US1086712A - Method of burning finely-divided fuel. - Google Patents
Method of burning finely-divided fuel. Download PDFInfo
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- US1086712A US1086712A US63663211A US1911636632A US1086712A US 1086712 A US1086712 A US 1086712A US 63663211 A US63663211 A US 63663211A US 1911636632 A US1911636632 A US 1911636632A US 1086712 A US1086712 A US 1086712A
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- Prior art keywords
- air
- burner
- blades
- plate
- fuel
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- 239000000446 fuel Substances 0.000 title description 28
- 238000000034 method Methods 0.000 title description 13
- 238000002485 combustion reaction Methods 0.000 description 13
- 239000000203 mixture Substances 0.000 description 6
- 239000007787 solid Substances 0.000 description 4
- 238000007599 discharging Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000011872 intimate mixture Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000007142 ring opening reaction Methods 0.000 description 1
Images
Classifications
-
- 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
Definitions
- WITNESSES )0 lNi/E TOR V A TTORNEYJ.
- FIG. l is a front elevation of a furnace adapted for burning fuel according to my invention; Fig. a longitudinal section of a portion of the furnace; Fig. :5 a front elevation of one form of the air-deflecting plate; Fig. i a. section on the plane of the line 14 of Fig. 3; Fig. 5 an enlarged section on the plane of the line 5 5 of Fig. 3; Fig. 6 a front elevation of another form of air-deflecting plate; Fig. .7 a section on the plane of the line 7-7 of Fig. 6; Fig.
- FIG. 8 an edge view of Fig. 6;
- FIG. 9 a front elevation of another form of air-deflecting plate;
- Fig. 10 a section on the plane of the line 10-1O of Fig. 9;
- Fig. 11 an edge view of Fig. 9;
- Fig. 12 a front elevation of the furnace showing a special air duct: Fig. 13.
- FIG. 12 a longitudinalsection of Fig. 12;
- Fig. 14 a front elevation of an air-deflecting plate having blades set tangentially to the central opening;
- Fig. 15 a similar view with the blades set in an opposite direction to the blades of Fig. ll.
- the prime object of all methods of burning finely-divided fuel is to obtain a continuous and intimate mixture of the fuel and an amount of air as nearly as possible equal to the theoretical quantity required to effect complete comhust ion. If the mixing process is not uniform an (1 continuous. an intermittent explosive ac tion takes place resulting in severe vibrations in the furnace. If the mixture is not thoroughly elfected, a large excess of air is required with resultant loss in elliciency.
- a substantially flat plate comprising blades set at an angle to the general plane of the plate, these blades being spaced apart so as to provide openings for the admission of air to the atomized fuel.
- any suitable form of atomizer or so-called burner may be used. such. for example, as that shown in United States Patent 1,007,793, dated November 7, 1911.
- the burner is connected to a supply pipe 1. and terminatescinwroximity to a central opening in flie plate; liat is, it may tenni nate a short distance 11 front or rear of said plate, or within said opening, in order that the issuing stream of fuel may be acted upon immediately by the whirling air current.
- the plate 2 is in the-form of a square or rectangular casting having suitable provision for securing it in an opening in the wall of the furnaee.
- the plate comprises a central ring 3 to provide an opening through which the fuel may be projected from the burner.
- the latter oes not completely fill the space within the ring so that, in addition to the air admitted between the blades, a rela* tively small column is admitted through the ring opening. From this ring radiate a series' of blades 4, inclined inwardly from ribs 5.
- FIGs. 6, 7 and 8 I have shown another form of air-directing plate in which the blades 6 are preferably of sheet metal having their ends secured to the plate 7 and a central ring 8.
- Figs. 3 and 6 the blades of the plate do not overlap each other.
- Figs. 9, ltland 11 show a modification in which the blades 9 are preferably made of sheet metal and so cut as to eye 'tp 4 a. other.
- the outer ends of the blades are riveted or otherwise secured to a plate 10, and their inner ends secured between two ring plates 11. This overlapping of the blades broadens the flame andjs of advantage, therefore, when a short, wide furnace is preferred.
