US1963009A - High-power gas heating apparatus - Google Patents
High-power gas heating apparatus Download PDFInfo
- Publication number
- US1963009A US1963009A US500969A US50096930A US1963009A US 1963009 A US1963009 A US 1963009A US 500969 A US500969 A US 500969A US 50096930 A US50096930 A US 50096930A US 1963009 A US1963009 A US 1963009A
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- US
- United States
- Prior art keywords
- gas
- air
- mixture
- conduit
- combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- 238000010438 heat treatment Methods 0.000 title description 5
- 239000007789 gas Substances 0.000 description 67
- 238000002485 combustion reaction Methods 0.000 description 54
- 239000000203 mixture Substances 0.000 description 45
- 239000011872 intimate mixture Substances 0.000 description 5
- 239000006185 dispersion Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000003467 diminishing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000000149 penetrating effect Effects 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
- F23C99/00—Subject-matter not provided for in other groups of this subclass
-
- 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
- F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
- F23C2700/04—Combustion apparatus using gaseous fuel
Definitions
- the invention has for its object, among other things, to overcome this difliculty by providing for a much more intimate admixture of the gases with ,the air, whereby the igniting speed of the gases is materially increased, and also preferably by providing a suitable impediment or impediments infront of the opening of the supply or feed conduit of the gas-air mixture into the combustion shaft.
- the gas-air mixture -breaks against said impediments, in the lee of which there is thus formeda zone, or zones, of lower velocity, lower than the speed of ignition.
- the flow or stream of the gas-air mixture rapidly spreads over a materially greater crosssectional area.- The mean speed of flow thus drops below the igniting speed. allowing the flame to ignite quietly in the lee of the impediments. A'quiet flame filling the combustion shaft is thus secured without the impediments diminishing in any degree the amount 01 the air and gas mixture supplied.
- Fig. 1 shows a Cowper'of conventional con-.
- Fig. 2 is a longitudinal sectional elevation of the air conduit, with the inserted gas pipes;
- Fig. 3 is an end view of the construction shown. 9 in Fig. 2, viewed from the right of the latter
- Fig. 4 is an'illustrative embodiment of an impedin'ient in accordance with the invention
- Fig. 5 is a further illustrative embodiment of an impediment in accordance with .the inven: tion;
- Fig. 6 shows a part of the. combustion shaft with the impediment illustrated in Fig. 5.
- the intimate mixture of the gas with the combustionair may be secured in various ways and by various means, without departing from. the spirit of the invention.
- the mixture of gas and combustion air can be secured in the simplest way by providing openings in the inside conduit through which the medium flowing through the outer conduit is sucked by the. action of the medium flowing through the inner conduit. Parts of the gases flowing through the outer conduit thus penetrate into the innermost core, of the inner gas'conduit,
- the gas mixture 0 supply conduit 2 opens into the combustion shaft 1 of the Cowper.
- the combustion gas is sucked through the gas conduit 3.
- Tim air supply conduit 4 is inserted in the/usual manner within the gas conduit 3.
- the combustion air is supplied under pressure by a fan '9a. driven by a To change over the Cowper from the heating period' to' the draft period there are used, as usual, quickly operable slide dampers 5 and 6, the former of which closes oil! the Cowper from the gas and air mixture, whereas the slide 6 serves to shut oi! the gas conduit itself.
- said means comprises ports 11 provided in the wall of the inner conduit 4, which in the illustrative embodiment of the invention supplies the combustion air.
- ports 11 are proorwardly inclined pipes 12 which are preferably welded in place.
- the current of combustion air driven through the air supply conduit 4 by operation of the fan 9a sucks the gas from the conduit 3 through said pipes 12 directly forwardly towards the centre of the combustion air stream, said gas thus penetrating to the innermost core of said combustion air stream.
- An extremely intimate mixture of the gas with the combustion air is thus secured.
- a spreading cone 10 having guiding surfaces 10a, may be provided.
- the mixture of gas and air then flows through the gas mixture supply conduit 2 into the combustion shaft of the Cowper.
- said grid comprises a plurality of vertical rods vd spaced apart preferably a distance greater than the width of the rods.
