US854156A - Process of conducting combustion. - Google Patents
Process of conducting combustion. Download PDFInfo
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- US854156A US854156A US23706504A US1904237065A US854156A US 854156 A US854156 A US 854156A US 23706504 A US23706504 A US 23706504A US 1904237065 A US1904237065 A US 1904237065A US 854156 A US854156 A US 854156A
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- Prior art keywords
- combustion
- flame
- jets
- air
- burning
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
- F23G5/44—Details; Accessories
- F23G5/46—Recuperation of heat
Definitions
- T0 calla/171 071 it may concern.
- This invention relates to the process of conducting combustion by producing a volu minous slow-burning flame with the use of neutral gas in the draft-current as a diluent for the oxygen, as described in my Patent No. 692,257, February 4, 1902.
- the present invention relates more particularly to that branch of the practice of said art according to which the flame is de veloped in a comparatively free space such as the hearth-chamber of a reverberatory furnace, and the invention has for its object the provision of means whereby an intense combustion may be obtained from a flame of the aforesaid character at any desired point or points.
- the present invention involves the same general idea of means as that disclosed in my aforesaid application, but specifically differs from it in that the terminus of the flame is not caused to shift, but the result of covering a considerable area of the materials with the localized combustion is obtained with stationary jets.
- This result may be brought about by causing a series of jets to act simultaneously at different points along the combustion chamber and so arranging as that those jets first encountered by the flame shall localize the combustion of a portion only of the gaseous current, the remaining portion passing on to the neXt jet or group of jets, which localize the combustion of a further portion of the current, and so on until the desired area has been covered.
- Figure 1 represents a longitudinal section of a reverberatory furnace equipped according to and adapted to carry out my invention
- Fig. 2 represents a plan view thereof
- Fig. 3 represents an enlarged transverse section on the line 3-3 of Fig. 2.
- 13 is the grate of the firebox, 14 the firechamber above the grate, 15 the ash-pit below, and 16 the bridge-wall.
- a pipe 18 leads back to the ash-pit 15 for conducting a portion of the stackgases underneath the grate.
- a fan-blower 19 and an air-inlet 20 back of said fan for supplying such portion of air to the draft as is necessary to maintain the desired combustion.
- valves or dampers in the pipe 18 and its air-branch for regulating the relative quantity of air and stack-gas in the draft current.
- Air is supplied by a pipe 25 from an air-compressor 26.
- the effect of the neutral diluent in the airdraft is to produce a voluminous slow-burning flame inflated by the inert gases and relatively cool as compared with an ordinary flame.
- the fuel-bed also burns at a lower temperature by reason of the presence of the stack gases, carbon dioxid reacting with carbon to form carbon monoxid by an endothermic reaction which counteracts the exothermic action of the air in the draft current.
- the flame which enters the hearth-chamber is capable of burning at a long distancefrom the seat of initial combustion.
- the lower and outer portions of the flaming gas-current are subjected to the influence of these jets, whichagitate the ingredients of the flame, bringing about a vigorous union of the oxygen and combustible and locally intensifying the combustion.
- the remaining portion of the slow-burning flame passes between and above the first pair of jets and encounters the second pair which, owing to their direction and greater elevation, will influence those portions of the flame which have passed above the first jets, and owing to the conical shape of the jets they may be caused to influence a larger area of the materials on the hearth.
- the results aimed at may be promoted by employing jets of diflerent velocities.
- jets of diflerent velocities By imparting to the first pair of jets, nearest to the hearth and to the fire-box, a light velocity and a relatively small volume, they may be caused to influence the lower portion only of the flaming gascurrent.
- the next pair of jets has a greater velocity and influences a higher portion of the gas current, and so on.
- the mixture of air and stack gases is supplied to the fuel bed faster than the reactive capacity -of the fuel and much of the same passes through to inflate the combustible gases produced, yielding a gaseous mixture in which the combustible burns tardily owing to the specific damping influence of carbon dioxid upon the formation of more carbon dioxid, the dilution and the comparative paucity of free oxygen.