- the blades and openings between them may extend radially from the central opening, or may be tangential to said opening, as shown in Figs. 14 and 15. 7
- the burner terminates 'in proximity to the central opening 12 of the plate, either immediately in front, or at the rear, or within said opening, and the issuing. fuel expands in the furnace chamber to assume the shape of a cone approximately as shown in Figs. 2 and 13.
- the column of air through the plate may be induced by the stack draft or by a forced draft. As the inner ends of the blades terminate in close proximity to the burner, the
- whirling motion begins immediately afterthe volume of air passes the plate so that the issuing stream of fuel is intermlxed with and surrounded bythe whirling volume of air practically immediately it is a-xierstisi from the burner.
- the number of blades in a pt 1.: and arrangement relative to each other, are i c1 erably as shown in the drawings; that is, I have shown 26 blades and they are so ar ranged relative to each other that the volume of air will be divided into columns, each column assuming a course determined by the angularity of the blades, the columns of air immediately uniting, after pass ng the blades, into a solid whirling column.
- the invention is not limited to the preferred number of blades or to the exact ar rangementshown, as the number may be reried and the relation of the blades may be changed to suit the particular furnace or fuel requirements.
- blades radiating from the ring 8 having an external diameter of about two and three-quarter inches, and the opening in the plate 7 having a diameter of about eight inches.
- the internal diameter of the ring 8 was about two inches, or about one-quarter that of the diameter of the plate opening.
- the blades 6 were each flat and about three-eighths of an inch wide at the inner end and one inch wide at the,
- the burner in this example was of the construction shown in the Peabody Patent. No. 1,007,793, dated November 7, 1911. with an outlet orifice three-sixtyfonrths of an inch in diameter.
- the pressure on the oil was about 135 pounds and the oil was what is commercially known as Texas Crude of about 27.
- the temperature of the oil entering the burneg was about 175 degrees Fahrenheit.
- the flame appeared to be a solid coho of flame filling the space between the e c
- the flame appeared to be a hollow cone because the front of the burner was visible the eye
- the extent of the flame back of the plate is from three and one-half to four feet, whereas, under the same conditions, excepting the omission of the blades 6, 6, the flame will be lengthened to about seven feet.
- the plate is substantially flat so that the air passes through it substantially in a whirling column, encompassing the nonwhirling column of air passing through the ring 8, which in turn encompasses the spray of oil at the start, after which the inner column is whirled by contact with the outer column making a solid whirling column.
- the method of firing which consists in discharging finely divided fuel from a burner into a combustion chamber, admitting the air for combustion in a column surrounding and coaxial with the burner through 0 enings terminating in close proximity to t e burner and in a plane substantially at right angles to the axis of the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to pause the air to penetrate and mix with the uel.
- the method of firing which consists in discharging finely divided fuel from a burner into a combustion chamber, admit ting the air for combustion in a column surrounding and coaxial with the burner through openings terminating in close proximity to the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to cause the air to penetrate and mix with the fuel, said deflection beginning after the air has passed the plane of the end of the burner.
- the method of firing which consists in discharging finely divided fuel from a burner in expanding cone form into a combustion chamber, admitting the air for combustion in a column surrounding and coaxial with the burner through openings terminating in close proximity to the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to cause the air to penetrate and mix with the fuel.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
Description
D. J. IRISH. METHOD OF BURNING FINBLY DIVIDED FUEL.
APPLICATION FILED JULY 3 1911. 1,086,712. Patented Feb. 10, 1914,
3 BHEBTa-BHEET 1.
D. J. IRISH. METHOD OF BURNING FINELY DIVIDED FUEL.
APPLIOATXON FILED JULY 3, 1911v 1 ,086,7 1 2 Patented Feb. 10, 1914.
3 SHEETS-SHEET 2.
WITNESSES: )0 lNi/E TOR V A TTORNEYJ.
D. J. IRISH. METHOD OF BUBNMG FINELY DWIDBD FUEL.
APPLIOATIOH IILED JULY 3, 1911 Patented Feb. 10, 1914,
3 SHEETS-SHEET 3.
UNrrED STATES PA rEnr OFFICE.