- Said rods may be of any suitable material, preferably of iron, and their spacing from each other may be equal to a multiple of their width.
- a combustion shaft a gas and air mixture conduit opening at its inner-end into said combustion shaft; a. gas supply tube and an air supply tube concentrically positioned for injecting a mixture of gas and air into said conduit through its outer end; means to-force air from atmosphere through said air tube; and a grid extending transversely of the opening between the. inner end of said conduit and'said combustion shaft, said grid being of relatively .large mesh so as not to impair materially .the volume of flow of the gas and air mixture to the combustion" shaft.
- a combustion shaft in combination, a combustion shaft; a gas supply conduit therefor; an air supply conduit for said combustion shaft; means cooperating with said conduits intimately to mix the gas and air sup-' bination, a combustion shaft; a gas supply conduit therefo an air supply conduit for said combustion shaft; means cooperating with said regions of lower velocity of flow of the gas and' conduits intimately t i th gas and air ,125
- the grid rods d3 radiate from a common central point and are preferably held together at their inner ends by a dispersion cone e having its apex directed towards the centre of the flow in the gas mixture supply conduit 2. Said dispersion cone effects a still better and wider dispersion of the mixture of gas and air over a greater cross-sectional area within the combustion shaft 1.
- a combustion shaft ; a gas supply conduit therefor; an air supply conduit for said combustion shaft; means cooperating with said bination, a combustion shaft; a conduit opening at its inner end into said combustion shaft; means comprising gas and air supply tubes at the outer end of said conduit to inject a mixture of gas and air through said" conduit into said combustion shaft; and means adjacent the inner end of said conduit and presenting upon one side areas of impact to the gas and air mixture flowing to the combustion shaft and upon the opposite side areas of adhesion for' the flame when said mixture is ignited, said areas being spaced apart sufliciently not to impair materially the volume of flow of said gas and air mixtureto said combustion shaft.
- a combustion shaft for injecting a mixture of gas and air into said, combustion shaft; and means spaced from the discharge openings of said tubes in the direction of said combustion shaft and presenting areas of impact to the gas and air mixture flowing with high velocity to said combustion shaft to form in the lee of said areas, zones ofreduced velocity in which the mixture can ignite without the flame being torn awayby the high velocity flow of said mixture, said areas being spaced apart sufliciently not to impair materially the volume of flow ofv said gas and air mixture to said combustion shaft.
- a combustion shaft for injecting a mixture of gas and air into said combustion shaft; and a grid spaced from the discharge openings of said tubes in the direction of said combustion shaft, the grid members being spaced apart sufficiently not to impair materially the volume of flow of the gas and air mixture to said combustion shaft and being of a cross section to form in the lee of said members zones of reduced velocity in which the gas and air mixture can ignite without the flame being torn away by the high velocity of the flow of said mixture.
- a combustion shaft a conduit opening gas and air through said conduit into said combustion shaft; and a grid comprising a plurality of superposed intersecting bars, said bars being spaced apart sufiiciently not to impair materially the volume of flow of said gas and air mixture to said combustion shaft, said grid being positioned across the opening of said conduit into said shaft.
- a combustion shaft means to inject a mixture of gas and air into said combustion shaft; and means disposed in a plane transversely of the flow of said gas and air mixture andpresenting areas of impact to said gas and air mixture as it flows with high velocity to said combustion shaft, to form in the lee of said areas zones of reduced velocity in which said gasand air mixture can ignite without the flame being torn away by the high velocity of the flow of said mixture, said areas being spaced apart sufliciently not to impair materially the volume of flow of said gas and air mixture to said combustion shaft.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Description
June 12, 1934. wU 1,963,009
' HI :H POWER GAS HEATING APPARATUS/ Filed Dec. 8, 19:0 ZSheets-Sheet 1 lnvenfor'a' I I l men-rowan GAS HEATING APPARATUS Guido Wiinsch, erna-si ma, Germany Application llecember 8; 1930. Serial In Germany December 9, 192
10 Claims. (Cl. 158-109) 'I'hisinvention relates to high-power gas heating apparatus and more particularly to highpower gas burners for the well-known Cowper apparatus of blast furnaces, for example. Cowper apparatus in use today for blast furnaces are very high-powered and require as much as 2000 or even more cubic meters of gas per hour. Such large quantities of gas can be fed or supplied only where the' gas is blown into the combustion shaft of the Cowper under much higher pressure than heretofore. however, ,presents the serious diflieulty that the gas and air mixture, by reason of the high pressure used,
acquires much too great a velocity relative to the igniting speed of the gas mixture. Asa result the flame cannot ignite quietly adhering to the opening of the gas and air mixture supply conduit in the combustion shaft, but continuously breaks or is torn away from said opening, thus giving rise to the popping orsputtering of the flame so injurious to the operation of the apparatus.