- the result is a tardily but uniformly burning flame atmosphere, with combustion. throughout its mass.
- the process of conducting combustion which consists in producing a tardily burning voluminous inflated flame and locally intensifying the COlnbUStlOTi of said flame in a plurality of horizontal strata at points at dill'erent distances from. its origin by a series ol piercing air jets directed into said strai a at such points from the side.
- the process of combustion which consists in passing through a shallow bed of ignitcd fuel a draft current of air diluted wit h products of COIl'l'lbllStlOi'l, passing the resultant ignitcd gaseous products through a reverberatory furnace and intensifying their combustion in a plurality of horizontal. stral a by piercing air jets located at dill'erent dis tanees from the fuel bed and directed into different strata.
- the process of combustion which consists in producing a tardily burning inflated voluminous flame and localizing the combustion of said flame by a plurality of jets operating at different distances from the origin of the flame and originating at distances from the hearth Which successively increase in the direction of travel of the flame.
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- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
PATENTED MAY'21, 1907.
- B. E. ELDRED'.
PROCESS OF CONDUCTING COMBUSTION.
APPLICATION FILED 10150.16, 1904.
3 SHEETS"SHEET 1.
gwa l -v w mm WITNESSES:
. ATT RNEY:
n .11. uammcrmyv. c.
PATENTED MAY 21, 1907.
7 B.E.ELDRED. PROGESS 0F CONDUCTING COMBUSTION.
APPLICATION FILED DEO.16, 1904.
' a sums-311mm 2.
WITNESSES:
ATTORNEYS THE mmms Pz-rsss co, wnsmnamlv, n. c.
3 SHEETS-SHET 3.
PATENTED MAY 21, 1907.
B. E. ELDRED. PROCESS OF CONDUCTING COMBUSTION.
APPLIOATION FILED 1330.16, 1904.
- ATTORNEYS WITNESSES TM: NORRIS PETERS cuv, WASHINGTON, n. c.
UNITED STATES PATENT OFFICE.
BYRON E. ELDREB, OF BRONXVILLE, NEW YORK, ASSIGNOR TO COMBUS- TION UTILITIES COMPANY, OF NET/V YORK, N. Y., A CORPORATION OF NEW YORK.
Specification of Letters Patent.
Patented May 21, 1907.
Application filed December 16, 190%. Serial N0. 237,065.
T0 calla/171 071 it may concern.
Be it known that I, BYRON E. ELDRED, a citizen of the United States, residing at BronXville, county of VVestchester, State of New York, have invented certain new and useful Improvements in Processes of Conducting Combustion, of which the following specification and accompanying drawings disclose as an illustration one embodiment thereof which I now regard as the best out of the various forms in which the principles of my invention may be applied.
This invention relates to the process of conducting combustion by producing a volu minous slow-burning flame with the use of neutral gas in the draft-current as a diluent for the oxygen, as described in my Patent No. 692,257, February 4, 1902.
The present invention relates more particularly to that branch of the practice of said art according to which the flame is de veloped in a comparatively free space such as the hearth-chamber of a reverberatory furnace, and the invention has for its object the provision of means whereby an intense combustion may be obtained from a flame of the aforesaid character at any desired point or points.
In an application Serial Number 225,395, filed Sept. 21, 1904 pending concurrently herewith I have described means for localizing and intensifying the combustion at any desired point by mechanical agitation which may be produced by a transverse jet of a gaseous nature such as an air-jet, and in order to cover any desired area of the materials under treatment my aforesaid application shows a series of nozzles and an air-distributing valve-mechanism whereby a series of jets are rojected in succession across the path of t e flame at successive points, the specific operation of that arrangement being that each jet or series of jets in action at any instant uses up substantially all of the combustible of the flame and abruptly terminates the combustion. The terminus of the flame must therefore according to that arrangement shift relatively to the material in order to make the localized or intensified combustion effective over a considerable area of the materials, which shifting is effected by the valve-mechanism.