DAVID J. IRISH, OF NEW YORK, N. Y., ASSIGNOR TO THE BABCOCK & WILCOX COMPANY, OF BAYONNE, NEXV JERSEY, A CORPORATION OF NEW JERSEY.
METHOD OF BURNING FINELY-DIVIDED FUEL.
Application filed July 3, 1911.
2' '0 all whom it may concern.
Be it known that I, DAVID J. linen, a citizen of the United States, residing in the city of New York, borough of Richmond, county of Richmond, and State of New York, have invented certain new and useful Improvements in the Method of Burning Finely-Divided Fuel, of which the following is a specification.
My invention relates to a method of burn ing finely-divided fuel, and will be under stood from the following description taken in connection. with the accompanying drawings, in which- Figure l is a front elevation of a furnace adapted for burning fuel according to my invention; Fig. a longitudinal section of a portion of the furnace; Fig. :5 a front elevation of one form of the air-deflecting plate; Fig. i a. section on the plane of the line 14 of Fig. 3; Fig. 5 an enlarged section on the plane of the line 5 5 of Fig. 3; Fig. 6 a front elevation of another form of air-deflecting plate; Fig. .7 a section on the plane of the line 7-7 of Fig. 6; Fig. 8 an edge view of Fig. 6; Fig. 9 a front elevation of another form of air-deflecting plate; Fig. 10 a section on the plane of the line 10-1O of Fig. 9; Fig. 11 an edge view of Fig. 9; Fig. 12 a front elevation of the furnace showing a special air duct: Fig. 13.
a longitudinalsection of Fig. 12; Fig. 14 a front elevation of an air-deflecting plate having blades set tangentially to the central opening; Fig. 15 a similar view with the blades set in an opposite direction to the blades of Fig. ll.
Similar reference numerals indicate similar parts in the several views.
The prime object of all methods of burning finely-divided fuel is to obtain a continuous and intimate mixture of the fuel and an amount of air as nearly as possible equal to the theoretical quantity required to effect complete comhust ion. If the mixing process is not uniform an (1 continuous. an intermittent explosive ac tion takes place resulting in severe vibrations in the furnace. If the mixture is not thoroughly elfected, a large excess of air is required with resultant loss in elliciency. By the present invention I aim to secure a. continuous, uniform and in timate mixture by causing the air which is being drawn or forced into the combustion Specification of Letters Patent.
Patented Feb. 10, 1914.
Serial No. 686,682.
chamber to come in contact with means so placed as to deflect the air in planes at ail angle to its direction of travel, and to impart to the air a whirling or rotating motion in a path surrounding, cutting through and mixing with the stream of finely-divided fuel. This action imparts to the fuel, as a consequence, a whirling or rotating motion in the same direction as that assumed by the air, and in so doing, thoroughly mixes the air with the fuel, thereby making a solid flame. The resulting turning over and over of the fuel in it gradually expanding volume brings all its particles into contact with the air and this insures complete combustion.
In practising the method herein described I provide a substantially flat plate comprising blades set at an angle to the general plane of the plate, these blades being spaced apart so as to provide openings for the admission of air to the atomized fuel.
As a result of experience I have determined upon an angle of inclination of the blades of forty-five degrees to the plane of their supporting plate as giving the best results. This angle, however, can be varied according to the pressure, or according to the character of the fuel, orthe character of the particular furnace to which the burner is applied. The blades which cause the deflection of the air are susceptible of various modifications coming within the scope of my invention. as, for example, they may be cast integral with a supporting plate, or may be secured thereto in fixed relation to one another and t0 the plate.
