cover virtually any condition arising in varying types and sizes of installation.
, A further object of the invention is that of constructing a burner in which the air and fuel may be more efficiently mixed than has heretofore been possible, and in which moreover the control and adjustment of this mixture will present no particular problem.
A further object is that of furnishing a unit of this type which will embody relatively few parts,
each individually simple and rugged in construction and capable of operating over long periods of time with freedom from all difliculties.
Another object is that of constructing an assembly capable of ready association with burners as heretofore furnished, so that the operation of such burners may be improved. It is to be understood, however, that preferably in accordance This invention relates to an improved burner Fig. 2 is a transverse sectional view taken along the broken line 2-2 and in the direction of the arrows of Fig. 1;
Fig. 3 is a view similar to Fig. 1, but showing a slightly different form of construction;
Figs. 4 and 5 are transverse sectional views taken along the lines 4-4 and 55 respectively,
and in the direction of the arrows indicated in Fig. 3, and
Fig. 6 is a somewhat schematic partly sectional 10 view showing a modified form of burner constructed in accordance with the teachings of the present invention.
In these views, reference numeral l0 indicates a tube formed of any desired material such as 15 brass, and which has adjacent its forward end a socket II to receive a nozzle (not shown). The rear end of the tube may have its bore connected to a pipe l2 through which fuel is fed toward the nozzle. Moreover, there is mounted upon the tube and adjacent the nozzle end of the same a cup element l3 having an outstanding portion M in the form of a truncated cone adjacent its edge and which is formed with slots l5 preferably extending at a tangent to the edge of tube II].
The method of attaching the cup i3 to the tube is relatively immaterial. For example, a set screw l6 may be used to lock the parts against movement, it being understood that the cup member is normally not subject to adjustment length- 30 wise of the tube. The base of the cup may be formed with a series of openings H as well as two larger openings through which electrodes i8 may extend the latter being maintained against movement by a bracket I9. 35
Tube l0 and cup l3 are positioned within a sleeve 20, the latter preferably having its forward edge inclined as at 2! to provide a reduced end portion against the inner face of which the edge of member 13 may be abutted. Sleeve 20- 40 may be supported adjacent its rear or inner end by the housing 22 which includes a duct 23 connected to a suitable blower or air compresser (not shown). It is also to be understood that while duct 23 in these views as well as in subse- 4 quent views, extends to one side of the center of sleeve 20, this duct or its functional equivalent might be positioned as desired, it being the primary purpose of this unit to supply air at high velocity to the interior of sleeve 20.
With air so supplied, it is obvious that it will be caused to flow toward the outer end of sleeve 20 adjacent which it will be compressed by the inturned end portion 2|. If cup member I3 is in contact with such portion-as shown in Fig.
10 amount of air flowing in this manner should preferably be relatively insignificant and serve primarily merely for the purpose of maintaining the nozzle, electrodes and associated parts at a comparatively low temperature. A setting of the parts such as noted may be ideal for a given installation, but we may now assume that another installation is in contemplation and that such new installation requires a larger nozzle or has a combustion chamber presenting co ditions such that a proper mixture would not, u der the given circumstances, be presented.
It is to be observed that casing 22 is for ed with an opening through which tube 10 extends and that while the latter is normally secured against movement with respect to the same, as for example by a set screw 24, adjustment is possible and intended. Of course, any desired mechanism normally maintaining a locked condition of the parts, but allowing for adjustment of the same, could be utilized. Under the conditions just described, the operator would simply release-bolt 24 and retract the tube It), cup l3, and associated parts within the bore of sleeve 20. Immediately upon the edge of the cone or cup l3 being spaced from the inner surface of flange 2|, it is obvious that air, in addition to flowing through openings l1 and slots l5, will begin to flow between the edge of portion M of the cup and the inner surface of the inturned portion 2!. It is, of course, to be understood 40 that an adjustment such as the foregoing is resorted to if the character of the mix is undesirable, or if it becomes necessary to replace the nozzle in socket II by a larger nozzle. Usually where a smaller nozzle is substituted, a reverse I 45 adjustment of the parts is resorted to. In any event, however, the fan or blower (not shown) under all circumstances continues to operate for example at a substantially constant speed and without change of its impeller; the entire air adjustment occurring adjacent the nozzle.
