US1647675A - Burner for gaseous and powderous solid fuel - Google Patents
Burner for gaseous and powderous solid fuel Download PDFInfo
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- US1647675A US1647675A US65490A US6549025A US1647675A US 1647675 A US1647675 A US 1647675A US 65490 A US65490 A US 65490A US 6549025 A US6549025 A US 6549025A US 1647675 A US1647675 A US 1647675A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion simultaneously or alternately of gaseous or liquid or pulverulent fuel
- F23D17/005—Burners for combustion simultaneously or alternately of gaseous or liquid or pulverulent fuel gaseous or pulverulent fuel
Definitions
- My invention relates to improvements in burners for powderous solid fuel, and the object of the improvements is to provide a burner by means of which low grade solid fuel may be economically burnt.
- my invention consists in providing a burner having a supply of a combustible gas or gases in addition to the supply of powderous solid fuel. I have found that when thus burning gaseous fuel together with solid fuel the solid fuel is completely burnt and produces a short flame thus gnsuring economy in the combustion of the uel.
- Fig. 1 is a sectional elevation showing the burner the section being taken along the line 11 of Figure 2,
- Fig. 2 is a sectional View taken on the line 22 of Fig. 1, p
- Fig. 3 is 'a development in section of the gas and air passages of the burner, the said section being taken on the line 3-3 of Fig. 2,
- Fig. 4 is a sectional elevation showing a modification of the burner, the section being taken in the same manner as Figure l, and
- Fig. 5 is a detail sectional view taken on the line 5-5 of Fig. 4 and showing the arrangement of the tangential passages for supplying compressed air to the passage for supplying solid fuel to the burner.
- Figure 6 is a horizontal cross-section taken along the line 66 of Figure 1, and showing the helical arrangement of the passages.
- the burner shown in the drawings is particularly adapted for burnin solid fuel, such as powderous coal containmg little gas, partly coked coal, the combustible deposit from flues of locomotives and other fire places, and the like. But I wish it to be understood that the burner may also be used for burning poor or rich gas without supplying solid fuel thereto.
- solid fuel such as powderous coal containmg little gas, partly coked coal, the combustible deposit from flues of locomotives and other fire places, and the like.
- the burner may also be used for burning poor or rich gas without supplying solid fuel thereto.
- m improved burner in the example shown in Figs. 1 to 3, and 6, m improved burnerconsists of a hollow member composed of a comparatively short cylindrical ortion a a tapering portion a, and a cylin rical portion a. At its top the said member is closed by a head In, and below the said head it is provided with a transverse partition 6, the head is and the partition e including an annual chamber it. Further, the hollowmember is provided with an axial passage 6 having an outwardly flaring delivery end 6 The .delivery end of the passage Z) is partly closed by a cone 6 connected with the portion 6 by spiral or helical ribs 0.
- the passage 6 is used for the supply of the solid powderous fuel, and the said fuel is delivered from the passage towards the wall a of the hollow member and into the combustion chamber F thereof.
- the fuel delivere from the passage 6 is whirled around thus insuring complete mixture of the solid fuel, the gaseous fuel and the air for sup orting combustion delivered into the com ustion chamber in the manner now to be described.
- the annular chamber 11. is made integral with a tubular inlet g, and the top part of the tapering portion a of the hollow memher is provided with an annular chamber d having a tubular inlet, 03.
- the annular chamber included between the wall a of the hollow member is 'provided with helical ribs r W, W, 7 extending from the pipe I) to the Wall a and dividin the said annular chamher into three sets of helical passages p 79 12
- the ribs 1'", 'r" are extended upwardly and through the annular chamber h, and the passages p included'between the said ribs are open to the outer air, and they are ada ted to be closed more or less by means 0 an annular slide m provided on the head is.
- the passages p are closed at" their top ends as against the chamber h, and they communicate through orts made in the wall a with the annular 0 amd and the inlet d.
- the passages p are narrow as compared to the passages p and p If it is desired to burn low grade solid fuel and low grade gaseous fuel by means of the burner, the powderous solid fuel is supplied by means of compressed air through the axial passage 6, the low grade gas is supplied through the inlet d, the annular chamber ti the ports q and the passages 12?, compressed air is supplied through the inlet 9, the chamber h and the passages p and the passages p are closed by means of the slide m.
