US3319692A - Oil burner - Google Patents
Oil burner Download PDFInfo
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- US3319692A US3319692A US460054A US46005465A US3319692A US 3319692 A US3319692 A US 3319692A US 460054 A US460054 A US 460054A US 46005465 A US46005465 A US 46005465A US 3319692 A US3319692 A US 3319692A
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- shroud
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S239/00—Fluid sprinkling, spraying, and diffusing
- Y10S239/07—Coanda
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- 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
I. REBA ET AL May 16, 1967 OIL BURNER Filed June 1,. 1965 2 Sheets-Sheet 1 INVENTORS WWI 76 P154 TORNEYS I. REBA ET AL OIL BURNER 2 Sheets-Sheet 2 Filed June 1. 1965 s M R 8 W w R m 2 M 0 A [firm z 4 M7 4/5 w M w p 2 N; Hf M 7 f C 4 0 0 Z m; m M 6 V Q 0 0% N05 2 Z V m? w a a e a z 4 5 z 2 M m I 2 Q s Q MM MW w \N 0 m 1 Wm 0% WWW 4 \.A\ 6 v! C w 7 0 0 0 0 a w a 6 4 3 2 I X 2 Q? @WNNQ LQR U Q 2 United States Patent 3,319,692 OIL BURNER Imants Reba, Chicago, IlL, and Paul W. Cooper, Albuquerque, N. Mex., assignors to HT Research Institute, Chicago, Ill., a corporation of Illinois Filed June 1, 1965, Ser. No. 460,054 8 Claims. (Cl. 158-11) The present invention relates to oil burner devices and is, more particularly, concerned with the provision of a simple, compact burner unit capable of highly eflicient use in homes, or the like. The burner of the present invention is constructed primarily for the non-commercial, relatively low cost heating installation while at the same time it is designed to produce blue-flame operation with oil of the household grade, commonly known as No. 2 Heating Oil, and at low air pressures.
As those familiar with the art of oil burner construction are aware, much development work has been undertaken in this field in the last twenty years. With such development work, substantially increased performance has been achieved. However, in spite of the forward strides of the heating industry, important deficiencies have existed in heating systems of the relatively inexpensive type designed to operate on residential type heating fuels. More particularly, a truly satisfactory low cost-low pressure burner capable of combustion with a blue or non-luminous flame has not heretofore been successfully achieved. In burner systems utilizing heating oil, the combustion processes have been carried on in the presence of a yellow flame, the best of which has been essentially a clean yellow flame, while the worst has been a yellow flame including substantial smoke propagation. The desirability of providing a blue or non-luminous flame has been generally recognized but the elimination of the smoke and yellow color accompanying prior art devices has eluded those working in the field.
In accordance with the present invention, an oil burner is provided in which smoke has been substantially completely eliminated and the burner operates with an ultimate degree of cleanliness, in the presence of a blue or nonluminous flame. This has been achieved without in any way sacrificing over-all safety of the burner, since operation is intended to be, and is readily accomplished, in a condition of excess combustion air so that carbon monoxide (CO) is eliminated from the combustion gases.
In accordance with the present invention, the products of combustion are recirculated in large proportion in the burner system. By providing a novel primary air flow system and simple vaneless, air flow control device, a very high rate of recirculation of the products of combustion is achieved with a highly efficient blue-flame burning condition.
