ES399060A1 - IMPROVEMENTS IN DEVICES TO MAKE SEVERAL, WITHIN A WIDE AREA, THE AMOUNT OF FUEL INTRODUCED INTO A NOZZLE. - Google Patents
IMPROVEMENTS IN DEVICES TO MAKE SEVERAL, WITHIN A WIDE AREA, THE AMOUNT OF FUEL INTRODUCED INTO A NOZZLE.Info
- Publication number
- ES399060A1 ES399060A1 ES399060A ES399060A ES399060A1 ES 399060 A1 ES399060 A1 ES 399060A1 ES 399060 A ES399060 A ES 399060A ES 399060 A ES399060 A ES 399060A ES 399060 A1 ES399060 A1 ES 399060A1
- Authority
- ES
- Spain
- Prior art keywords
- neck
- tuyere
- shock wave
- amount
- nozzle
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/34—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by ultrasonic means
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21B—MANUFACTURE OF IRON OR STEEL
- C21B7/00—Blast furnaces
- C21B7/16—Tuyéres
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Blast Furnaces (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Manufacture Of Iron (AREA)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Spray-Type Burners (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Nozzles (AREA)
Abstract
A method and an arrangement for operating a supersonic tuyere having a convergent and a divergent passage portion separated by a neck in such a manner so as to produce in the divergent passage portion a shock wave to atomize a combustible material fed in the region of the neck into the tuyere. The shock wave is produced by more or less restricting the open cross section of the neck, preferably by adjusting the axial position of a solid body in the convergent portion of the tuyere with respect to the neck, to maintain the pressure of a combustion sustaining material fed into the tuyere upstream of the convergene portion, during variation of the fed amount of such material within predetermined limits, at such a magnitude to assure production of a shock wave at the divergent portion.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7101742A FR2122682A5 (en) | 1971-01-20 | 1971-01-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES399060A1 true ES399060A1 (en) | 1975-06-01 |
Family
ID=9070543
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES399060A Expired ES399060A1 (en) | 1971-01-20 | 1972-01-20 | IMPROVEMENTS IN DEVICES TO MAKE SEVERAL, WITHIN A WIDE AREA, THE AMOUNT OF FUEL INTRODUCED INTO A NOZZLE. |
Country Status (17)
| Country | Link |
|---|---|
| US (1) | US3771473A (en) |
| JP (1) | JPS52442B1 (en) |
| AT (1) | AT319295B (en) |
| AU (1) | AU470614B2 (en) |
| BE (1) | BE778109A (en) |
| BR (1) | BR7200222D0 (en) |
| CA (1) | CA979646A (en) |
| DD (1) | DD96509A5 (en) |
| DE (1) | DE2201607A1 (en) |
| ES (1) | ES399060A1 (en) |
| FR (1) | FR2122682A5 (en) |
| GB (1) | GB1367204A (en) |
| IT (1) | IT946421B (en) |
| LU (1) | LU64608A1 (en) |
| NL (1) | NL7117957A (en) |
| PL (1) | PL71082B1 (en) |
| SU (1) | SU452965A3 (en) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4021512A (en) * | 1976-02-12 | 1977-05-03 | Aeronutronic Ford (Now Ford Aerospace And Communications) | Carburetor air turbine fuel distributor |
| US4021511A (en) * | 1976-02-12 | 1977-05-03 | Ford Aerospace & Communications | Fuel distributor apparatus for plug-type carburetor |
| US4171798A (en) * | 1976-03-26 | 1979-10-23 | Koppers Company, Inc. | Method and apparatus for obtaining and securing optimum thrust of blast fluid flowing into a metallurgical furnace |
| US4109862A (en) * | 1977-04-08 | 1978-08-29 | Nathaniel Hughes | Sonic energy transducer |
| US4189101A (en) * | 1977-04-08 | 1980-02-19 | Nathaniel Hughes | Stable vortex generating device |
| US4154056A (en) | 1977-09-06 | 1979-05-15 | Westinghouse Electric Corp. | Fuel nozzle assembly for a gas turbine engine |
| FR2561539B1 (en) * | 1984-03-20 | 1988-09-16 | Raffinage Cie Francaise | DEVICE FOR SPRAYING A LIQUID IN A GAS STREAM WITH MULTIPLE SUCCESSIVE VENTURIS AND APPLICATIONS THEREOF |
| CA1272662A (en) * | 1985-03-26 | 1990-08-14 | Canon Kabushiki Kaisha | Apparatus and process for controlling flow of fine particles |
| FR2579487B1 (en) * | 1985-03-26 | 1989-05-12 | Canon Kk | APPARATUS FOR CONTROLLING THE FLOW OF FINE PARTICLES |
| US4867918A (en) * | 1987-12-30 | 1989-09-19 | Union Carbide Corporation | Gas dispersion process and system |
| US4931225A (en) * | 1987-12-30 | 1990-06-05 | Union Carbide Industrial Gases Technology Corporation | Method and apparatus for dispersing a gas into a liquid |
| DE3913334A1 (en) * | 1989-04-22 | 1990-10-25 | Caldyn Apparatebau Gmbh | DEVICE FOR SPRAYING LIQUID OR FOR SPRAYING GAS INTO SMALL BUBBLES |
| US5436210A (en) * | 1993-02-04 | 1995-07-25 | Molten Metal Technology, Inc. | Method and apparatus for injection of a liquid waste into a molten bath |