For the purpose of illustration, I have shown my invention as applied to a boiler furnace. Any suitable form of atomizer or so-called burner may be used. such. for example, as that shown in United States Patent 1,007,793, dated November 7, 1911. The burner is connected to a supply pipe 1. and terminatescinwroximity to a central opening in flie plate; liat is, it may tenni nate a short distance 11 front or rear of said plate, or within said opening, in order that the issuing stream of fuel may be acted upon immediately by the whirling air current. In burners used by me the fuel, as it is projected into the furnace chamber, assumes a conical shape and, to effect the desired intimate mixture therewith of the air necessary for complete'combustion, I provide means comprising blades to deflect the column of air from its normal patlras it enters the combustion chamber around the burner. These blades which effect a change in the direction of travel of the air may be supported in any suitable manner in an opening in the furnace wall. I prefer, however, to mount them on a plate, either integral with the plate or secured thereto by any suitable means. By employing a plate to which the blades are secured they may be conveniently handled and mounted in the furnace wall. 4
Referring to Figs. 3, 4 and 5, the plate 2 is in the-form of a square or rectangular casting having suitable provision for securing it in an opening in the wall of the furnaee. The plate comprises a central ring 3 to provide an opening through which the fuel may be projected from the burner. The latter oes not completely fill the space within the ring so that, in addition to the air admitted between the blades, a rela* tively small column is admitted through the ring opening. From this ring radiate a series' of blades 4, inclined inwardly from ribs 5.
In Figs. 6, 7 and 8 I have shown another form of air-directing plate in which the blades 6 are preferably of sheet metal having their ends secured to the plate 7 and a central ring 8.
In Figs. 3 and 6 the blades of the plate do not overlap each other. Figs. 9, ltland 11 show a modification in which the blades 9 are preferably made of sheet metal and so cut as to eye 'tp 4 a. other. In this form the outer ends of the blades are riveted or otherwise secured to a plate 10, and their inner ends secured between two ring plates 11. This overlapping of the blades broadens the flame andjs of advantage, therefore, when a short, wide furnace is preferred.
In the constructions above described the plates as a whole are substantially flat, and
the blades rigidly secured in position.
The blades and openings between them may extend radially from the central opening, or may be tangential to said opening, as shown in Figs. 14 and 15. 7
As before stated, the burner terminates 'in proximity to the central opening 12 of the plate, either immediately in front, or at the rear, or within said opening, and the issuing. fuel expands in the furnace chamber to assume the shape of a cone approximately as shown in Figs. 2 and 13.
The column of air through the plate may be induced by the stack draft or by a forced draft. As the inner ends of the blades terminate in close proximity to the burner, the
whirling motion begins immediately afterthe volume of air passes the plate so that the issuing stream of fuel is intermlxed with and surrounded bythe whirling volume of air practically immediately it is a-xierstisi from the burner.
The number of blades in a pt 1.: and arrangement relative to each other, are i c1 erably as shown in the drawings; that is, I have shown 26 blades and they are so ar ranged relative to each other that the volume of air will be divided into columns, each column assuming a course determined by the angularity of the blades, the columns of air immediately uniting, after pass ng the blades, into a solid whirling column. The invention, however, is not limited to the preferred number of blades or to the exact ar rangementshown, as the number may be reried and the relation of the blades may be changed to suit the particular furnace or fuel requirements.
In Figs. 12 and 13 I have shown the application of the invention with a forced draft air duct, the air duct 13 leading from any suitable source of supply and terminating at a point to completely inclose the substantially flat air-directing plate. However, as above stated, the air supply may be in duced by the stack draft To still more thoroughly explain the nature of my invention, I will describe a specitic example of-practising it when using the air-directing plate and burner shown in Figs. 2, 6, T and 8.
There were 26 blades radiating from the ring 8, the latter having an external diameter of about two and three-quarter inches, and the opening in the plate 7 having a diameter of about eight inches. The internal diameter of the ring 8 was about two inches, or about one-quarter that of the diameter of the plate opening. The blades 6 were each flat and about three-eighths of an inch wide at the inner end and one inch wide at the,
outer end, and separated about one-eighth of an inch apart at the inner end and onehalf of an inch apart at the outer 'end. They were set at an angle of about forty-five degrees. The outlet of the burner was set about one-half inch back of the outer plane of ring; 8. The burner in this example was of the construction shown in the Peabody Patent. No. 1,007,793, dated November 7, 1911. with an outlet orifice three-sixtyfonrths of an inch in diameter. The pressure on the oil was about 135 pounds and the oil was what is commercially known as Texas Crude of about 27. The temperature of the oil entering the burnegwas about 175 degrees Fahrenheit. Natural draft was employed of two-tenths an inch in the furioo tier, and in this experiment only the middle] one of the upper tier was lighted; that being the one upon which observations were made. There were about 75 pounds pressure in the boiler which was of the type shown in Figs. 2 and 13 with the grate bars removed.
