US3076642A - Injection devices - Google Patents
Injection devices Download PDFInfo
- Publication number
- US3076642A US3076642A US62273A US6227360A US3076642A US 3076642 A US3076642 A US 3076642A US 62273 A US62273 A US 62273A US 6227360 A US6227360 A US 6227360A US 3076642 A US3076642 A US 3076642A
- Authority
- US
- United States
- Prior art keywords
- duct
- tube
- supply means
- outlet
- outer tube
- 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
Links
- 238000002347 injection Methods 0.000 title description 8
- 239000007924 injection Substances 0.000 title description 8
- 239000000126 substance Substances 0.000 claims description 11
- 239000012530 fluid Substances 0.000 claims description 10
- 239000000446 fuel Substances 0.000 claims description 10
- 239000007788 liquid Substances 0.000 claims description 3
- 239000012159 carrier gas Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 230000008439 repair process Effects 0.000 description 3
- 238000005336 cracking Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 101100128278 Mus musculus Lins1 gene Proteins 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000012265 solid product Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21B—MANUFACTURE OF IRON OR STEEL
- C21B7/00—Blast furnaces
- C21B7/16—Tuyéres
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21B—MANUFACTURE OF IRON OR STEEL
- C21B5/00—Making pig-iron in the blast furnace
- C21B5/001—Injecting additional fuel or reducing agents
-
- 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
- F23C1/00—Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel being either a fluid fuel or a solid fuel suspended in a carrier gas or air
- F23C1/02—Combustion apparatus specially adapted for combustion of two or more kinds of fuel simultaneously or alternately, at least one kind of fuel being either a fluid fuel or a solid fuel suspended in a carrier gas or air lump and liquid fuel
Definitions
- This invention relates in general to injection nozzles and has specific reference to a device for injecting fuel or any other liquid or fluidized, pulverulent or similar substance nto enclosures in which a relatively high temperature is maintained, for example in hot-blast tuyeres of blast-furnaces.
- the nozzle or innermost end of the burner or tuyere cannot be properly cooled (the slightest break in the supply of carrier and cooling fluid, whether gas or vapour, involves serious consequences), the fuel undergoes a certain amount of cracking, the solid product resulting from this cracking clogs the tuyere nozzle and this failure, while being already extremely detrimental per se due to the resulting stoppage, is further aggravated by other complications characterizing the hitherto used devices, which are set forth hereafter:
- the fuel may invade the network of carrier gas (compressed air, steam, etc.) or the carrier gas may force the fuel back to its supply tank and escape therefrom, with all the extremely serious consequences likely to arise in this case.
- carrier gas compressed air, steam, etc.
- an injector device of the type comprising an inner duct or tube connected with the source of the substance to be injected, and another duct or tube surrounding the rst one and adapted to carry the fluid for cooling and projecting the aforesaid substance.
- the device according to this invention is remarkable notably in that itycomprises a support or socket-forming piece disposed externally of the aforesaid enclosure and acting on the one hand as a means for mounting the jets through which the projection uid and the substance to be injected are introduced, and on the other hand as a means for assembling and mounting the ends of said ducts or tubes.
- This invention also contemplates providing the outer duct with ⁇ acentering and positioning member tting for example in the blast nozzle of the blast-furnace.
- the complete device is in the form of .a single unit ⁇ adapted to be mounted from the outside through the walls of the enclosure in which the injection is to be effected.
- FIGURE l is a longitudinal axial section of a device constructed according to the teachings of this invention.
- FIGURE 2 is a section taken across the line II-II of FIG. l;
- FIGURE 3 is another longitudinal axial section showing on a smaller scale the mounting of adevice of this invention in a blast-furnace, and
- FIGURE 4 is a section taken across the line IV-IV of FIG. 3.
- the injector device of this invention comprises an inner duct or tube 1 opening into any enclosure in which a high temperature is maintained, this inner duct or tube being secured by its oppositeend in a support-forming element or socket 2.
- this inner duct may be mounted by means of an intermediate tubular piece 3 fitting in a bore 4 formed in the support or socket 2.
- the tubular connecting piece 3 may be formed with an integral flange 5 tting on a ange 6 rigid with the inlet or feed pipe 7 for the substance to be projected into the enclosure.
- the tube 1 may be formed with a jet tone 8.