- the gas delivered into the combustion chamber F is burnt and develops a heat sufficient to burn the low grade solid fuel delivered from the axial passage 6, a rapid and complete combustion being insured by the whirling movement of the solid fuel, the gaseous fuel and the air for supporting combustion. Thus the fuel burns with a very short flame.
- the pipe I For operating the burner exclusively by means of gaseous fuel, the pipe I) is closed, and the gas is supplied through the inlet d and the passages 79 In case of a low grade gas compressed air is supplied through the inlet 9, the chamber h and the passages But for burning a high grade gas I open t e passages p thus admitting air under atmospheric pressure to the burner, the said air being taken in by suction produced by the gas delivered from the passages 12.
- the hollow member including the annular chamber 72. and the combustion chamber F is made in two sections, one section comprising the cylindrical wall a. and the top part of the tapering wall indicated in Fig. 4 by the letter a, and the other part comprising a jacketed tapering member A having an outwardly flaring delivery end A
- the tapering member A is adapted to be cooled by circulating cooling water through the annular chamber included between the inner tapering wall A and the jacket thereof the water inlet and outlet pipes not shown.
- the conical portion a is made integral with a rounded annular flange a by means of which it is supported on a base frame D, bolts a being provided for holding the flange a in position on the frame I).
- the frame I) is providedwitha flange a which is directed downwardly and curved'inwardly, the flanges a and a providing an annular rounded seat for'the top part of the member A.
- the said member A At its top the said member A is bulged outwardly so as to provide a rounded head A adapted for bear ing on the inner rounded face of the flanges a anda.
- jointing the bottom part A to the top part a at I am enabled to direct the bottom part A in lateral direction, which is desirable for example when using the biirner for internally heating rotary furnaces and for directing the flame to different parts of the said furnace.
- A" screwthreaded rod B is jointed by means of a spherical joint 13 to an eyeiB cast integral with the top part of the member A, so that the said rod can be rocked and rotated relatively to the said eye.
- the screw-threaded part of the said rod is passed through a nut C formed with laterally projecting trunnions C mounted in a bearing C cast integral with the frame D.
- the rod B car ries a hand wheel B By turning the rod B by means-of the said handwheel the main-.-
- Fig.4 1 have shown only one mechanism for rocking the member A, so that the member A can be rockedonly in one direction. But I wish it to be understood that I do not limit myself to this construction, and that I provide two setting mechanisms,- if it is desired to impart universal rocking movement to the member A.
- a burner comprising an outer casing, a central tubular passage, and three sets of passages therebetween, the passages of said sets being mutually interposed and located radially osaidtube','the passages of two sets communicating respectively with inlets for gas and air, and the passages of the third'set communicating with the outer air.
- a burner comprising an outer casing, a central tubular passage, and three sets of helical passages therebetween, the passages of said sets being mutually interposed and located radially of said tube, the passages of two sets communicatingrespectively with inlets for gas and air, and the passages of the third set communicating with the outer air.
- a burner comprising an outer casing
- a burner comprising an outer casing, a central tubular passage, an annular chamber therebetween at one end and three sets of helical passages therebetween adjoin ng said chamber, the passages of said sets being mutually interposed and arranged radially of said tube, one set communicating with said chamber, the second set communicating with a gas inlet, and the third set extending through said chamber and communicating with the outer air.
- a burner comprising an outer casing, a central tubular passage, an annular chamber therebetween at one end and three sets of passages therebetween adjoining said chamber, the passages of said sets being mutually interposed and arranged radially of said tube, one set communicating with said chamber, the second set communicating with a gas inlet, and the third set extending through said chamber and communicating with the outer air, said chamber also having communication with said central tubular passage through tangential nozzles inclined toward the delivery end of the burner.
- a burner comprising a hollow member having an axial passage for the delivery oi sages, an annular cham solid fuel, the delivery end of said passage having an outwardly flaring wall, means to conduct air under pressure into said passage in a direction tangential of the passage and towards the delivery end thereof, and helical passages around said axial passage for the delivery of gaseous fuel and air for supporting combustion.
- a burner comprising an outer casing and an axial passage therein for the delivery of solid fuel, the delivery end of said passage having an outwardly flaring wall, means to conduct air under pressureinto said passage in a direction tangential of the passage and toward the delivery end thereof, and helical passages around said axial passage formed by radial division of the space inside said outer casing, each third passage being in communication with said air conductmg means, each passage adjacent thereto on one side supplying gaseous fuel, and each passage therebetween being in communication with the outside air.