In accordance with the present invention, extremely simple structural components are employed. The burner comprises a generally cylindrical outer housing open at the downstream end to provide flue gas exhaust. Air and oil are introduced at the upstream end and a cylindrical intermediate diameter body is positioned within the outer cylindrical housing providing an annular recirculation path about its outer peripheral surface and a combustion zone within its internally facing surface. Air is introduced axially into the housing but is radially ejected upstream of and immediately adjacent to a flow directing body comprising, preferably, a solid of revolution from providing a surface generally curved, or relieved in the downstream direction. This surface causes a radially outwardly directed stream of air to deflect toward and adjacent to the solid body under the phenomenon generally known as the Coanda effect. As a result of the phenomenon, no upstream air flow deflecting vanes are required. Instead, as a result of the simple configuration, air flows ice downstream along the surface of revolution and acts as a pump to entrain a relatively high percentage of recirculated products of combustion. These products, along with primary air, are directed past the solid of revolution into a mixing chamber where they are mixed with atomized oil from a high pressure oil nozzle. The intermixed oil, air and recirculated combustion products pass into the combustion zone where, upon ignition, they are burned in an efiicient manner. A portion of the combustion gases are, preferably after complete combustion has occurred therein, recirculated, in the manner above described, thereby providing a particularly efficient combustion system operating without any trace of yellow in the flame.
It is, accordingly, an object of the present invention to provide an improved burner for the combustion of household heating oil.
Another object of the present invention is to provide a simple generally cylindrical, oil burner capable of operation at blue or non-luminous flame conditions in the presence of an excess of air.
Still another object of the present invention is to provide a simple, highly eflicient burner construction for the combustion of household fuel, and which has no vanes or moving burner components.
A feature of the invention resides in the provision of a Coanda flow control mechanism for the control of air flow through the burner system.
Another feature of the invention resides in the utilization of a simple, yet highly eflicient, recirculation system for recirculating a substantial portion of combustion gases within the combustion area of the burner.
Another feature of the invention resides in the provision of a separation aperture between the fuel and air mixing chamber and the combustion zone providing a pressure differential operative to enhance the recirculation of the products of combustion into substantially direct contact with incoming fuel and air.
Still other and further objects and features of the present invention will at once become apparent to those skilled in the art from a consideration of the attached sheets of drawings wherein one embodiment of the invention is shown by way of illustration only, and wherein:
FIGURE 1 is a generally cross-sectional view, in schematic form, of a burner constructed in accordance with the provisions of the present invention;
FIGURE 2 is a cross-sectional View taken along the line Iii-11 of FIGURE 1;
FIGURE 3 is a cross-sectional view taken along the line III-J11 of FIGURE 1; and
FIGURE 4 is a chart illustrating certain fuel-air relationships discovered to be important in the successful propagation of a blue-flame oil burner.
As shown on the drawings:
We have discovered as a result of extensive experimentation, including operation of full-size oil burner configurations, that oil may be burned with suflicient efficiency to provide a blue-flame in the presence of excess air. A preferred embodiment of our construction may be seen from a consideration of FIGURES 1 through 3 where our improved burner is shown in a somewhat schematic form.
As maybe seen from FIGURES 1 through 3, the burner of the present invention comprises an outer housing generally indicated at 10, constructed in a generally cylindrical form. Closing off the downstream end of the main housing 10, is an end .plate 11 having an exhaust aperture 12 therein. Oil is introduced under relatively high pressure by Way of a conduit 13 leading to a conventional high pressure atomizing nozzle 13a. Primary air for combustion purposes is introduced into the cylindrical housing 1'0 by way of a generally cylindrical conduit 14 which enters the housing by way of an opening in the upstream closure wall 16. Primary air under a relatively low fan induced pressure of two inches of water has been found satisfactory and may be supplied from any conventional low pressure fan or blower, not illustrated.
Within the central area of the housing 10 a generally cylindrical shroud 17 is rigidly secured. The shroud 17 is divided into two generally cylindrical chambers, indicated at 18 and 19 and comprising, respectively, a mixing chamber and a combustion chamber separated by a separation plate 20 having a separation orifice 21 therein. The shroud 17 may be fixedly positioned within the outer chamber 10 by any conventional means, such as for example a plurality of generally radial spider elements 22 providing a recirculation passageway 27. Air entering the housing by way of conduit 14 is radially directed outwardly in the direction indicated by the arrows 23, leaving an annular slit 24 formed by the upstream surface of a body 25 having a curved surface of revolution 25a, and the downstream or trailing edge 14a of the inlet conduit 14. The body 25 is rigidly secured in place within the mixing zone 18 by any convenient construction. For example, in the embodiment illustrated, the solid of revolution 25 is rigidly mounted directly on, and to, the fuel oil inlet conduit 13. It will be understood, however, that the body of revolution 25 may be supported within the mixing zone by securing it directly to the shroud 17 by a spider, in the same manner as indicated at 22 with respect to the shroud 17.