- the tube 1 is housed within an outer duct or tube 9 ⁇ of which the free end constitutes a narrower or tapered nozzle 10 converging toward the end of the inner duct.
- a kind of annular-sectioned nozzle having tapered and convergent inner walls is formed.
- the opposite end of the outer duct is secured in a bore 12 of the support-forming element or socket 2.
- This bore has a perpendicular orifice 13 having tted therein the delivery end of a pipe 14 supplying the injector with cooling and projection fluid.
- a centering piece 15 Disposed between the two ducts or tubes 1 and 9 is a centering piece 15 for example of cylindrical configuration which is formed with passages 16 (see also FIG. 2) opening into a central aperture of the piece and separated by radial partitions 17. The ends of these radial partitions 17 are in frictional contact with the inner tube or duct 9. Upstream, that is, at 18, the centering piece 15 is bevelled to form a kind of funnel 18. Of course, several centering pieces of this type may be aligned internally of the outer tube 9. Their number depends of course on the length of the injection pipe thus formed.
- the jet issuing from the pipe of this invention is shown only very diagrammatically in FIG. 1 in the form of two thick lines 19, 20, intersecting each other at 21, and of broken lines 22.
- the carrier or projection gas which may be itself a fuel, a combustion-assisting gas or an inert gas
- the carrier or projection gas gushes out from the tube end in the form of a conical convergent beam which becomes divergent after 21.
- the fuel even if it is not atomized, which is delivered from the tube 1 is carried along by the jet of carrier gas and atomized outside the injector.
- FIGS. 3 and 4 there is shown the use of an injector device according to this invention in the case of a blastfurnace.
- the reference numeral 23 designates the blast nozzle through which a hot blast is introduced in the direction of the arrow F.
- the outer tube 9 is provided with radial blades or fins 24, 25 and 26 (see FIG. 4) secured on the outer tube as a function of the length of the nozzle 23.
- these blades or lins may be secured in any suitable and desired manner on the outer walls of tube 9. Their shape and dimensions depend of course on the position to be given to the injection pipe inside said nozzle.
- Device for injecting fuel and other liquid and pulverulent substances into enclosures wherein high temperatures are prevailing, such as blast-furnaces and the like comprising at least one inner duct-means with an outlet, lirst supply means for said substances to be injected connected to said duct-means, at least one outer tube provided for carrying a uid intended to project said substance to be injected, said outer tube surrounding said duct-means, and being provided with a nozzle having conical inner walls converging toward the outlet of said inner ductmeans whereby said fluid is carried to gush out in the form of a conical convergent beam, said nozzle having an outlet substantially coplanar with the outlet of said inner duct-means, both outlets opening in the free air, second supply means for said fluid, said supply means being connected to said outer tube, a supporting means situated at the end of said tube and duct opposite said outlets, means for securing to -said supporting means said outer tube and said second supply means for slidably mounting on
- Device comprising at least one centering perforated element inserted between said duct and tube affording a relative sliding thereof with a smooth frictional contact, said element being hollowed to a funnel configuration on its upstream side and being provided with channels located concentrically around the longitudinal axis of said duct and tube and opened towards the said axis.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Description
Feb. 5, 1963 P. DHENEIN INJECTION DEVICES Filed oct. 12, Iseo United States Patent C) Claims priority, application France June 21, 1960 2 Claims. (Cl. 266--41) This invention relates in general to injection nozzles and has specific reference to a device for injecting fuel or any other liquid or fluidized, pulverulent or similar substance nto enclosures in which a relatively high temperature is maintained, for example in hot-blast tuyeres of blast-furnaces.
It is known that conventionalburners and atomizers or nozzles do not extend deeply inside the combustion chamber equipped therewith, and that the problem of cooling these devices, particularly their inner nozzle, is not very difcult.
However, when it is desired to cause an injection device to project deeply, for example more than 20 and notably nearly 80 as in the case of blast-furnaces, inside an enclosure in which a high temperature is maintained, serious diiliculties are encountered.
