US3823929A - Nozzle for fuel and oxygen lance assembly - Google Patents

Nozzle for fuel and oxygen lance assembly Download PDF

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Publication number
US3823929A
US3823929A US00396912A US39691273A US3823929A US 3823929 A US3823929 A US 3823929A US 00396912 A US00396912 A US 00396912A US 39691273 A US39691273 A US 39691273A US 3823929 A US3823929 A US 3823929A
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US
United States
Prior art keywords
pipe
fuel
closure wall
oxygen
accordance
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
Application number
US00396912A
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English (en)
Inventor
N Rymarchyk
L Meinert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Berry Metal Co
Original Assignee
Berry Metal Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Berry Metal Co filed Critical Berry Metal Co
Priority to US00396912A priority Critical patent/US3823929A/en
Priority to AU65410/74A priority patent/AU484075B2/en
Priority to NL7401854A priority patent/NL7401854A/xx
Priority to BE140984A priority patent/BE811113A/xx
Priority to CA193,073A priority patent/CA1002314A/en
Priority to JP2507774A priority patent/JPS535962B2/ja
Priority to FR7412757A priority patent/FR2243999B1/fr
Priority to DE2420444A priority patent/DE2420444C3/de
Priority to DE19747414810U priority patent/DE7414810U/de
Priority to BR5645/74A priority patent/BR7405645D0/pt
Application granted granted Critical
Publication of US3823929A publication Critical patent/US3823929A/en
Priority to GB3960574A priority patent/GB1477390A/en
Priority to US05/531,005 priority patent/USRE28769E/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C5/00—Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28—Manufacture of steel in the converter
    • C21C5/42—Constructional features of converters
    • C21C5/46—Details or accessories
    • C21C5/4606—Lances or injectors