- a device for burning powderous solid fuel comprising in combination, a hollow casing, an axial tube therein and a plurality of radial vanes extending outward from'said axial tube, orming three sets of passages, an annular chamber within said casing at one end having a compressed air inlet and being in communication with one set of passages, pairs of said vanes extending through said chamber and forming passages in communication with the outside air, a second annular chamber adjacent said first chamber and having a gas inlet and being in communication with the third set of passages.
- a device for burning powderous solid fuel comprising in combination, a hollow casing, an axial tube therein and a plurality of radlal' vanes extending outward from said axial tube, forming three sets of pas- 1ng at one end having a compressed air inlet, and being in communication with one set of passages, pairs of said vanes extending through said chamber and forming passages in communication with the outside air, a second annular chamber adjacent'said first chamber and havin a gas inlet and being in communication with the third set of passages, said axial tube being formed with inclined tangential nozzles communicating with said first chamber whereby 'ets of air act onthe powderous fuel in said tube to give it a whirling motion.
- a device for burnlng powderous solid fuel comprising in combination, a hollow casing, an axial tube therein and a plurality of radlal vanes extending outward from sa1d axial tube, forming three sets of passages, an annular chamber within said casing at one end having a compressed air inlet.
- p rs Of said vanes extending through er within said casin combination, a substantially fusto-coni cal casing, an axial tube within said casing for supplying the powderous solid fuel, a transverse Wall forming an annular chamber surrounding said fuel passage and having an nlet for receiving compressed air, a plurality of radial helical vanes extending out- Ward from said axial tube and through said 4 Wall, forming three sets of passages one set in communication with the outside air, one set in communication with the annular chamber, and a third set; a cylindrical well outside said casing forming therewith a chamber having an inlet for receiving combustible gas, said chamber being in communication with said third set of passages.
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- General Engineering & Computer Science (AREA)
Description
Nov. 1, 1957.
2 Sheets-Sheet 1 Filed Oct. 28. 1925 Nov.'1, 1927.
W. VEDDER BURNER FOR GASEOUS AND POWDEROUS SOLID FUEL Filed 001;. 28, 1925 2 eets-Sheet 2 Patented Nov. 1, 1927.
UNITED'STATES PATENT OFFICE.
WILHELM VEDDER, OF ESSEN-ON-THE-RUHR, GERMANY.
BURNER FOR GASEOUS AND POWDEROUS SOLID FUEL.
Application filed October 28, 1925, Serial No. 85,490, and in Germany October 24, 1924.
My invention relates to improvements in burners for powderous solid fuel, and the object of the improvements is to provide a burner by means of which low grade solid fuel may be economically burnt. With this object in view my invention consists in providing a burner having a supply of a combustible gas or gases in addition to the supply of powderous solid fuel. I have found that when thus burning gaseous fuel together with solid fuel the solid fuel is completely burnt and produces a short flame thus gnsuring economy in the combustion of the uel.
I For the purpose of explaining the invention two examples embodying the same have been shown in the accompanying drawings, in which the same reference characters have been used in all the views to indicate corresponding parts. In said drawings,
Fig. 1, is a sectional elevation showing the burner the section being taken along the line 11 of Figure 2,
Fig. 2, is a sectional View taken on the line 22 of Fig. 1, p
Fig. 3, is 'a development in section of the gas and air passages of the burner, the said section being taken on the line 3-3 of Fig. 2,
Fig. 4, is a sectional elevation showing a modification of the burner, the section being taken in the same manner as Figure l, and
along the line 4-4 of Figure 5, and
Fig. 5, is a detail sectional view taken on the line 5-5 of Fig. 4 and showing the arrangement of the tangential passages for supplying compressed air to the passage for supplying solid fuel to the burner.
Figure 6 is a horizontal cross-section taken along the line 66 of Figure 1, and showing the helical arrangement of the passages.
The burner shown in the drawings is particularly adapted for burnin solid fuel, such as powderous coal containmg little gas, partly coked coal, the combustible deposit from flues of locomotives and other fire places, and the like. But I wish it to be understood that the burner may also be used for burning poor or rich gas without supplying solid fuel thereto.