Firstly, the nozzle or innermost end of the burner or tuyere cannot be properly cooled (the slightest break in the supply of carrier and cooling fluid, whether gas or vapour, involves serious consequences), the fuel undergoes a certain amount of cracking, the solid product resulting from this cracking clogs the tuyere nozzle and this failure, while being already extremely detrimental per se due to the resulting stoppage, is further aggravated by other complications characterizing the hitherto used devices, which are set forth hereafter:
(a) These devices are not designed to permit the rapid and easy replacement of the clogged part (jet, atomizing chamber, fuel Afeed duct). The complete injection pipe assembly must be removed and replaced and this, notably when-these parts are mountedV in blast-furnace tuyeres, involves the dismantling of the jet support or socket and therefore the blast stoppage during the repair works.
y(b) On the other hand, if only the end of the jet is clogged, thus allowing the fuel to mix with the carrier lluid in the atomizing chamber thus separated from the outside, the fluid having the highest pressure ows back into the circuit of the other Huid.
Under these conditions, the fuel may invade the network of carrier gas (compressed air, steam, etc.) or the carrier gas may force the fuel back to its supply tank and escape therefrom, with all the extremely serious consequences likely to arise in this case.
It is the essential object of the present invention to avoid these various inconveniences by providing an injector device of the type comprising an inner duct or tube connected with the source of the substance to be injected, and another duct or tube surrounding the rst one and adapted to carry the fluid for cooling and projecting the aforesaid substance. The device according to this invention is remarkable notably in that itycomprises a support or socket-forming piece disposed externally of the aforesaid enclosure and acting on the one hand as a means for mounting the jets through which the projection uid and the substance to be injected are introduced, and on the other hand as a means for assembling and mounting the ends of said ducts or tubes. t .t
According to another feature of this invention, the outlet orices of the two ducts or tubes in the aforesaid enclosure aresubstantially coplanar. i
According to a further feature characterizing this invention there 'is disposed between the two ducts at least one centering perforated member whereby said ducts may ICC slide for example in smooth frictional engagement in each other for properly positioning them.
It is a further feature of this invention to constrict the front end of the outer duct on the inner duct to form a nozzle having tapered and convergent inner walls.
This invention also contemplates providing the outer duct with` acentering and positioning member tting for example in the blast nozzle of the blast-furnace.
The considerable advantages arising from the device of this invention will be readily apparent to anybody conversant withthe art. Firstly, the complete device is in the form of .a single unit `adapted to be mounted from the outside through the walls of the enclosure in which the injection is to be effected. Thus, for example, in
the case of a blast-furnace the injector assembly forming a kind of pipe is simply fitted in the walls of the blast nozzle. Y
It will be noted that when it is desired to carry out repairs or clean the device, it is not necessary to dismantle the outer duct since the inner duct can be removed very easily through the support-forming member. Thus, it is not necessary to stop the operation or effect more complicated dismantling steps.
Moreover, in case one or both of the outlet orifices of the two innerA and outer ducts were clogged, it is not possible that one of the fluids penetrates into the circuit of the other fluid, since these ducts have substantially the same length and ope-n into a. common plane.
Other features and advantages of this invention will appear as the following description proceeds with reference to the accompanying drawing illustrating diagrammatically by way of example a typical form of embodiment of the invention. In the drawings:
FIGURE l is a longitudinal axial section of a device constructed according to the teachings of this invention;
FIGURE 2 is a section taken across the line II-II of FIG. l;
FIGURE 3 is another longitudinal axial section showing on a smaller scale the mounting of adevice of this invention in a blast-furnace, and
FIGURE 4 is a section taken across the line IV-IV of FIG. 3.
In the form of embodiment illustrated the injector device of this invention comprises an inner duct or tube 1 opening into any enclosure in which a high temperature is maintained, this inner duct or tube being secured by its oppositeend in a support-forming element or socket 2. If desired, this inner duct may be mounted by means of an intermediate tubular piece 3 fitting in a bore 4 formed in the support or socket 2. If desired, the tubular connecting piece 3 may be formed with an integral flange 5 tting on a ange 6 rigid with the inlet or feed pipe 7 for the substance to be projected into the enclosure.
At its free end the tube 1 may be formed with a jet orice 8.
The tube 1 is housed within an outer duct or tube 9` of which the free end constitutes a narrower or tapered nozzle 10 converging toward the end of the inner duct. Thus, a kind of annular-sectioned nozzle having tapered and convergent inner walls is formed.