Definitions

  • a lance for directing oxygen and fuel oil to a basic oxygen furnace includes a central fuel pipe, an insulating pipe around said fuel pipe, an oxygen pipe and water coolant pipes, all concentrically disposed.
  • the central fuel pipe and insulating pipe have closed bottom walls and a plurality of relatively narrow fuel tubes are connected to bores in the bottom wall of the fuel tube, extend through the bottom wall of the insulating pipe and extend into three converging-diverging orifices.
  • the narrow fuel tubes are supported in cantilever fashion and-are concentricwith each orifice.
  • the present lance includes five concentric pipes, with a central fuel pipe having a transverse first closure wall.
  • An insulating pipe around said closure wall also lance assembly 10 comprises a first inner pipe 13 which is utilized for the flow of fuel oil, or similar type of fuel,
  • the first inner pipe 13 which extends substantially the full length of the lance is surrounded and concentric with a second insulating pipe 14 which provides therebetween an insulating space 15.
  • the upper end of the pipe 13 is provided with an enlargement and which has integral therewith an enlarged sleeve 16 of piston-like configuration.
  • the enlarged piston type sleeve is provided with'a plurality of 0 sealing rings 17.
  • the sealing rings 17 may be of any includes a second transverse closure wall below said first wall.
  • Thelance end or nozzle is of the multiple type including three equally spaced orifices of conver-. gent-divergent cylindrical wall construction. Three relatively narrow fuel tubes are secured to the first wall, communicate with the first or central fuel pipe and project through the second wall in cantilever relation.
  • FIG. I is a perspective view disclosing one embodiment of the gas injection lance of this invention.
  • FIG. 2 is a cross'sectional view disclosing a. top adapter assembly of the injection lance shown in FIG. 1-
  • FIG. 4 is a detail view in cross section taken substantially along the line 44 of FIG. 1;
  • FIG. 5 is a detail cross sectional view through the uppermost part of an adaptor assembly showing a modified detail of the invention.
  • FIG. 6 is a cross sectional view taken substantially along the line 6-6 of FIG. 3.
  • an oxygen fuel lance assembly is designated at 10 and includes a top assembly 11 and a lower nozzle or lance tip designated at 12.
  • FIG. 3 is a cross sectional view through the lower I suitable conventional construction and O-type sealing rings are effective for this purpose.
  • a stub pipe 18 is in mating relation with respect to the sleeve 16 and is'provided at its upper end with an adaptor connection 19 which may be suitably connected to a source of fuel oil.
  • the lower end of the stub pipe 18 is provided with a piston sleeve portion 20, alsoincluding a plurality of sealing rings 21.
  • the second insulating pipe 14 is also similarly provided with an enlarged piston sleeve 22 at its upper end which projects upwardly beyond the sleeve 16.
  • the piston sleeve 22 is also provided with a plurality of seals 23.
  • a third pipe is indicatedat 24 and is provided with an extension or lower section 24, the connection therebetween which will be later described.
  • the third pipe 24 has connected thereto an oxygen inlet connection 26 which provides for the flow of oxygen through an oxygen passage 25 provided between the pipe 24 and the pipe 14.
  • a cover plate 27 is removably connected by means of cap screws 28 to the upper ends of a sleeve or bushing 29.
  • the piston sleeves 16 may be simply referred to as sleeves, as well as the bushing 29, since they are of sleeve-like construction and are all connected to respective pipes.
  • the sleeve 29 is provided with a circumferential flange 30 and has also connected thereto a reduced portion 31 which is in overlapping engagement with the upper end of the third pipe 24. Since the upper terminal ends of the enlarged sleeves l6 and 22 are disposed below or in spaced relation with respect to the cover plate 27, there is provided a space or chamber 32.
  • the upper portions of the bushing 29 are provided with a pair of threaded bores 33, only one of which is shown in FIG. 4, the said bores 33 having contained therein threaded plugs 34 which each include a vent bore 35 adapted to vent the chamber 32 to the atmosphere.
  • a circumferential flange 36 is connected to the flange 30 by means of bolt and nut assemblies 37.
  • a circumferential flange 38 is connected to the third pipe 24 and a fourth pipe 39 is provided with a flange 40 suitably connected to the flange 38 by means of bolt and nut assemblies 41.
  • a flange 42 is sandwiched between flanges 38 and 40, the said flange 42 being provided on a bushing or sleeve 43 which is provided with a circumferential seal 44 in sealingengagement with respect to the fourth pipe 39.
  • the flange 42 is sealed against the 3 flange 40 by means of a circumferential seal 45.
  • a vent space orchamber 46 is provided between the pipe 24 and the bushing 43, the same being vented to the atmosphere by virtue of a pair of vent Openings 46'. As shown in FIG.
  • the third pipe 24 consists of two sections and the section 24' is provided with an upwardly extending sleeve 47 which is in sliding engagement with a piston sleeve 48 connected to the lower end of the third pipe 24.
  • Suitable seals 49 on the piston sleeve 48 are in sealing engagement with an inner surface of the sleeve 47 and similarly, seals 50 on the sleeve 47 are in sealing relation with respect to the cylindrical surface of the bushing or sleeve 43.
  • the third pipe section 24' and fourth pipe extension section 39' provide a water directing space 51 which communicates with the water inlet 52.
  • a flange 53 is connected to the lower end of the section 39 and the extension 39 of the pipe 39 provides a passage 54 in communication with the water circulating space 51.
  • a flange 55 is connected to a fifth pipe 57 and suitable bolt and nut connections 56 connect flanges 53 and 55.
  • the lower portions of the fifth pipe 57 are connected by means'of a flange 59 to which is connected a downwardly projecting pipe extension 57 providing for a continuation of the pipe 57.
  • the fifth pipe 57 provides for a water outlet space 60 which is fed by means of a water circulating space 60' formed by the fifth pipe extension 57 thereby circulating water outwardly through the discharge pipe 58.
  • the fifth pipe extension 57' extends downwardly and is suitably connected by welding to a dish-shaped lower or transverse wall 61 having upwardly extending peripheral edge portions 62 conforming and being connected to the-pipe extension 57.
  • the pipe extension 57' may consist of suitable similar extensions connected together by welding, these additional extensions not being designated separately but being considered part of the fifth pipe arrangement.
  • the same is true for the 4 nozzle arrangement 12, only one of which is shown.
  • the cylindrical walls 70 are cooled by means of the water circulating within the chamber 66.
  • the lower ends of each of the cylindrical walls 70 are provided with an outlet orifice 71 through which the combined fuel and oxygen flows into the oxygen vessel of a BOF operation.
  • Each orifice 71 is of converging diverging type in that a cylindrical diverging wall portion 74 is provided at the upper end of the orifice 71 and communicates with a cylindrical portion 73 of constant diameter throughout its length, the said cylindrical portion 73 then communicating with the diverging cylindrical portion 74 extending to the end of the nozzle tip.
  • Each of the orifices 74 is provided with a fuel tube 75 welded within an opening 76 in' the closure wall 67.
  • Each fuel tube 75 extends through an opening 77 provided in the other pipes in that the extensions are provided and are necessary to form slip joints accommodating the longitudinal expansion and contraction to which these assemblies are subjected by extreme temperatures.
  • the pipe extension 39' for instance, is provided with a re **d portion 63 which is in relative sliding and mating relation with a pipe extension 64 which still is considered an extension of the pipes 39 and 39'.
  • This type of arrangement accommodates the contractions and expansions which occur.
  • the extension 64 is provided at its lower end with a skirt 65 defining a portion of an enlarged cooling chamber 66.
  • the present nozzle arrangement is of the multiple orifice type, meaning that in this case three orifices are utilized.