The present invention involves the same general idea of means as that disclosed in my aforesaid application, but specifically differs from it in that the terminus of the flame is not caused to shift, but the result of covering a considerable area of the materials with the localized combustion is obtained with stationary jets. This result may be brought about by causing a series of jets to act simultaneously at different points along the combustion chamber and so arranging as that those jets first encountered by the flame shall localize the combustion of a portion only of the gaseous current, the remaining portion passing on to the neXt jet or group of jets, which localize the combustion of a further portion of the current, and so on until the desired area has been covered.
Figure 1 represents a longitudinal section of a reverberatory furnace equipped according to and adapted to carry out my invention; Fig. 2 represents a plan view thereof; Fig. 3 represents an enlarged transverse section on the line 3-3 of Fig. 2.
- The same reference characters indicate the same parts in all the figures.
indicates a hearth-chamber having fireboX 11 at one end and a stack 12 at the other end.
13 is the grate of the firebox, 14 the firechamber above the grate, 15 the ash-pit below, and 16 the bridge-wall.
From a point below the damper 17 in the stack 12 a pipe 18 leads back to the ash-pit 15 for conducting a portion of the stackgases underneath the grate. In this pipe is a fan-blower 19 and an air-inlet 20 back of said fan for supplying such portion of air to the draft as is necessary to maintain the desired combustion.
21 and 22 are valves or dampers in the pipe 18 and its air-branch for regulating the relative quantity of air and stack-gas in the draft current.
From the sides of the hearthchamb er 10 a series of inclined nozzles 23 project toward each other and downward toward the lower.
minate at vertical distances from the hearth increasing successively 1n the direction of travel of the flame. They are shown in. pairs as indicated in Fig. 2. Air is supplied by a pipe 25 from an air-compressor 26.
The effect of the neutral diluent in the airdraft is to produce a voluminous slow-burning flame inflated by the inert gases and relatively cool as compared with an ordinary flame. The fuel-bed also burns at a lower temperature by reason of the presence of the stack gases, carbon dioxid reacting with carbon to form carbon monoxid by an endothermic reaction which counteracts the exothermic action of the air in the draft current. The flame which enters the hearth-chamber is capable of burning at a long distancefrom the seat of initial combustion. Upon encountering the air-jets issuing from the first pair of nozzles 23 the lower and outer portions of the flaming gas-current are subjected to the influence of these jets, whichagitate the ingredients of the flame, bringing about a vigorous union of the oxygen and combustible and locally intensifying the combustion. The remaining portion of the slow-burning flame passes between and above the first pair of jets and encounters the second pair which, owing to their direction and greater elevation, will influence those portions of the flame which have passed above the first jets, and owing to the conical shape of the jets they may be caused to influence a larger area of the materials on the hearth. Those portions of the original flaming gas-current which escape past the second pair of jets, upon encountering the third pair will be furt-her consumed thereby and the combustion locally intensified, and so on. In this way the original relatively-cool and voluminous slow-burning flame is distributed over a large area of the materials under treatment and its combustion locally intensified in a series of restricted regions simultaneously, at different distances from the origin of the flame.
The results aimed at may be promoted by employing jets of diflerent velocities. By imparting to the first pair of jets, nearest to the hearth and to the fire-box, a light velocity and a relatively small volume, they may be caused to influence the lower portion only of the flaming gascurrent. The next pair of jets has a greater velocity and influences a higher portion of the gas current, and so on.
The mixture of air and stack gases is supplied to the fuel bed faster than the reactive capacity -of the fuel and much of the same passes through to inflate the combustible gases produced, yielding a gaseous mixture in which the combustible burns tardily owing to the specific damping influence of carbon dioxid upon the formation of more carbon dioxid, the dilution and the comparative paucity of free oxygen. The result is a tardily but uniformly burning flame atmosphere, with combustion. throughout its mass.