Substantially the same construction as that aforedescribed occurs in Figs. 3, 4 and 5, in which the same reference numerals have been used to identify the heretofore referred to parts. However, two factors are additionally present in these views, either one or both of which may be employed if the construction shown in Figs. 1 and 2 wouldfor some reason-not suffice. Thus, it is primarily to be observed that the outer end of sleeve 20 may be inwardly extended or tapered as at 25 to functionally correspond to flange 2|. In addition, however, this inwardly extending portion is formed with a plurality of spirally curved or tapered ribs or vanes 26. Preferably, the inner portion, of these vanes define in aggregate an annular space of constant radius and corresponding substantially to the maximum diameter of cup member l3. The latter has sliding contact with these edges so that it may ride along toward and away from the outer end of sleeve 20. It is apparent by this construction that the air adjustment desired is again achieved adjacent the nozzle and not, for example, at the In such flow it will, of course, be given a outlet or intake end of the blower or fan, or by changing the size of the impeller associated with the latter. However, as the cone or cup member I3 is shifted to provide a greater or lesser space between the inner surface of member 25 and the cup or cone; a greater or lesser volume of air passes through this space. All such air in flowing in contact with the vanes, will be given a twisting or spiral motion which will complement the flow of air passing through slots or openings [5, resulting in an axial twist being imparted to the column of air flowing from sleeve 20. It is preferred that, as shown, the twisting action imparted to the columns of air flowing through the slots of the cup member or between the edge of the latter and the adjacent tube surface coincide. This need not necessarily be the case and, of course, if desired, the parts might be modified to such an extent that the two layers of air would be given reverse rotations resulting in a condition of extreme turbulence. -While this might, in certain installations, be desirable, I have found that under ordinary circumstances such a construction is not conducive to a proper combustion and desirable flame.
The second factor present in this latter group .of figures is embraced within the casing connected to the rear end of sleeve 20. This may include a forward section 21 and a cover plate 29. This forward section carries a series of spirally extending vanes 28. The inlet 3|, to this casing assembly may be ofi center as illustrated or otherwise disposed. In any event, air will flow around the casing and be distributed between vanes 28 so that as it enters sleeve 20 it will move in a spiral path. This path may again coincide to that imparted to it by slots I5 or vanes 26. As heretofore brought out, however, any desired path of travel may be imparted to the air, according to the curvature and disposition of the vanes.
Finally, referring to Fig. 6, it will be observed that substantially the same construction as heretofore illustrated in Figs. 1 to 3 is employed with the exception that a casing has been indicated at 32, which casing may form the housing for the fan, it being understood that the sleeve 20 is directly connected thereto. This follows more commonly accepted practice, it being appreciated that Fig. 6 discloses the unit comprising the outer cup member I3 and its associated parts as a replacement structure. In any event, again in this type of apparatus the volume of air is controlled adjacent the burner tip or nozzle.
It is apparent, from the foregoing, that among others, the several objects of the invention as specifically heretofore noted are achieved. It will be appreciated that numerous changes in construction and re-arrangement of the parts might be resorted to without departing from the spirit of the invention as defined by the claims.
Having described my invention, what I claim as new and desire to secure by Letters Patent is:
l. A burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, a cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis of said tube and sleeve, the discharge end of said sleeve tially equal to the greatest diameter of the outwardly flared portion, said cup being shiftable toward the reduced end of said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiitable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, and a spray nozzle on said tube adjacent the outwardly flared portion of said cup.
2. A burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, 9. cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis oi said tube and sleeve, the discharge end 01' said sleeve being reduced and having an opening substantially equal to the greatest diameter of the outwardly flared portion, said cup being shittable toward the reduced end 01' said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiftable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, a spray nozzle on said tube adjacent the outwardly flared portion of said cup, a housing connected to the other end of said sleeve, and a duct coupled to said housing and extending at a tangent to the same, said housing having a diameter greater than that of said sleeve whereby air enters said housing through said duct and rotates through the housing and said sleeve in its passage toward said cup.
3. A burner including a sleeve to be coupled to a source of air supply, an oil discharge tube extending within said sleeve, a cup encircling said tube and adjacent the discharge end of the latter, the base of said cup being formed with openings for the passage of air from said sleeve to the space defined by said cup, said cup having an outwardly flared portion at its open end, said portion being formed with slots extending at a tangent to a circle concentric with the axis of said tube and sleeve, the discharge and of said sleeve being reduced and having an opening substantially equal to the greatest diameter of the outwardly flared portion, said cup being shiftable toward the reduced end of said sleeve whereby to force substantially all the air flowing through said sleeve to traverse said slots and shiitable away from the sleeve end to permit increasing amounts of air to flow between the outer edge of said flared portion and the inner surface of the reduced end of said sleeve, a spray nozzle on said tube adjacent the outwardly flared portion of said cup, and ribs extending inwardly from the inner face of said sleeve and adjacent the discharge end or the latter, said ribs being spaced to receive the outwardly flared portion of said cup and the edges of such portion having sliding engagement with the edges of said ribs.
JAMES N. MACRAE.