As shown, air entering the mixing zone by way of the conduit 14 passes through slit 24 radially outwardly in the direction of the arrow 23. The presence of the curved upstream surface of the solid of revolution 25 causes, as a result of the known Coanda effect, an attachment of the air stream to the surface 25a with the resultant flow of the air outwardly along the surface 25a and downstream to the mixing zone. It has been found as a result of our experimentation that this tendency of the air toward attachment to the surface 2.5a causes a pumping action or entrainment of air or other gaseous material located in the area 26 immediately upstream of the curved body 25. In fact, the entrainment provides an efiicient pump for causing forced draft recirculation of products of combustion by way of the passageway 27. This entrainment is improved significantly by providing a sharp edge 14a 0n conduit 14 in the manner shown at 14b.
Due to the positioning of the separation plate 20 and the mixing of primary air with the atomized fuel immediately upstream of the separation plate 20, ignition of the combustible mixture may satisfactorily be accomplished by an electrode 30 positioned in the combustion chamber 19 or immediately upstream of the ignition orifice 21. This provides for the burning process in chamber 19, and, as will be more fully set forth below, the combustion chamber length is preferably sufiiciently great to provide complete combustion of the fuel prior to movement of the combustion gases downstream and out of the combustion chamber. As a result of this relationship combustion gases, that are recirculated upstream by way of the annular passageway 27 back into the shroud at area 26 for entrainment with the primary air passing about the flow body 25, are substantially completely burned prior to movement through passage 27 and addition to the primary air. It has been found that for the purposes of providing a blue or nonluminous flame condition, substantially complete combustion of the recirculated gases is desirable.
Operation of the system hereinabove broadly disclosed is based upon discovered relationships relative to the recirculation of combustion gases. As may be clearly seen from a consideration of the chart, FIGURE 4, various conditions of excess air and percentage of recirculation of combustion products provide significantly different flame characteristics. As may be seen, at levels of burner operation providing greater than 50% recirculation of combustion products and moderate amounts of excess air, the flame propagated is clean, blue or nonluminous, and quiet. It is extremely desirable to provide for such a clean, blue-flame and, accordingly, apparatus capable of satisfying these requirements at reasonable cost provides a major contribution in the burner field. The burner illustrated in applicants FIGURES 1 through 3 fully satisfies these requirements both as to burning characteristics and as to expense.
In further considering the chart, FIGURE 4, it will be observed that percent recirculation identified by R: standard c.f.m. of stoichiometric air The stoichiometric condition, in which no excess air is present, can theoretically produce a clean blue-flame. Although such stoichiometric combustion would be highly desirable from the standpoint of maintaining high unit efficiency, it is considered important to 'provide excess air under substantially all furnace operation conditions to reduce the dangers of carbon monoxide. Accordingly, it is preferred that the system be operated at conditions of excess air. For example, it has been found through operation of a burner constructed in accordance with the present invention, and in the form illustrated in the drawings hereof, operation at approximately 15% excess air with an inlet air pressure of 2.7 inches of water and R=75%, no carbon monoxide appeared at the exhaust and the burner was operating at a substantially smokeless condition with an essentially blue-flame. These results were achieved employing a firing rate of .95 gallon per hour of No. 2 Distillate Fuel Oil with a nozzle temperature of 300 F. and a temperature in the annular flow recycle path 27 of approximately 1000 F. Further, at stoichiometric conditions and with a blue-flame only 10 to 20 ppm. CO was present. These characteristics coincided with the expectations indicated from the chart of FIGURE 4 and were accomplished with a burner constructed in accordance with the structure of FIGURES 1 through 3 and having the following dimensions:
Length of housing 10 24". Length of shroud 17 18". Spacing between shroud 17 and housing wall16 2".
solid spray nozzle spaced 1 /8" upstream of separation plate 20.