The opposite end of the outer duct is secured in a bore 12 of the support-forming element or socket 2. This bore has a perpendicular orifice 13 having tted therein the delivery end of a pipe 14 supplying the injector with cooling and projection fluid.
Disposed between the two ducts or tubes 1 and 9 is a centering piece 15 for example of cylindrical configuration which is formed with passages 16 (see also FIG. 2) opening into a central aperture of the piece and separated by radial partitions 17. The ends of these radial partitions 17 are in frictional contact with the inner tube or duct 9. Upstream, that is, at 18, the centering piece 15 is bevelled to form a kind of funnel 18. Of course, several centering pieces of this type may be aligned internally of the outer tube 9. Their number depends of course on the length of the injection pipe thus formed.
The jet issuing from the pipe of this invention is shown only very diagrammatically in FIG. 1 in the form of two thick lines 19, 20, intersecting each other at 21, and of broken lines 22. Due to the convergent shape of the end 1.0 of tube 9, the carrier or projection gas (which may be itself a fuel, a combustion-assisting gas or an inert gas) gushes out from the tube end in the form of a conical convergent beam which becomes divergent after 21. It will be noted that the fuel, even if it is not atomized, which is delivered from the tube 1 is carried along by the jet of carrier gas and atomized outside the injector.
It is clear that in case of failure the inner pipe 1 can be removed for repair or replacement without any difficulty. The repaired or new piece is replaced automatically, due notably to the centering piece 15.
In FIGS. 3 and 4 there is shown the use of an injector device according to this invention in the case of a blastfurnace. The reference numeral 23 designates the blast nozzle through which a hot blast is introduced in the direction of the arrow F.
The mounting of the injector of this invention is extremely simple. For the sake of constructional simplicity the outer tube 9 is provided with radial blades or fins 24, 25 and 26 (see FIG. 4) secured on the outer tube as a function of the length of the nozzle 23. Of course, these blades or lins may be secured in any suitable and desired manner on the outer walls of tube 9. Their shape and dimensions depend of course on the position to be given to the injection pipe inside said nozzle.
Although the present invention has been described in conjunction with a preferred embodiment, it is to be understood that modifications and variations may be resorted to without departing from the spirit and scope of the invention, as those skilled in the art will readily understand. Such modifications `and variations are considered to be within the purviews and scope of the invention and appended claims.
What I claim is:
1. Device for injecting fuel and other liquid and pulverulent substances into enclosures wherein high temperatures are prevailing, such as blast-furnaces and the like, comprising at least one inner duct-means with an outlet, lirst supply means for said substances to be injected connected to said duct-means, at least one outer tube provided for carrying a uid intended to project said substance to be injected, said outer tube surrounding said duct-means, and being provided with a nozzle having conical inner walls converging toward the outlet of said inner ductmeans whereby said fluid is carried to gush out in the form of a conical convergent beam, said nozzle having an outlet substantially coplanar with the outlet of said inner duct-means, both outlets opening in the free air, second supply means for said fluid, said supply means being connected to said outer tube, a supporting means situated at the end of said tube and duct opposite said outlets, means for securing to -said supporting means said outer tube and said second supply means for slidably mounting on said supporting means said duct and said rst supply means, the said supporting means with the duct, tube and -supply means forming an independant complete unit.
2. Device according to claim 1 comprising at least one centering perforated element inserted between said duct and tube affording a relative sliding thereof with a smooth frictional contact, said element being hollowed to a funnel configuration on its upstream side and being provided with channels located concentrically around the longitudinal axis of said duct and tube and opened towards the said axis.