  • FIG. 3 discloses only one such orifice since they are identical and are equally spaced about the circumference of the nozzle arrangement 12.
  • the dishshaped lower wall 61 which encloses the lower end of the nozzle can be described as transverse in that it extends across the lower end of the pipe section 57'.
  • an arcuate but nevertheless somewhat transverse closure wall 67 encloses the lower end of the first inner pipe 13.
  • the insulating pipe 14 is enclosed by a transverse or generally arcuate closure wall 68.
  • a similarly extending wall 69 encloses the oxygen space which is provided between the pipes 14 and 24.
  • Three cylindrical walls 70 are provided in the lower end of the transverse closure walls 68 to which it is also welded.
  • the fuel tube is thus supported in cantilever relation relative to the tubes 13 and 14 and projects centrally into the nozzle 71 terminating slightly below the terminal end of the constant cylindrical wall portion 73.
  • the tube 75 is also supported as best shown in FIGS. 3 and 6 by means of spacers 78 and 79 in turn rigidly welded to the cylindrical converging wall portion 72.
  • Each tube 75 thus is effectively supported within each orifice 71, yet permitting the free flow of oxygen and fuel through the ends of each orifice.
  • FIG. 2 Referring now to FIG. 2 and particularly to the portion of the insulating pipe 14 below its piston sleeve 22, there is provided a threaded test opening 80 which is normally closed by means of a threaded plug 81.
  • the parts are identical except that the piston sleeve 16 forming part of the firstpipe 13 is provided with one or more passages 82 which communicate at their lower ends with the insulating space 15, the said passage 82 being normally closed at its upper end by means of a threaded plug 83.
  • the lance In the operation of the lance, it is supported at its upper end by means of a suitable crane type structure above a bath provided in a basic oxygen furnace.
  • the nozzle is disposed a predetermined distance from the bath and fuel oil may enter through the stub pipe 18,
  • One of the primary features of the invention is the easily repairable feature and also the ease with'which the sealing surfaces and seals may be inspected.
  • the seals 23 may be immediately inspected and replaced. Further, by the removal of the stub pipe 18, the seals 21 may be either inspected or replaced.
  • the vent chamber is extremely important in venting any leaking oxygen to the atmosphere before it can be intermixed with other elements which might be leaking.
  • oxygen which may leak past the seals 23 immediately is vented to the atmosphere through the vent openings 35.
  • the threaded bores 33 also serve the purpose of permitting the insertion of a test nipple replacing the one-half inch plug which is shown in FIG. 4.
  • a test nipple may be a portion of a pressure testing unit which provides high pressure fluid into the vent chamber 32 for the purpose of testing the seals 23 and 21.
  • the insulating pipe 14 provides an insulating space 15 which serves as a safety chamber between the oxygen passage in the event that there is a leakage of any of the connections of the pipe 13.
  • the pipes may all be made in sections which are welded together and any leakage such as could occur because of an improper weld in the fuel tube 13 will be taken care of because of the insulating space 15.
  • the seal 17 prevents the escape of fuel oil from the insulating chamber, but in the event some does escape by the seals 17, the same is carried from the vent chamber 32 through the vent openings and is quickly noticed the operator so that the operation may be halted for repair.
  • the threaded test opening 80 and pipe plug arrangement 81 also serve a distinct and effective purpose during the testing procedure of the lance.
  • a suitable nipple is attachedto the threaded opening 18 to direct water under pressure into the insulating chamber 15 thereby providing for the desired test of the seals 17 and the welds of the various sections of the pipes involved. It is apparent that in view of the arrangement of the sleeves 16, 22 and bushing 29 with their respective seals, vertical expansion and contraction of the pipes is accommodated. Expansion of the pipe 39 and section 39' is accommodated as shown in FIG. 3 by the sliding slip joint or reduced section 63 relative to the pipe extension 64.
  • FIG. 5 shows a modified arrangement.
  • the sleeve 16 is provided with one or more vertical passages 82 which communicates with the insulating chamber 15.
  • the passages 82 would be closed by the pipe plug 83.
  • the seals 17 would be effectively tested.
  • the seals 17 could be eliminated or the passage 82 could remain open so as to permit any leakage from the chamber 15 to be immediately directed into the chamber 32 where it would become quickly visible to the operator.
  • the alternate is provided in that during operation where the seals 17 are employed the operator may remove the pipe plug 83, opening the bore 82 to accommodate the free flow of escaping fuel oil into the vent chamber 32, whereupon it would be quickly noticed due to leakage outwardly of the vent openings.
  • the O-rings or seals 17 would be primarily utilized in the pressure testing of the unit, but would not have any effect during the normal operation of the lance, since the passages 82 would be open.
  • a further advantage is the provision of the venting chamber 46 and the vent opening 46.
  • any leakage of oxygen past the seals 49 would immediately appear in the chamber 46 and be dissipated through the openings 46'.
  • the advantages of the quickly removable disconnect of the bushing 43 is also apparent, the same permitting quick inspection of the seals and proper replacement of any portions of this particular assembly.
  • the arrangement permits pressure testing of the lance prior to its use which is not accomplished or contemplated in the prior art.
  • the tubes are effectively cantilevered on the lower ends of the pipes 13 and 14, and thus an effective operation is secured.
  • the cantilever arrangement of the tubes 75 provides for a strong anchoring of said tubes. Further, the spacers 78 and 79 further support the tubes 75in the orifices 71 effectively and thereby eliminate the tendency of vibration which would otherwise occur. Yet the passage of oxygen through the orifices is facilitated and Y mixture of oxygen and oil is achieved in the diverging position of the orifice thereby effectively mixing and discharging the combination.
  • a lance adapted for mixing oxygen and fuel and including,
  • fourth and fifth pipes concentric with each other and said other pipes providing concentric coolant circulating spaces;
  • At least one cylindrical passage means opening outwardly of said first closure wall to provide an oxygen and fuel discharge orifice
  • said tube being connected to and extending through said third closure wall
  • closure walls extending-transversely to the axis of said lance.
  • said discharge orifice having a cylindrical wall portion converging inwardly and then outwardly toward said first closure wall.
  • said cylindrical wall having a portion thereof disposed between said converging diverging portion of constant cross sectional diameter.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Blast Furnaces (AREA)
  • Gas Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
US00396912A 1973-09-13 1973-09-13 Nozzle for fuel and oxygen lance assembly Expired - Lifetime US3823929A (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
US00396912A US3823929A (en) 1973-09-13 1973-09-13 Nozzle for fuel and oxygen lance assembly
AU65410/74A AU484075B2 (en) 1974-02-08 Nozzle for fuel and oxygen lance assembly
NL7401854A NL7401854A (ja) 1973-09-13 1974-02-12
BE140984A BE811113A (fr) 1973-09-13 1974-02-15 Tuyere pour assemblage de lance a combustible et a oxygene
CA193,073A CA1002314A (en) 1973-09-13 1974-02-20 Nozzle for fuel and oxygen lance assembly
JP2507774A JPS535962B2 (ja) 1973-09-13 1974-03-04
FR7412757A FR2243999B1 (ja) 1973-09-13 1974-04-11
DE2420444A DE2420444C3 (de) 1973-09-13 1974-04-26 Blaslanze zum Mischen von Sauerstoff und Brennstoff
DE19747414810U DE7414810U (de) 1973-09-13 1974-04-26 Blaslanze zum mischen von sauerstoff und brennstoff
BR5645/74A BR7405645D0 (pt) 1973-09-13 1974-07-09 Lanca adaptada para misturar oxigenio
GB3960574A GB1477390A (en) 1973-09-13 1974-09-11 Oxygen-fuel lance
US05/531,005 USRE28769E (en) 1973-09-13 1974-12-09 Nozzle for fuel and oxygen lance assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00396912A US3823929A (en) 1973-09-13 1973-09-13 Nozzle for fuel and oxygen lance assembly