Length of shroud downstream of separation wall 21 11".
During the experimental work, it became apparent that variations may be made in the shape of the body 25 and the surface 25a thereof, with some effect on entrainment efliciency. However, that addition of axial extension of the flow body after it attains its maximum diameter made no signifiacnt difference in operation. Variations in various of the components will affect operation of the system somewhat and the preferred embodiments of the invention will conform generally to the system equation:
in which the first term defines the geometry of the system, the second term contains the flow parameters and the terms at the right of the equality sign relate to the entrainment ratio. In the formula the terms are defined as follows:
entrainment ratio, standard e.fm. entrained gas standard c.f.m. primary air A =annular area between shroud and inlet air tube 14,
square inches.
It has been found from experimentation that a burner constructed in accordance with the form illustrated in the drawings fully satisfies successful operation under the formula and provides a very high percent of recirculation, necessary to the provision of a blue or non-luminous flame. At the same time, it has been found that operation of the burner is successful at very low primary air inlet pressures. These pressures may be on the order of 2 inches of H 0 which, when compared with the much higher air pressures employed in commercial burner installations, clearly places the burner of the present invention in the category of the inexpensive home oil burner type of apparatus. Accordingly, we have found that calculation of a burner in accordance with the formulae above set forth, permits utilization of an extremely inexpensive design at a cost sufiiciently low to permit its widespread use in ordinary residential operation. Of course, design considerations suggest that a relatively simple construction be employed if possible. Toward this end, the design of a specific installation for any given need suggests that a number of the factors in the formula be considered as predetermined by the economics of commercial manufacture. Thus, in designing a burner along the lines of the burner illustrated in the drawings of the present application, certain areas may be predetermined from presently accepted practice. Thus, by using the chart, FIGURE 4, and employing a fixed predetermined firing rate for the fuel, a fixed air flow rate to provide the percent excess air, the amount of inlet air is calculatable and the fiow rate of the recirculated products may readily be determined. The diameter of the separation orifice is chosen in accordance with present accepted practice for high pressure type oil burners, i.e., between 2.5 and 3.0" for operation in the range of one gallon per hour. The position of the nozzle upstream of the separation orifice is, similarly, determined by a conventional practice and as such, is on the order of slightly over an inch from the separation orifice. The shape of the flow body may be modified somewhat but choice of the generally circular solid of revolution provides a simply calculatable form having very adequate performance. The diameter of the flow body and the diameter of the shroud is readily computed by equating the sum of the recirculation and inlet air flow rates, combined to the estimated flame velocity such that the flame is stabilized within the shroud. As above noted, the
shroud is constructed of sufficient length to encompass substantially complete combustion whereby recirculated gases are essentially completely burned prior to their recirculation. A factor of importance in design consideration, which was determined experimentally, is the fact that the shroud should, for excellent performance, extend at least one inch upstream of the inlet air slit 24. A lesser dimension provides incomplete entrainment while greater length of shroud upstream of the flow body produces substantially no improvement of entrainment. The utilization of a dimension of 1 /2" for this factor has proved very satisfactory in operation.
It will be apparent from the discussion above, that it is extremely important, in the propagation of a blue or nonluminous flame, in connection with low pressure primary air combined with household fuel oil to provide high percentages of recirculated products of combustion. It has been found that the vaneless entrainment established by the structure herein illustrated provides a completely satisfactory burner capable of successfully employing low pressure primary air available from inexpensive home-use type blowers, conventional household fuel oil, and extremely inexpensive construction to provide blue-flame operation. It will be clear to those skilled in the art that the recirculation of combustion gases may be accomplished in manners different from that shown in the embodiment illustrated herein. It is, accordingly, our intention that the present invention be limited solely to that scope set forth in the appended claims.