References Cited in the tile of this patent UNITED STATES PATENTS 199,134 Witherbee Jan. 8, 1878 370,251 Field Sept. 20, 1887 1,629,045 Parker May 17, 1927 1,729,447 McKee sept. 24, 1929 2,338,623 Crowe Ian. 4, 1944 2,446,511 Kerry et al Aug. 3, 1948 2,829,960 Vogt Apr. 8, 1958
Claims (1)
1. DEVICE FOR INJECTING FUEL AND OTHER LIQUID AND PULVERULENT SUBSTANCES INTO ENCLOSURES WHEREIN HIGH TEMPERATURES ARE PREVAILING, SUCH AS BLAST-FURNACES AND THE LIKE, COMPRISING AT LEAST ONE INNER DUCT-MEANS WITH AN OUTLET, FIRST SUPPLY MEANS FOR SAID SUBSTANCES TO BE INJECTED CONNECTED TO SAID DUCT-MEANS, AT LEAST ONE OUTER TUBE PROVIDED FOR CARRYING A FLUID INTENDED TO PROJECT SAID SUBSTANCE TO BE INJECTED, SAID OUTER TUBE SURROUNDING SAID DUCT-MEANS, AND BEING PROVIDED WITH A NOZZLE HAVING CONICAL INNER WALLS CONVERGING TOWARD THE OUTLET OF SAID INNER DUCTMEANS WHEREBY SAID FLUID IS CARRIED TO GUSH OUT IN THE FORM OF A CONICAL CONVERGENT BEAM, SAID NOZZLE HAVING AN OUTLET SUBSTANTIALLY COPLANAR WITH THE OUTLET OF SAID INNER DUCT-MEANS, BOTH OUTLETS OPENING IN THE FREE AIR, SECOND SUPPLY MEANS FOR SAID FLUID, SAID SUPPLY MEANS BEING CONNECTED TO SAID OUTER TUBE, A SUPPORTING MEANS SITUATED AT THE END OF SAID TUBE AND DUCT OPPOSITE SAID OUTLETS, MEANS FOR SECURING TO SAID SUPPORTING MEANS SAID OUTER TUBE AND SAID SECOND SUPPLY MEANS FOR SLIDABLY MOUNTING ON SAID SUPPORTING MEANS SAID DUCT AND SAID FIRST SUPPLY MEANS, THE SAID SUPPORTING MEANS WITH THE DUCT, TUBE AND SUPPLY MEANS FORMING AN INDEPENDANT COMPLETE UNIT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR830839A FR1280598A (en) | 1960-06-21 | 1960-06-21 | Device for injecting liquid, semi-liquid, pulverulent, fluidized or the like substances |
Publications (1)
Publication Number | Publication Date |
---|---|
US3076642A true US3076642A (en) | 1963-02-05 |
Family
ID=8734005
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US62273A Expired - Lifetime US3076642A (en) | 1960-06-21 | 1960-10-12 | Injection devices |
Country Status (5)
Country | Link |
---|---|
US (1) | US3076642A (en) |
BE (1) | BE604348A (en) |
ES (1) | ES268327A1 (en) |
FR (1) | FR1280598A (en) |
LU (1) | LU40214A1 (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3281136A (en) * | 1960-09-12 | 1966-10-25 | Arbed | Method and apparatus for the gas injection into a metal bath |
US3387784A (en) * | 1966-10-27 | 1968-06-11 | Chemetron Corp | Burner for fluid fuels |
US3547624A (en) * | 1966-12-16 | 1970-12-15 | Air Reduction | Method of processing metal-bearing charge in a furnace having oxy-fuel burners in furnace tuyeres |
US3608881A (en) * | 1967-03-24 | 1971-09-28 | Za Zvetni Metali K | Tuyere apparatus for using liquid fuel in the fuming process |
US3703279A (en) * | 1969-08-15 | 1972-11-21 | Joslyn Mfg & Supply Co | Reactor |
US3771473A (en) * | 1971-01-20 | 1973-11-13 | Siderurgie Fse Inst Rech | Tuyere for a blast furnace and a method for operating the tuyere to atomize combustible material fed into the tuyere by a shock wave |
US3811386A (en) * | 1971-12-09 | 1974-05-21 | Maximilianshuette Eisenwerk | Tuyere for introducing oxygen and a protective medium into converter vessels |
DE4136274A1 (en) * | 1991-11-04 | 1993-05-06 | Kortec Ag, Zug, Ch | METHOD AND DEVICE FOR PROTECTING A BLOWING DEVICE ARRANGED IN A HOT WIND LINE OF A BLAST FURNACE |
US5645615A (en) * | 1992-08-13 | 1997-07-08 | Ashland Inc. | Molten decomposition apparatus and process |
US20110197588A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Fuel Injector Nozzle |
US20110197594A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Method of Controlling a Combustor for a Gas Turbine |
US20110197589A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Fuel Injector Nozzle |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