The excess of free oxygen furnished by ihc penetrating air jets causes free combustion in their vicinity and consequent quick de velopment of heat. This flame almosphei-e as compared with an ordinary flame, may be said to be dilated. or inflated. by the presence of the diluting substances named.
What I claim as new and desire to secure by Letters Patent is:
1.. The process of conducting combustion which consists in producing a tardily burnin voluminous inflated flame and locally intensifying the combustion of said flame in a plurality of horizontal strata at points at dill'er ent distances from its origin.
2. The process of conductii'ig combustion which consists in producing a l'ardily bnning voluminous inflated flame and locally intensifying the combustion of said flame in a plurality of horizontal strata at points at dillcrent distances from. its origin, each further point being located in higher strata than each nearer.
The process of conducting combustion which consists in producing a tardily burning voluminous inflated flame and locally intensifying the COlnbUStlOTi of said flame in a plurality of horizontal strata at points at dill'erent distances from. its origin by a series ol piercing air jets directed into said strai a at such points from the side.
4. The process of conducting combustion which consists in producing a tardily burning voluminous inflated flameand locally intensifying the combustion of said :llamc in a plurality of horizontal strata at points at dill'er ent distances from .its origii'i by a series of piercing air jets directed into said strata at such points from the side, each further point being located in a higher stratum than each nearer.
The process of combustion which consists in passing through a shallow bed of ignitcd fuel a draft current of air diluted wit h products of COIl'l'lbllStlOi'l, passing the resultant ignitcd gaseous products through a reverberatory furnace and intensifying their combustion in a plurality of horizontal. stral a by piercing air jets located at dill'erent dis tanees from the fuel bed and directed into different strata.
6. The process of con'ibustion which consists in passing through a shallow bed of ignited fuel a draft currei'it of air diluted wit h products of combustion, passing the resultant ignitcd gaseous products through. a reverberatory furnace and intensifying their combustion in a plurality of horizontal stral a each further jet being directed into a higher stratum than each nearer.
7. The process of combustion which consists in producing a tardily burning inflated VOl'tlll'llllOUS flame, localizing the combustion of said flame at a plurality of points at difl'crcnt distances from its origin. and in. different strata of said flame by ets of different velocities.
8. The process of combustion which consists in producing a tardily burning inflated voluminous flame, and localizing the combustion of said flame by a plurality of air jets of diflerent velocities acting simultaneously at different distances from the origin of the flame and in different strata of said flame.
9. The process of combustion which consists in producing a tardily burning inflated voluminous flame and localizing the combustion of said flame by a plurality of jets operating at different distances from the origin of the flame and originating at distances from the hearth Which successively increase in the direction of travel of the flame.
10. The process of heating material in re- BYRON E. ELDRED.
WVitnesses:
JAs. W. KEILL, M. W. BACON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US23706504A US854156A (en) | 1904-12-16 | 1904-12-16 | Process of conducting combustion. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US23706504A US854156A (en) | 1904-12-16 | 1904-12-16 | Process of conducting combustion. |
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US854156A true US854156A (en) | 1907-05-21 |
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US23706504A Expired - Lifetime US854156A (en) | 1904-12-16 | 1904-12-16 | Process of conducting combustion. |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447252A (en) * | 1940-07-17 | 1948-08-17 | Jimenez Ramon Castro | Heating apparatus with provision for utilizing combustion gases |
US2541588A (en) * | 1947-07-15 | 1951-02-13 | Leighton P Kerruish | Air injection smoke-consuming structure for furnaces |
-
1904
- 1904-12-16 US US23706504A patent/US854156A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447252A (en) * | 1940-07-17 | 1948-08-17 | Jimenez Ramon Castro | Heating apparatus with provision for utilizing combustion gases |
US2541588A (en) * | 1947-07-15 | 1951-02-13 | Leighton P Kerruish | Air injection smoke-consuming structure for furnaces |
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