We claim as our invention:
1. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured Within said housing providing an axially extending passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining therewith to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, means introducing fuel into said shroud downstream of said body for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion at the downstream end of said shroud and an opening in the downstream end of said housing providing for the escape of exhaust gases following combustion.
2. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a fiow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining with the open end of said conduit to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, means introducing fuel into said shroud downstream of said body for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion at the downstream end of said shroud, and an opening in the downstream end of said housing extending beyond the downstream end of said annular passage and providing for the escape of exhaust gases following combustion.
3. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining with the open end of said conduit to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, an annular separating plate providing a separation orifice intermediate the ends of said shroud dividing the shroud into a mixing chamber upstream of a combustion chamber, means introducing fuel into said shroud downstream of said body and upstream of said plate for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion in said combustion chamber and an opening in the downstream end of said housing providing for the escape of exhaust gases following combustion.
4. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermedaite the ends thereof and immediately downstream of the open end of said conduit and combining with the open end of said conduit to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, an annular separating plate providing a separation orifice intermediate the ends of said shroud dividing the shroud into a mixing chamber upstream of a combustion chamber, means introducing fuel into said shroud downstream of said body and upstream of said plate for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion in said combustion chamber and an opening in the downstream end of said housing at a point beyond the downstream end of said annular passage providing for the escape of exhaust gases following combustion while permitting recirculation of part of the prodnets of combustion via said annular passage.
5. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured within said housing providing an axially extending passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining therewith to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, means introducing atomized liquid fuel into said shroud downstream of said body for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion at the downstream end of said shroud and an opening in the downstream end of said housing providing for the escape of exhaust gases following combustion.
6. In combination in a fuel burner, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under ositive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immedaitely downstream of the open end of said conduit and combining with the open end of said conduit to provide an annular radially opening slit for the passage of air from the conduit in a direction radially outwardly adjacent said body, means providing an opening between the interior of said shroud and said passage upstream of said body, the upstream surface of said body being gradually curved in the downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, an annular separating plate providing a separation orifice intermediate the ends of said shroud dividing the shroud into a mixing chamber upstream of a combustion chamber, means introducing atomized liquid fuel into said shroud downstream of said body and upstream of said plate for mixture with air flowing downstream around said body, means for igniting said mixture in said shroud to provide combustion in said combustion chamber and an opening in the downstream end of said housing at a point beyond the downstream end of said annular passage providing for the escape of exhaust gases following combustion while permitting recirculation of part of the products of combustion via said annular passage.
7. In combination in a fuel burner providing blueflame operation, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining with the open end of said conduit to provide an annular radially open slit for the passage of air from said conduit in a direction radially outwardly adjacent said body, said shroud being axially spaced from said means closing said one end of said housing to provide an annular opening between the interior of said shroud and said passage at a point upstream of said body, the upstream surface of said body being gradually curved in a downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, an annular separating plate providing a separation orifice intermediate the ends of said shroud dividing the shroud into a mixing chamber upstream of -a combustion chamber, means introducing atomized liquid fuel into said shroud downstream of said body and upstream of said plate for mixture with air flowing downstream around said body, means for igniting said mixture and said shroud to provide combustion in said combustion chamber, and an opening in the downstream end of said housing at a point beyond the downstream end of said annular passage providing for the escape of exhaust gases following combustion while permitting recirculation of part of the products of combustion via said annular passage.