LU88065A1 (en) * | 1992-02-05 | 1993-08-17 | Paul Wurth S.A. | BURNER FOR A TANK OVEN |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US199134A (en) * | 1878-01-08 | Improvement in tuyeres | ||
US370251A (en) * | 1887-09-20 | Half to edward b | ||
US1629045A (en) * | 1925-07-07 | 1927-05-17 | John A Parker | Blast furnace |
US1729447A (en) * | 1929-09-24 | Cooling well foe burners | ||
US2338623A (en) * | 1941-01-30 | 1944-01-04 | Crowe John Marshall | Burner structure |
US2446511A (en) * | 1946-08-21 | 1948-08-03 | Air Liquide | Open-hearth steelmaking |
US2829960A (en) * | 1954-01-18 | 1958-04-08 | Henry J Kaiser Company | Method and metallurgical device for the refining of steel |
-
1960
- 1960-06-21 FR FR830839A patent/FR1280598A/en not_active Expired
- 1960-10-12 US US62273A patent/US3076642A/en not_active Expired - Lifetime
-
1961
- 1961-05-29 BE BE604348A patent/BE604348A/en unknown
- 1961-06-02 LU LU40214A patent/LU40214A1/xx unknown
- 1961-06-17 ES ES0268327A patent/ES268327A1/en not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US199134A (en) * | 1878-01-08 | Improvement in tuyeres | ||
US370251A (en) * | 1887-09-20 | Half to edward b | ||
US1729447A (en) * | 1929-09-24 | Cooling well foe burners | ||
US1629045A (en) * | 1925-07-07 | 1927-05-17 | John A Parker | Blast furnace |
US2338623A (en) * | 1941-01-30 | 1944-01-04 | Crowe John Marshall | Burner structure |
US2446511A (en) * | 1946-08-21 | 1948-08-03 | Air Liquide | Open-hearth steelmaking |
US2829960A (en) * | 1954-01-18 | 1958-04-08 | Henry J Kaiser Company | Method and metallurgical device for the refining of steel |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3281136A (en) * | 1960-09-12 | 1966-10-25 | Arbed | Method and apparatus for the gas injection into a metal bath |
US3387784A (en) * | 1966-10-27 | 1968-06-11 | Chemetron Corp | Burner for fluid fuels |
US3547624A (en) * | 1966-12-16 | 1970-12-15 | Air Reduction | Method of processing metal-bearing charge in a furnace having oxy-fuel burners in furnace tuyeres |
US3608881A (en) * | 1967-03-24 | 1971-09-28 | Za Zvetni Metali K | Tuyere apparatus for using liquid fuel in the fuming process |
US3703279A (en) * | 1969-08-15 | 1972-11-21 | Joslyn Mfg & Supply Co | Reactor |
US3771473A (en) * | 1971-01-20 | 1973-11-13 | Siderurgie Fse Inst Rech | Tuyere for a blast furnace and a method for operating the tuyere to atomize combustible material fed into the tuyere by a shock wave |
US3811386A (en) * | 1971-12-09 | 1974-05-21 | Maximilianshuette Eisenwerk | Tuyere for introducing oxygen and a protective medium into converter vessels |
DE4136274A1 (en) * | 1991-11-04 | 1993-05-06 | Kortec Ag, Zug, Ch | METHOD AND DEVICE FOR PROTECTING A BLOWING DEVICE ARRANGED IN A HOT WIND LINE OF A BLAST FURNACE |
US5645615A (en) * | 1992-08-13 | 1997-07-08 | Ashland Inc. | Molten decomposition apparatus and process |
US20110197588A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Fuel Injector Nozzle |
US20110197594A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Method of Controlling a Combustor for a Gas Turbine |
US20110197589A1 (en) * | 2010-02-12 | 2011-08-18 | General Electric Company | Fuel Injector Nozzle |
US8468834B2 (en) | 2010-02-12 | 2013-06-25 | General Electric Company | Fuel injector nozzle |
US8555648B2 (en) * | 2010-02-12 | 2013-10-15 | General Electric Company | Fuel injector nozzle |
US8584467B2 (en) | 2010-02-12 | 2013-11-19 | General Electric Company | Method of controlling a combustor for a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
LU40214A1 (en) | 1962-12-03 |
ES268327A1 (en) | 1961-12-16 |
FR1280598A (en) | 1962-01-08 |
BE604348A (en) | 1961-11-29 |
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