In the example shown in Figs. 1 to 3, and 6, m improved burnerconsists of a hollow member composed of a comparatively short cylindrical ortion a a tapering portion a, and a cylin rical portion a. At its top the said member is closed by a head In, and below the said head it is provided with a transverse partition 6, the head is and the partition e including an annual chamber it. Further, the hollowmember is provided with an axial passage 6 having an outwardly flaring delivery end 6 The .delivery end of the passage Z) is partly closed by a cone 6 connected with the portion 6 by spiral or helical ribs 0. The passage 6 is used for the supply of the solid powderous fuel, and the said fuel is delivered from the passage towards the wall a of the hollow member and into the combustion chamber F thereof. By providin the spiral or helical ribs the fuel delivere from the passage 6 is whirled around thus insuring complete mixture of the solid fuel, the gaseous fuel and the air for sup orting combustion delivered into the com ustion chamber in the manner now to be described.
The annular chamber 11. is made integral with a tubular inlet g, and the top part of the tapering portion a of the hollow memher is provided with an annular chamber d having a tubular inlet, 03. The annular chamber included between the wall a of the hollow member is 'provided with helical ribs r W, W, 7 extending from the pipe I) to the Wall a and dividin the said annular chamher into three sets of helical passages p 79 12 The ribs 1'", 'r" are extended upwardly and through the annular chamber h, and the passages p included'between the said ribs are open to the outer air, and they are ada ted to be closed more or less by means 0 an annular slide m provided on the head is. Thus atmospheric air can be taken in through the passages 12*, the supply being controlled by the valve m. In some cases the'passages p, are entirely closed, as will be described hereinafter. As is shown in Fig. 2 the parts of the helical ribs 1', r passing through the chamber it do not extend to the wall a of the hollow, member, but to points a suitable distance away therefrom, and the said ends are connected by arcuate walls 7* thus providing arcuate passages it through which the parts of the annular chamber h communicate with the inlet passage g. i
The passages 17 provided between the ribs 1' and r open lnto the annular chamber It, so that the said passages communicate with the tubular inlet 9. The passages p are closed at" their top ends as against the chamber h, and they communicate through orts made in the wall a with the annular 0 amd and the inlet d. v
As is best shown in Fig. 3, the passages p are narrow as compared to the passages p and p If it is desired to burn low grade solid fuel and low grade gaseous fuel by means of the burner, the powderous solid fuel is supplied by means of compressed air through the axial passage 6, the low grade gas is supplied through the inlet d, the annular chamber ti the ports q and the passages 12?, compressed air is supplied through the inlet 9, the chamber h and the passages p and the passages p are closed by means of the slide m. The gas delivered into the combustion chamber F is burnt and develops a heat sufficient to burn the low grade solid fuel delivered from the axial passage 6, a rapid and complete combustion being insured by the whirling movement of the solid fuel, the gaseous fuel and the air for supporting combustion. Thus the fuel burns with a very short flame.
For burning coal dust or the like by means of a high grade gas, I'supply the high grade gas through the inlet g, the annular chamber hand the narrow passages 17 The air is admitted under pressure through the inlet (1 and the passages 37 while the solid fuel is supplied through the pipe 6. In case of a high grade gaseous fuel I may admit air under atmospheric pressure through the passages p in which case the inlet d and the passages p communicating therewith are not used.
For operating the burner exclusively by means of gaseous fuel, the pipe I) is closed, and the gas is supplied through the inlet d and the passages 79 In case of a low grade gas compressed air is supplied through the inlet 9, the chamber h and the passages But for burning a high grade gas I open t e passages p thus admitting air under atmospheric pressure to the burner, the said air being taken in by suction produced by the gas delivered from the passages 12.