8. In combination in a fuel burner providing blueflame operation, a generally cylindrical housing, a generally cylindrical shroud fixedly secured concentrically within said housing and spaced therefrom providing an axially extending annular passage between said housing and said shroud, :an axially extending open-ended tubular conduit introducing primary air under positive pressure axially into one end of said cylindrical shroud, means closing said one end of said housing around said conduit, a flow directing body in said shroud intermediate the ends thereof and immediately downstream of the open end of said conduit and combining with the open end of said 10 conduit to provide an annular radially open slit for the passage of air from said conduit in a direction radially outwardly adjacent said body, said shroud being axially spaced from said means closing said one end of said housing to provide an opening between the interior of said shroud and said passage at a point upstream of said body and providing an extension of said shroud a dis tance in excess of one inch upstream of said slit, the upstream surface of said body being gradually curved in a downstream direction whereby air leaving said slit attaches to said surface for deflection downstream in said shroud and for entrainment of gas in said shroud upstream of the body, means introducing atomized liquid fuel into said shroud downstream of said body, for mixture with air flowing around said body, means igniting said mixture, and an opening in the downstream end of the housing at a point beyond the downstream end of said annular passage providing for the escape of exhaust gases following combustion while permitting recirculation of part of the products of combustion via said annular passage.
References Cited by the Examiner UNITED STATES PATENTS 2,056,531 10/ 1936 Morton 1581 2,701,608 2/1955 Johnson l581 2,918,117 12/1959 Griffin 1581 3,174,526 3/1965 Von Linde 1581 X FREDERICK L. MATTESON, JR., Primary Examiner. E. G. FAVORS, Assistant Examiner.
Claims (1)
1. IN COMBINATION IN A FUEL BURNER, A GENERALLY CYLINDRICAL HOUSING, A GENERALLY CYLINDRICAL SHROUD FIXEDLY SECURED WITHIN SAID HOUSING PROVIDING AN AXIALLY EXTENDING PASSAGE BETWEEN SAID HOUSING AND SAID SHROUD, AN AXIALLY EXTENDING OPEN-ENDED TUBULAR CONDUIT INTRODUCING PRIMARY AIR UNDER POSITIVE PRESSURE AXIALLY INTO ONE END OF SAID CYLINDRICAL SHROUD, MEANS CLOSING SAID ONE END OF SAID HOUSING AROUND SAID CONDUIT, A FLOW DIRECTING BODY IN SAID SHROUD INTERMEDIATE THE ENDS THEREOF AND IMMEDIATELY DOWNSTREAM OF THE OPEN END OF SAID CONDUIT AND COMBINING THEREWITH TO PROVIDE AN ANNULAR RADIALLY OPENING SLIT FOR THE PASSAGE OF AIR FROM THE CONDUIT IN A DIRECTION RADIALLY OUTWARDLY ADJACENT SAID BODY, MEANS PROVIDING AN OPENING BETWEEN THE INTERIOR OF SAID SHROUD AND SAID PASSAGE UPSTREAM OF SAID BODY, THE UPSTREAM SURFACE OF SAID BODY BEING GRADUALLY CURVED IN THE DOWNSTREAM DIRECTION WHEREBY AIR LEAVING SAID SLIT ATTACHES TO SAID SURFACE FOR DEFLECTION DOWNSTREAM IN SAID SHROUD AND FOR ENTRAINMENT OF GAS IN SAID SHROUD UPSTREAM OF THE BODY, MEANS INTRODUCING FUEL INTO SAID SHROUD DOWNSTREAM OF SAID BODY FOR MIXTURE WITH AIR FLOWING DOWNSTREAM AROUND SAID BODY, MEANS FOR IGNITING SAID MIXTURE IN SAID SHROUD TO PROVIDE COMBUSTION AT THE DOWNSTREAM END OF SAID SHROUD AND AN OPENING IN THE DOWNSTREAM END OF SAID HOUSING PROVIDING FOR THE ESCAPE OF EXHAUST GASES FOLLOWING COMBUSTION.