| US5679132A (en) * | 1995-06-07 | 1997-10-21 | Molten Metal Technology, Inc. | Method and system for injection of a vaporizable material into a molten bath |
| DE102010047969A1 (en) * | 2010-03-31 | 2011-10-06 | Sms Siemag Aktiengesellschaft | Device for injecting gas into a metallurgical vessel |
| DE102014102913A1 (en) * | 2014-03-05 | 2015-09-10 | Thyssenkrupp Ag | Method for operating a shaft furnace, in particular a blast furnace |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1171136A (en) * | 1957-04-11 | 1959-01-22 | Siderurgie Fse Inst Rech | Improvements to shaft furnace nozzles and in particular to blast furnace nozzles |
| FR1280598A (en) * | 1960-06-21 | 1962-01-08 | Pompey Acieries | Device for injecting liquid, semi-liquid, pulverulent, fluidized or the like substances |
| FR1559679A (en) * | 1967-12-08 | 1969-03-14 | ||
| FR95501E (en) * | 1967-12-13 | 1971-01-22 | Raffinage Cie Francaise | Improved process for blowing furnaces and device for carrying out the process. |
-
1971
- 1971-01-20 FR FR7101742A patent/FR2122682A5/fr not_active Expired
- 1971-11-30 SU SU1718599A patent/SU452965A3/en active
- 1971-12-28 NL NL7117957A patent/NL7117957A/xx unknown
-
1972
- 1972-01-07 GB GB74172A patent/GB1367204A/en not_active Expired
- 1972-01-10 IT IT19183/72A patent/IT946421B/en active
- 1972-01-11 JP JP47005049A patent/JPS52442B1/ja active Pending
- 1972-01-14 BR BR222/72A patent/BR7200222D0/en unknown
- 1972-01-14 AU AU37936/72A patent/AU470614B2/en not_active Expired
- 1972-01-14 DE DE19722201607 patent/DE2201607A1/en active Pending
- 1972-01-17 BE BE778109A patent/BE778109A/en unknown
- 1972-01-17 CA CA132,622A patent/CA979646A/en not_active Expired
- 1972-01-18 LU LU64608D patent/LU64608A1/xx unknown
- 1972-01-19 AT AT42472A patent/AT319295B/en not_active IP Right Cessation
- 1972-01-19 PL PL1972152966A patent/PL71082B1/pl unknown
- 1972-01-19 US US00218962A patent/US3771473A/en not_active Expired - Lifetime
- 1972-01-19 DD DD160417A patent/DD96509A5/xx unknown
- 1972-01-20 ES ES399060A patent/ES399060A1/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US3771473A (en) | 1973-11-13 |
| BR7200222D0 (en) | 1973-05-17 |
| IT946421B (en) | 1973-05-21 |
| CA979646A (en) | 1975-12-16 |
| AT319295B (en) | 1974-12-10 |
| BE778109A (en) | 1972-07-17 |
| JPS52442B1 (en) | 1977-01-07 |
| SU452965A3 (en) | 1974-12-05 |
| PL71082B1 (en) | 1974-04-30 |
| GB1367204A (en) | 1974-09-18 |
| DD96509A5 (en) | 1973-03-20 |
| AU3793672A (en) | 1973-07-19 |
| FR2122682A5 (en) | 1972-09-01 |
| AU470614B2 (en) | 1976-03-25 |
| DE2201607A1 (en) | 1972-08-03 |
| NL7117957A (en) | 1972-07-24 |
| LU64608A1 (en) | 1972-06-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB973319A (en) | Improvements in supersonic fuel injector | |
| GB680371A (en) | Reheater for jet propulsion engines | |
| GB782323A (en) | Improvements in devices for regulating the effective cross-section of a discharge nozzle | |
| GB1037287A (en) | Hot gas generating installation | |
| GB731054A (en) | Gas turbine combustion chamber | |
| GB1009323A (en) | Rocket motor with exhaust nozzle closure device | |
| ES422411A1 (en) | Supersonic shock wave tuyere | |
| Priem | Propellant vaporization as a criterion for rocket engine design: calculations of chamber length to vaporize a single n-heptane drop | |
| ES395943A1 (en) | PROCEDURE FOR THE INTRODUCTION OF A LIQUID AUXILIARY FUEL INTO A HIGH OVEN. | |
| GB505747A (en) | Improvements connected with rockets | |
| GB1026996A (en) | Supersonic intake for a jet propulsion engine | |
| GB416030A (en) | Improved process of and means for feeding gas turbines | |
| GB1381118A (en) | Fluid flow regulator | |
| CH289804A (en) | Process for the intermittent forced pulverization of fuel in internal combustion engines and carburetor for carrying out the process. | |
| GB585801A (en) | Improvements in and relating to internal combustion engines operating with fuel injection | |
| GB1411007A (en) | Sludge injector | |
| GB1239693A (en) | ||
| GB838326A (en) | Method and means for control of combustion in internal combustion engines | |
| GB821693A (en) | Improvements in or relating to diesel engines and to precombustion chambers therefor | |
| GB1173098A (en) | Projectile for Supersonic Flight | |
| GB708343A (en) | Improvements in or relating to ram jets | |
| GB800548A (en) | Improvements in and relating to convergent-divergent turbine nozzles with a quadrilateral-shaped outlet orifice, and method for their manufacture | |
| GB708266A (en) | Improvements in or relating to ram jets | |
| BROWN et al. | Combustion instability study of solid propellants(Combustion instability analysis of solid propellants)[Final Report, Sep. 1971- Mar. 1973] | |
| GB1355680A (en) | Internal combustion fuel injection engines and method of operating them |