By looking between the plates the following observations were made. Ignition began in a plane about one and onequarter inches behind the plate and about two inches from the front of the burner, and the flame extended into the furnace a distance of from three and onc-half to four feet back'of the plate, and at its farther end was about 36 inches in diameter. From the observations made, it appeared that the oil spray diverged at an angle of about 31 degrees from the axis of the burner, and. to all appear and the burner.
ances the oil spray commenced its rotary or whirling motion by the time it reached the plane of ignition and continued the same until consumed.
Looking at the flame through a peep-hole in the rear end of the furnace opposite the burner, the flame appeared to be a solid coho of flame filling the space between the e c On the contrary, when t e same conditions were maintained with the exception of omitting the blades 6, the flame appeared to be a hollow cone because the front of the burner was visible the eye The conclusion from this circumstance is, that the rotary or whirling motion imparted to the column of air by theblades 6, 6, from the outside to the center, causes the air to penetrate the 'Qone of oil vapor and to extend the combustion inward into the cone.
As already stated, in the example given, the extent of the flame back of the plate is from three and one-half to four feet, whereas, under the same conditions, excepting the omission of the blades 6, 6, the flame will be lengthened to about seven feet.
As shown, the plate is substantially flat so that the air passes through it substantially in a whirling column, encompassing the nonwhirling column of air passing through the ring 8, which in turn encompasses the spray of oil at the start, after which the inner column is whirled by contact with the outer column making a solid whirling column. I
do not wish to limit myself, however, to a flat directing plate since I am aware that it may be inclined inward from the ring 8 to a considerable extent, say, not to exceed degrees from the plane of ring 8.
burner into a combustion chamber, admit-,
ting the air for combustion in a column sur-" rounding and coaxial with. the burner through openings terminating in close proximity to the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to cause the air to penetrate and mix with the fuel.
2. The method of firing which consists in discharging finely divided fuel from a burner into a combustion chamber, admitting the air for combustion in a column surrounding and coaxial with the burner through 0 enings terminating in close proximity to t e burner and in a plane substantially at right angles to the axis of the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to pause the air to penetrate and mix with the uel.
3.,The method of firing which consists in discharging finely divided fuel from a burner into a combustion chamber, admit ting the air for combustion in a column surrounding and coaxial with the burner through openings terminating in close proximity to the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to cause the air to penetrate and mix with the fuel, said deflection beginning after the air has passed the plane of the end of the burner.
4. The method of firing which consists in discharging finely divided fuel from a burner in expanding cone form into a combustion chamber, admitting the air for combustion in a column surrounding and coaxial with the burner through openings terminating in close proximity to the burner, and deflecting the air as it passes said openings so as to give it a whirling motion to cause the air to penetrate and mix with the fuel.
In testimony whe eof, I have hereunto signed my name in the presence of two subscribing witnesses.
DAVID J. IRISH.
Vitnesses E. H. PEABODY, CHARLES A. J ones.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US63663211A US1086712A (en) | 1911-07-03 | 1911-07-03 | Method of burning finely-divided fuel. |
| US745009A US1086715A (en) | 1911-07-03 | 1913-01-29 | Apparatus for burning finely-divided fuel. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US63663211A US1086712A (en) | 1911-07-03 | 1911-07-03 | Method of burning finely-divided fuel. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1086712A true US1086712A (en) | 1914-02-10 |
Family
ID=3154936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US63663211A Expired - Lifetime US1086712A (en) | 1911-07-03 | 1911-07-03 | Method of burning finely-divided fuel. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1086712A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2464791A (en) * | 1943-11-05 | 1949-03-22 | Claude A Bonvillian | Apparatus for the combustion of fuel |
-
1911
- 1911-07-03 US US63663211A patent/US1086712A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2464791A (en) * | 1943-11-05 | 1949-03-22 | Claude A Bonvillian | Apparatus for the combustion of fuel |
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