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US460054A US3319692A (en) | 1965-06-01 | 1965-06-01 | Oil burner |
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US460054A US3319692A (en) | 1965-06-01 | 1965-06-01 | Oil burner |
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Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3419339A (en) * | 1967-02-08 | 1968-12-31 | Hauck Mfg Co | Inspirator assembly |
US3540821A (en) * | 1968-04-01 | 1970-11-17 | Exxon Research Engineering Co | Flue gas recirculation burner |
US3609073A (en) * | 1968-02-26 | 1971-09-28 | Dickinson S Ltd | Oil burner apparatus |
US3639094A (en) * | 1969-01-30 | 1972-02-01 | Gerard Pierre Marie Joseph Dup | Space-heating burner |
US3744242A (en) * | 1972-01-25 | 1973-07-10 | Gen Motors Corp | Recirculating combustor |
US3786799A (en) * | 1972-02-07 | 1974-01-22 | Cox Mfg Co Inc | Pulse relief damper |
US3799734A (en) * | 1973-05-03 | 1974-03-26 | J Bailey | Combustion device |
US3826083A (en) * | 1973-07-16 | 1974-07-30 | Gen Motors Corp | Recirculating combustion apparatus jet pump |
US3833337A (en) * | 1971-04-29 | 1974-09-03 | British Petroleum Co | Flarestacks |
US3852021A (en) * | 1973-11-05 | 1974-12-03 | Gen Motors Corp | Internal recirculation burner |
US3880354A (en) * | 1971-12-23 | 1975-04-29 | Chemetron Corp | Method and apparatus for controlling heat effect in metal cutting operations |
EP0003000A1 (en) * | 1977-12-23 | 1979-07-11 | Fascione, Pietro | Burner head for a combustion chamber |
US4260367A (en) * | 1978-12-11 | 1981-04-07 | United Technologies Corporation | Fuel nozzle for burner construction |
US4802423A (en) * | 1987-12-01 | 1989-02-07 | Regenerative Environmental Equipment Co. Inc. | Combustion apparatus with auxiliary burning unit for liquid fluids |
EP0985882B1 (en) * | 1998-09-10 | 2003-12-03 | ALSTOM (Switzerland) Ltd | Vibration damping in combustors |
US7410288B1 (en) * | 1998-12-24 | 2008-08-12 | Luminis Pty. Ltd. | Fluid mixing device |
WO2009014654A3 (en) * | 2007-07-20 | 2009-03-05 | Astec Ind | Coal burner assembly |
US20090246719A1 (en) * | 2008-03-28 | 2009-10-01 | Newby John N | Method of operating a furnace |
US20130340404A1 (en) * | 2012-06-22 | 2013-12-26 | General Electric Company | Hot egr driven by turbomachinery |
US20140123632A1 (en) * | 2012-05-25 | 2014-05-08 | Hino Motors, Ltd. | Burner for exhaust purifying device |
WO2015154969A1 (en) * | 2014-04-10 | 2015-10-15 | Sofinter S.P.A. | Burner |
US20170108224A1 (en) * | 2014-04-03 | 2017-04-20 | Siemens Aktiengesellschaft | Burner, gas turbine having such a burner, and fuel nozzle |
US10105676B2 (en) * | 2015-08-06 | 2018-10-23 | Guangdong Hydrogen Energy Science And Technology Co., Ltd | Start-up system for starting reforming hydrogen production device |
US20190093948A1 (en) * | 2016-02-17 | 2019-03-28 | Eisenman Se | Burner unit and device for the temperature control of objects |
US10569619B2 (en) * | 2016-09-15 | 2020-02-25 | Eberspächer Climate Control Systems GmbH & Co. KG | Combustion chamber assembly unit for a fuel-operated vehicle heater |
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US2056531A (en) * | 1933-05-22 | 1936-10-06 | Amco Inc | Process for luminous flame heating |
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Cited By (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3419339A (en) * | 1967-02-08 | 1968-12-31 | Hauck Mfg Co | Inspirator assembly |