The general construction of the modification shown in Figs. 4 and 5 is similar to the one described above, and similar letters of reference have been used to indicate corresponding parts, so that it is not necessary to repeat the general description of the burner. I i
The hollow member including the annular chamber 72. and the combustion chamber F is made in two sections, one section comprising the cylindrical wall a. and the top part of the tapering wall indicated in Fig. 4 by the letter a, and the other part comprising a jacketed tapering member A having an outwardly flaring delivery end A The tapering member A is adapted to be cooled by circulating cooling water through the annular chamber included between the inner tapering wall A and the jacket thereof the water inlet and outlet pipes not shown. I
have foundthat by thus cooling the member A providing the wall of the combustion chamber the wear of the said member by the heat of the flame is reduced, and further, by cooling the combustible mixture ignition of the gas flowing through the helical passages is avoided' Near its bottom end the conical portion a is made integral with a rounded annular flange a by means of which it is supported on a base frame D, bolts a being provided for holding the flange a in position on the frame I). The frame I) is providedwitha flange a which is directed downwardly and curved'inwardly, the flanges a and a providing an annular rounded seat for'the top part of the member A. At its top the said member A is bulged outwardly so as to provide a rounded head A adapted for bear ing on the inner rounded face of the flanges a anda. By thus jointing the bottom part A to the top part a at I am enabled to direct the bottom part A in lateral direction, which is desirable for example when using the biirner for internally heating rotary furnaces and for directing the flame to different parts of the said furnace. For setting the member A in the desired position the following mechanism is provided: A" screwthreaded rod B is jointed by means of a spherical joint 13 to an eyeiB cast integral with the top part of the member A, so that the said rod can be rocked and rotated relatively to the said eye. The screw-threaded part of the said rod is passed through a nut C formed with laterally projecting trunnions C mounted in a bearing C cast integral with the frame D. The rod B car: ries a hand wheel B By turning the rod B by means-of the said handwheel the main-.-
her A can be rocked from the position shown in Fig. 4 in full lines for example into the position shown in broken lines. In Fig.4 1 have shown only one mechanism for rocking the member A, so that the member A can be rockedonly in one direction. But I wish it to be understood that I do not limit myself to this construction, and that I provide two setting mechanisms,- if it is desired to impart universal rocking movement to the member A.
In the construction shown in Figs. 4 and 5 the helical ribs 0 and the cone b shown in Fig. 1 are omitted, and whirling movement is imparted to the powderous fuel by means of jets of compressed air thrown into the pipe I) in tangential direction through tangential passages t, as is best shown in Fig. 5. These passages are also inclined so as to direct the jets toward the delivery end of the pipe I), as shown in Figure 4. By thus whirling .the powderous fuel around within i is thoroughly admixed with the gas and air.
While in describing the invention reference has been made to two particular ex amples embodying the same I wish it to be understood that my invention is not limited to the constructions shown in the drawings, and that various changes may be made in the general arrangement of the apparatus and the construction of its parts without departing from the invention.
I claim:
1. A burner, comprising an outer casing, a central tubular passage, and three sets of passages therebetween, the passages of said sets being mutually interposed and located radially osaidtube','the passages of two sets communicating respectively with inlets for gas and air, and the passages of the third'set communicating with the outer air.
2. A burner, comprising an outer casing, a central tubular passage, and three sets of helical passages therebetween, the passages of said sets being mutually interposed and located radially of said tube, the passages of two sets communicatingrespectively with inlets for gas and air, and the passages of the third set communicating with the outer air.
3. A burner, comprising an outer casing,
' a central tubular passage, an annular chamber therebetween at one end and three sets of passages therebetween adjoining said chamber, the passages of said sets beingmutually interposed and arranged radially of said tube, one set communicating with said chamber, the second set communicating with a gas inlet, and the third set extending through said chamber and communicating wit-h the outer air.
4"." A burner, comprising an outer casing, a central tubular passage, an annular chamber therebetween at one end and three sets of helical passages therebetween adjoin ng said chamber, the passages of said sets being mutually interposed and arranged radially of said tube, one set communicating with said chamber, the second set communicating with a gas inlet, and the third set extending through said chamber and communicating with the outer air.
5. A burner, comprising an outer casing, a central tubular passage, an annular chamber therebetween at one end and three sets of passages therebetween adjoining said chamber, the passages of said sets being mutually interposed and arranged radially of said tube, one set communicating with said chamber, the second set communicating with a gas inlet, and the third set extending through said chamber and communicating with the outer air, said chamber also having communication with said central tubular passage through tangential nozzles inclined toward the delivery end of the burner.
6. A burner,comprising a hollow member having an axial passage for the delivery oi sages, an annular cham solid fuel, the delivery end of said passage having an outwardly flaring wall, means to conduct air under pressure into said passage in a direction tangential of the passage and towards the delivery end thereof, and helical passages around said axial passage for the delivery of gaseous fuel and air for supporting combustion.
7. A burner comprising an outer casing and an axial passage therein for the delivery of solid fuel, the delivery end of said passage having an outwardly flaring wall, means to conduct air under pressureinto said passage in a direction tangential of the passage and toward the delivery end thereof, and helical passages around said axial passage formed by radial division of the space inside said outer casing, each third passage being in communication with said air conductmg means, each passage adjacent thereto on one side supplying gaseous fuel, and each passage therebetween being in communication with the outside air.