The invention has for its object, among other things, to overcome this difliculty by providing for a much more intimate admixture of the gases with ,the air, whereby the igniting speed of the gases is materially increased, and also preferably by providing a suitable impediment or impediments infront of the opening of the supply or feed conduit of the gas-air mixture into the combustion shaft. The gas-air mixture -breaks against said impediments, in the lee of which there is thus formeda zone, or zones, of lower velocity, lower than the speed of ignition. Furthermore, behind the impediments the flow or stream of the gas-air mixture rapidly spreads over a materially greater crosssectional area.- The mean speed of flow thus drops below the igniting speed. allowing the flame to ignite quietly in the lee of the impediments. A'quiet flame filling the combustion shaft is thus secured without the impediments diminishing in any degree the amount 01 the air and gas mixture supplied.
The invention and its aims and objects will be best understood from the following description,
purposes, the true scope of the. invention being more particularly pointed out in the appended claims.
Iii the drawings:
Fig. 1 shows a Cowper'of conventional con-.
"inotor 9 (see Fig. 1).
taken in connection with the accompanying drawings of one embodiment of the invention herein described and shown for illustrative 'struction with an illustrative embodiment of the invention, partly in section;
Fig. 2 is a longitudinal sectional elevation of the air conduit, with the inserted gas pipes;
Fig. 3 is an end view of the construction shown. 9 in Fig. 2, viewed from the right of the latter Fig. 4 is an'illustrative embodiment of an impedin'ient in accordance with the invention;
Fig. 5 is a further illustrative embodiment of an impediment in accordance with .the inven: tion;
Fig. 6 shows a part of the. combustion shaft with the impediment illustrated in Fig. 5.
The intimate mixture of the gas with the combustionair may be secured in various ways and by various means, without departing from. the spirit of the invention. In the Cowpers commonly used today the combustion air conduit and the gas conduit .are surrounded one by the other at their opening into the mixing chamber in such manner that .one conduit opens into the other in form of a suction jet. In the case of Cowper burners of this type the mixture of gas and combustion air can be secured in the simplest way by providing openings in the inside conduit through which the medium flowing through the outer conduit is sucked by the. action of the medium flowing through the inner conduit. Parts of the gases flowing through the outer conduit thus penetrate into the innermost core, of the inner gas'conduit,
'thus producing a much more intimate mixture than it was possible to produce heretofore.
Referring to the drawings, the gas mixture 0 supply conduit 2 opens into the combustion shaft 1 of the Cowper. The combustion gas is sucked through the gas conduit 3. Tim air supply conduit 4 is inserted in the/usual manner within the gas conduit 3. The combustion air is supplied under pressure by a fan '9a. driven by a To change over the Cowper from the heating period' to' the draft period there are used, as usual, quickly operable slide dampers 5 and 6, the former of which closes oil! the Cowper from the gas and air mixture, whereas the slide 6 serves to shut oi! the gas conduit itself.
For the operation of said slide dampers 5 and 6 there are provided a crank 7 and a hand 1 wheel 8. a p The parts described in the above paragraph are of conventional and well known construction and need not be more fully described.