US3609073A (en) * | 1968-02-26 | 1971-09-28 | Dickinson S Ltd | Oil burner apparatus |
US3540821A (en) * | 1968-04-01 | 1970-11-17 | Exxon Research Engineering Co | Flue gas recirculation burner |
US3639094A (en) * | 1969-01-30 | 1972-02-01 | Gerard Pierre Marie Joseph Dup | Space-heating burner |
US3833337A (en) * | 1971-04-29 | 1974-09-03 | British Petroleum Co | Flarestacks |
US3880354A (en) * | 1971-12-23 | 1975-04-29 | Chemetron Corp | Method and apparatus for controlling heat effect in metal cutting operations |
US3744242A (en) * | 1972-01-25 | 1973-07-10 | Gen Motors Corp | Recirculating combustor |
US3786799A (en) * | 1972-02-07 | 1974-01-22 | Cox Mfg Co Inc | Pulse relief damper |
US3799734A (en) * | 1973-05-03 | 1974-03-26 | J Bailey | Combustion device |
US3826083A (en) * | 1973-07-16 | 1974-07-30 | Gen Motors Corp | Recirculating combustion apparatus jet pump |
US3852021A (en) * | 1973-11-05 | 1974-12-03 | Gen Motors Corp | Internal recirculation burner |
EP0003000A1 (en) * | 1977-12-23 | 1979-07-11 | Fascione, Pietro | Burner head for a combustion chamber |
US4260367A (en) * | 1978-12-11 | 1981-04-07 | United Technologies Corporation | Fuel nozzle for burner construction |
US4802423A (en) * | 1987-12-01 | 1989-02-07 | Regenerative Environmental Equipment Co. Inc. | Combustion apparatus with auxiliary burning unit for liquid fluids |
EP0985882B1 (en) * | 1998-09-10 | 2003-12-03 | ALSTOM (Switzerland) Ltd | Vibration damping in combustors |
US7410288B1 (en) * | 1998-12-24 | 2008-08-12 | Luminis Pty. Ltd. | Fluid mixing device |
WO2009014654A3 (en) * | 2007-07-20 | 2009-03-05 | Astec Ind | Coal burner assembly |
US8083517B2 (en) * | 2008-03-28 | 2011-12-27 | Fives North American Combustion, Inc. | Method of operating a furnace |
US20090246719A1 (en) * | 2008-03-28 | 2009-10-01 | Newby John N | Method of operating a furnace |
US20140123632A1 (en) * | 2012-05-25 | 2014-05-08 | Hino Motors, Ltd. | Burner for exhaust purifying device |
US20130340404A1 (en) * | 2012-06-22 | 2013-12-26 | General Electric Company | Hot egr driven by turbomachinery |
US9347375B2 (en) * | 2012-06-22 | 2016-05-24 | General Electronic Company | Hot EGR driven by turbomachinery |
US20170108224A1 (en) * | 2014-04-03 | 2017-04-20 | Siemens Aktiengesellschaft | Burner, gas turbine having such a burner, and fuel nozzle |
US10125993B2 (en) * | 2014-04-03 | 2018-11-13 | Siemens Aktiengesellschaft | Burner, gas turbine having such a burner, and fuel nozzle |
US10612773B2 (en) | 2014-04-10 | 2020-04-07 | Sofinter S.P.A. | Burner |
WO2015154969A1 (en) * | 2014-04-10 | 2015-10-15 | Sofinter S.P.A. | Burner |
CN106415127A (en) * | 2014-04-10 | 2017-02-15 | 索斐特公司 | Burner |
CN106415127B (en) * | 2014-04-10 | 2020-09-15 | 索斐特公司 | Burner with a burner head |
RU2689654C2 (en) * | 2014-04-10 | 2019-05-28 | Софинтер С.П.А. | Burner |
US10105676B2 (en) * | 2015-08-06 | 2018-10-23 | Guangdong Hydrogen Energy Science And Technology Co., Ltd | Start-up system for starting reforming hydrogen production device |
US20190093948A1 (en) * | 2016-02-17 | 2019-03-28 | Eisenman Se | Burner unit and device for the temperature control of objects |
US10928134B2 (en) * | 2016-02-17 | 2021-02-23 | Eisenmann Se | Burner unit and device for the temperature control of objects |
US10569619B2 (en) * | 2016-09-15 | 2020-02-25 | Eberspächer Climate Control Systems GmbH & Co. KG | Combustion chamber assembly unit for a fuel-operated vehicle heater |
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