8. A device for burning powderous solid fuel, comprising in combination, a hollow casing, an axial tube therein and a plurality of radial vanes extending outward from'said axial tube, orming three sets of passages, an annular chamber within said casing at one end having a compressed air inlet and being in communication with one set of passages, pairs of said vanes extending through said chamber and forming passages in communication with the outside air, a second annular chamber adjacent said first chamber and having a gas inlet and being in communication with the third set of passages.
9. A device for burning powderous solid fuel, comprising in combination, a hollow casing, an axial tube therein and a plurality of radlal' vanes extending outward from said axial tube, forming three sets of pas- 1ng at one end having a compressed air inlet, and being in communication with one set of passages, pairs of said vanes extending through said chamber and forming passages in communication with the outside air, a second annular chamber adjacent'said first chamber and havin a gas inlet and being in communication with the third set of passages, said axial tube being formed with inclined tangential nozzles communicating with said first chamber whereby 'ets of air act onthe powderous fuel in said tube to give it a whirling motion.
10. A device for burnlng powderous solid fuel, comprising in combination, a hollow casing, an axial tube therein and a plurality of radlal vanes extending outward from sa1d axial tube, forming three sets of passages, an annular chamber within said casing at one end having a compressed air inlet. and being in communication with one set of passages: p rs Of said vanes extending through er within said casin combination, a substantially fusto-coni cal casing, an axial tube within said casing for supplying the powderous solid fuel, a transverse Wall forming an annular chamber surrounding said fuel passage and having an nlet for receiving compressed air, a plurality of radial helical vanes extending out- Ward from said axial tube and through said 4 Wall, forming three sets of passages one set in communication with the outside air, one set in communication with the annular chamber, and a third set; a cylindrical well outside said casing forming therewith a chamber having an inlet for receiving combustible gas, said chamber being in communication with said third set of passages.
In testimony whereof I hereunto aflix my signature.
WILl-IELM VEDDER.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1647675X | 1924-10-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1647675A true US1647675A (en) | 1927-11-01 |
Family
ID=7738159
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US65490A Expired - Lifetime US1647675A (en) | 1924-10-24 | 1925-10-28 | Burner for gaseous and powderous solid fuel |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1647675A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2616488A (en) * | 1951-05-05 | 1952-11-04 | California Portland Cement Co | Fuel burner |
| US2627307A (en) * | 1950-07-24 | 1953-02-03 | Brassert & Co | Concentric gas and air burner |
| US2638974A (en) * | 1947-01-24 | 1953-05-19 | Ralph C Brierly | Fuel burner diffuser |
| US2823628A (en) * | 1953-01-21 | 1958-02-18 | Babcock & Wilcox Co | Multi-fuel burner |
| US3236279A (en) * | 1960-10-07 | 1966-02-22 | Maschf Augsburg Nuernberg Ag | Combustion apparatus for both gaseous and non-gaseous fuels |
| US3265114A (en) * | 1964-07-20 | 1966-08-09 | Gen Dynamics Corp | Ignitor-burner assembly |
| US4610136A (en) * | 1982-05-06 | 1986-09-09 | Abom Jan J V | Device for ignition of the powder in powder engines and powder-operated turbine engines |
| US5415114A (en) * | 1993-10-27 | 1995-05-16 | Rjc Corporation | Internal air and/or fuel staged controller |
-
1925
- 1925-10-28 US US65490A patent/US1647675A/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2638974A (en) * | 1947-01-24 | 1953-05-19 | Ralph C Brierly | Fuel burner diffuser |
| US2627307A (en) * | 1950-07-24 | 1953-02-03 | Brassert & Co | Concentric gas and air burner |
| US2616488A (en) * | 1951-05-05 | 1952-11-04 | California Portland Cement Co | Fuel burner |
| US2823628A (en) * | 1953-01-21 | 1958-02-18 | Babcock & Wilcox Co | Multi-fuel burner |
| US3236279A (en) * | 1960-10-07 | 1966-02-22 | Maschf Augsburg Nuernberg Ag | Combustion apparatus for both gaseous and non-gaseous fuels |
| US3265114A (en) * | 1964-07-20 | 1966-08-09 | Gen Dynamics Corp | Ignitor-burner assembly |
| US4610136A (en) * | 1982-05-06 | 1986-09-09 | Abom Jan J V | Device for ignition of the powder in powder engines and powder-operated turbine engines |
| US5415114A (en) * | 1993-10-27 | 1995-05-16 | Rjc Corporation | Internal air and/or fuel staged controller |
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