I will now describe means for securing the vided more intimate mixture of the combustion gases. In the illustrative embodiment of the invention said means comprises ports 11 provided in the wall of the inner conduit 4, which in the illustrative embodiment of the invention supplies the combustion air. In said ports 11 are proorwardly inclined pipes 12 which are preferably welded in place. The current of combustion air driven through the air supply conduit 4 by operation of the fan 9a sucks the gas from the conduit 3 through said pipes 12 directly forwardly towards the centre of the combustion air stream, said gas thus penetrating to the innermost core of said combustion air stream. An extremely intimate mixture of the gas with the combustion air is thus secured. For the better distribution of the stream of combustion air within its conduit a spreading cone 10, having guiding surfaces 10a, may be provided. The mixture of gas and air then flows through the gas mixture supply conduit 2 into the combustion shaft of the Cowper.
- While the ports 11 of the air supply conduit, by effecting a much more intimate mixture of the gas with the combustion air, materially in crease or raise the igniting speed of the mixture, the velocity of the flow of the gas and air mixture still exceeds said igniting speed, so that a quiet flame does not yet form adhering -to the opening of the supply conduit 2 into the combustion shaft 1. Means are accordingly provided in accordance with the invention for this purpose,'said means in the illustrative embodiment of the invention comprising impediments as already set forth. Said impediments :may conveniently take the form of a grid. In
the illustrative form of grid shown in Fig. 4 said grid comprises a plurality of vertical rods vd spaced apart preferably a distance greater than the width of the rods. Said rods may be of any suitable material, preferably of iron, and their spacing from each other may be equal to a multiple of their width. Under some conditions it is preferable to provide a second grid situated centrally of the grid (1, said second -grid consisting of a plurality of rods d1, d2,
In the lee of the grid rods there are formedcombustion shaft and extending transversely of the inner opening of said conduit, said grid being of relatively large mesh so as not to impair materially the, volume of flow of the gas and air mixture to the combustion shaft.
. 2. In apparatusof the class described,- in combination, a combustion shaft; a gas and air mixture conduit opening at its inner-end into said combustion shaft; a. gas supply tube and an air supply tube concentrically positioned for injecting a mixture of gas and air into said conduit through its outer end; means to-force air from atmosphere through said air tube; and a grid extending transversely of the opening between the. inner end of said conduit and'said combustion shaft, said grid being of relatively .large mesh so as not to impair materially .the volume of flow of the gas and air mixture to the combustion" shaft.
3. In apparatus of the class described, in combination, a combustion shaft; a gas supply conduit therefor; an air supply conduit for said combustion shaft; means cooperating with said conduits intimately to mix the gas and air sup-' bination, a combustion shaft; a gas supply conduit therefo an air supply conduit for said combustion shaft; means cooperating with said regions of lower velocity of flow of the gas and' conduits intimately t i th gas and air ,125
air mixture, in which the flame can ignite. By means of the grid the air and gas mixture is relatively quickly distributed over a wider crosssectional area, so that withina short distance at the 'rear of the grid the mean velocity of flow of the air and gas mixture will be below the igniting speed of said gas mixture, so that the flame that ignites-against the grid rods twill burn quietly without being torn away therefrom. Y a
In the illustrative embodiment of the grid shown in Figs. 5 and 6, the grid rods d3 radiate from a common central point and are preferably held together at their inner ends bya dispersion cone e having its apex directed towards the centre of the flow in the gas mixture supply conduit 2. Said dispersion cone effects a still better and wider dispersion of the mixture of gas and air over a greater cross-sectional area within the combustion shaft 1.
I am aware that my invention may be embodied in other specific forms without departing from the spirit or essential attributes of said invention, and I therefore desire the present embodiment to be considered in all respec s plied thereby, in their passage to said combustion shaft; and a grid extending transversely of the fiow of the gas and air mixture at its entrance into. said combustion shaft, said grid being of relatively large mesh so as not to impair materially the volume of flow of the gas and air mixture to said combustion shaft.
5. In apparatus of. the class described, in i,
combination, a combustion shaft; a gas supply conduit therefor; an air supply conduit for said combustion shaft; means cooperating with said bination, a combustion shaft; a conduit opening at its inner end into said combustion shaft; means comprising gas and air supply tubes at the outer end of said conduit to inject a mixture of gas and air through said" conduit into said combustion shaft; and means adjacent the inner end of said conduit and presenting upon one side areas of impact to the gas and air mixture flowing to the combustion shaft and upon the opposite side areas of adhesion for' the flame when said mixture is ignited, said areas being spaced apart sufliciently not to impair materially the volume of flow of said gas and air mixtureto said combustion shaft.