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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472720A (en) * 1944-12-19 1949-06-07 Nagel Theodore Method of burning oil
US2473347A (en) * 1943-04-08 1949-06-14 Cleaver Brooks Co Air directing means in gun type burners
US2500344A (en) * 1946-06-03 1950-03-14 Harvey Whipple Inc Oil burner apparatus
US2505337A (en) * 1946-09-04 1950-04-25 Monarch Mfg Works Inc Counterrotational air flow gun type oil burner
US2516063A (en) * 1948-08-19 1950-07-18 Gilbert & Barker Mfg Co Pressure atomizing oil burner with a built-in combustion chamber
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2527503A (en) * 1949-02-12 1950-10-24 Harvey Whipple Inc Burner head for gun-type oil burners
US2530019A (en) * 1944-11-11 1950-11-14 Elliott Co Combustion chamber with side air entrance and hollow ignition cone
US2531027A (en) * 1947-12-17 1950-11-21 Monarch Mfg Works Inc Oil burner
US2539165A (en) * 1946-11-30 1951-01-23 Cyclotherm Corp Dispersible fuel burner having a reverse gas flow flame stabilizer
US2553520A (en) * 1947-04-15 1951-05-15 York Shipley Inc Burner nozzle pipe assembly
US2565879A (en) * 1947-03-28 1951-08-28 Persiro Mfg Corp Burner for combustion chambers
US2661199A (en) * 1948-10-12 1953-12-01 Curtiss Wright Corp Burner for liquid fuel
US2706150A (en) * 1949-01-14 1955-04-12 Power Jets Res & Dev Ltd Gas producer for use with a turbine power plant
US2717638A (en) * 1949-09-14 1955-09-13 William B Perdue Oil burner
US2753929A (en) * 1951-12-27 1956-07-10 Silent Flame Mfg Co Inc Oil burner
US2765842A (en) * 1952-03-05 1956-10-09 Preferred Utilities Mfg Corp Hydrocarbon burner head
US2821246A (en) * 1951-05-14 1958-01-28 Synchronous Flame Inc Combination oil-gas burner and gas burner adapter for gun-type oil burner
US3033278A (en) * 1958-12-22 1962-05-08 Gulf Research Development Co Air directing apparatus
US3115924A (en) * 1960-02-03 1963-12-31 Selas Corp Of America Burner
US3126939A (en) * 1964-03-31 de lancey
US3129748A (en) * 1961-06-15 1964-04-21 Master Cons Inc Oil burner
US3285724A (en) * 1962-12-05 1966-11-15 Johns Manville Apparatus for producing glass fibers
US4484887A (en) * 1979-11-29 1984-11-27 Ab Allterm Device in burners

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126939A (en) * 1964-03-31 de lancey
US2473347A (en) * 1943-04-08 1949-06-14 Cleaver Brooks Co Air directing means in gun type burners
US2530019A (en) * 1944-11-11 1950-11-14 Elliott Co Combustion chamber with side air entrance and hollow ignition cone
US2472720A (en) * 1944-12-19 1949-06-07 Nagel Theodore Method of burning oil
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2500344A (en) * 1946-06-03 1950-03-14 Harvey Whipple Inc Oil burner apparatus
US2505337A (en) * 1946-09-04 1950-04-25 Monarch Mfg Works Inc Counterrotational air flow gun type oil burner
US2539165A (en) * 1946-11-30 1951-01-23 Cyclotherm Corp Dispersible fuel burner having a reverse gas flow flame stabilizer
US2565879A (en) * 1947-03-28 1951-08-28 Persiro Mfg Corp Burner for combustion chambers
US2553520A (en) * 1947-04-15 1951-05-15 York Shipley Inc Burner nozzle pipe assembly
US2531027A (en) * 1947-12-17 1950-11-21 Monarch Mfg Works Inc Oil burner
US2516063A (en) * 1948-08-19 1950-07-18 Gilbert & Barker Mfg Co Pressure atomizing oil burner with a built-in combustion chamber
US2661199A (en) * 1948-10-12 1953-12-01 Curtiss Wright Corp Burner for liquid fuel
US2706150A (en) * 1949-01-14 1955-04-12 Power Jets Res & Dev Ltd Gas producer for use with a turbine power plant
US2527503A (en) * 1949-02-12 1950-10-24 Harvey Whipple Inc Burner head for gun-type oil burners
US2717638A (en) * 1949-09-14 1955-09-13 William B Perdue Oil burner
US2821246A (en) * 1951-05-14 1958-01-28 Synchronous Flame Inc Combination oil-gas burner and gas burner adapter for gun-type oil burner
US2753929A (en) * 1951-12-27 1956-07-10 Silent Flame Mfg Co Inc Oil burner
US2765842A (en) * 1952-03-05 1956-10-09 Preferred Utilities Mfg Corp Hydrocarbon burner head
US3033278A (en) * 1958-12-22 1962-05-08 Gulf Research Development Co Air directing apparatus
US3115924A (en) * 1960-02-03 1963-12-31 Selas Corp Of America Burner
US3129748A (en) * 1961-06-15 1964-04-21 Master Cons Inc Oil burner
US3285724A (en) * 1962-12-05 1966-11-15 Johns Manville Apparatus for producing glass fibers
US4484887A (en) * 1979-11-29 1984-11-27 Ab Allterm Device in burners

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