7. In apparatus of the class described, in combination, a combustion shaft; gas and air supply tubes for injecting a mixture of gas and air into said, combustion shaft; and means spaced from the discharge openings of said tubes in the direction of said combustion shaft and presenting areas of impact to the gas and air mixture flowing with high velocity to said combustion shaft to form in the lee of said areas, zones ofreduced velocity in which the mixture can ignite without the flame being torn awayby the high velocity flow of said mixture, said areas being spaced apart sufliciently not to impair materially the volume of flow ofv said gas and air mixture to said combustion shaft.
8. In apparatus of the class described, in combination, a combustion shaft; gas and air supply tubes for injecting a mixture of gas and air into said combustion shaft; and a grid spaced from the discharge openings of said tubes in the direction of said combustion shaft, the grid members being spaced apart sufficiently not to impair materially the volume of flow of the gas and air mixture to said combustion shaft and being of a cross section to form in the lee of said members zones of reduced velocity in which the gas and air mixture can ignite without the flame being torn away by the high velocity of the flow of said mixture.
9. In apparatus of the class described, in combination, a combustion shaft; a conduit opening gas and air through said conduit into said combustion shaft; and a grid comprising a plurality of superposed intersecting bars, said bars being spaced apart sufiiciently not to impair materially the volume of flow of said gas and air mixture to said combustion shaft, said grid being positioned across the opening of said conduit into said shaft.
10. In apparatus of the class described, in combination, a combustion shaft; means to inject a mixture of gas and air into said combustion shaft; and means disposed in a plane transversely of the flow of said gas and air mixture andpresenting areas of impact to said gas and air mixture as it flows with high velocity to said combustion shaft, to form in the lee of said areas zones of reduced velocity in which said gasand air mixture can ignite without the flame being torn away by the high velocity of the flow of said mixture, said areas being spaced apart sufliciently not to impair materially the volume of flow of said gas and air mixture to said combustion shaft.
GUIDO wimscn.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1963009X | 1929-12-09 |
Publications (1)
Publication Number | Publication Date |
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US1963009A true US1963009A (en) | 1934-06-12 |
Family
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Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US500969A Expired - Lifetime US1963009A (en) | 1929-12-09 | 1930-12-08 | High-power gas heating apparatus |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500787A (en) * | 1944-12-15 | 1950-03-14 | Orr & Sembower Inc | Fluid fuel burner apparatus for effecting diffusion combustion |
US3037553A (en) * | 1957-10-29 | 1962-06-05 | Utah Hydro Corp | Gas burner |
US3195872A (en) * | 1963-02-04 | 1965-07-20 | Zimmermann & Jansen Gmbh | Burner constructions for hot blast stoves |
US3216709A (en) * | 1961-09-21 | 1965-11-09 | Jones & Laughlin Steel Corp | Blast gas heating |
EP0019386A2 (en) * | 1979-05-02 | 1980-11-26 | Atlantic Richfield Company | Method and apparatus for flame modification to reduce NOx-emissions |
-
1930
- 1930-12-08 US US500969A patent/US1963009A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500787A (en) * | 1944-12-15 | 1950-03-14 | Orr & Sembower Inc | Fluid fuel burner apparatus for effecting diffusion combustion |
US3037553A (en) * | 1957-10-29 | 1962-06-05 | Utah Hydro Corp | Gas burner |
US3216709A (en) * | 1961-09-21 | 1965-11-09 | Jones & Laughlin Steel Corp | Blast gas heating |
US3195872A (en) * | 1963-02-04 | 1965-07-20 | Zimmermann & Jansen Gmbh | Burner constructions for hot blast stoves |
EP0019386A2 (en) * | 1979-05-02 | 1980-11-26 | Atlantic Richfield Company | Method and apparatus for flame modification to reduce NOx-emissions |
EP0019386A3 (en) * | 1979-05-02 | 1981-06-03 | Atlantic Richfield Company | Method and apparatus for flame modification to reduce NOx-emissions |
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