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US05/531,005 Reissue USRE28769E (en) 1973-09-13 1974-12-09 Nozzle for fuel and oxygen lance assembly

Publications (1)

Publication Number Publication Date
US3823929A true US3823929A (en) 1974-07-16

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Family Applications (1)

Application Number Title Priority Date Filing Date
US00396912A Expired - Lifetime US3823929A (en) 1973-09-13 1973-09-13 Nozzle for fuel and oxygen lance assembly

Country Status (9)

Country Link
US (1) US3823929A (ja)
JP (1) JPS535962B2 (ja)
BE (1) BE811113A (ja)
BR (1) BR7405645D0 (ja)
CA (1) CA1002314A (ja)
DE (2) DE7414810U (ja)
FR (1) FR2243999B1 (ja)
GB (1) GB1477390A (ja)
NL (1) NL7401854A (ja)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4245824A (en) * 1978-12-28 1981-01-20 Pullman Berry Chute for charging vessels
US4809911A (en) * 1987-08-20 1989-03-07 John Ryan High pressure mixing and spray nozzle apparatus and method
US5635130A (en) * 1995-06-07 1997-06-03 Berry Metal Co. Combined oxygen blowing/fuel burner lance assembly
US6217824B1 (en) 1999-05-20 2001-04-17 Berry Metal Company Combined forged and cast lance tip assembly
US20070210186A1 (en) * 2004-02-26 2007-09-13 Fenton Marcus B M Method and Apparatus for Generating a Mist
US20070246869A1 (en) * 2006-04-21 2007-10-25 Berry Metal Company Metal making lance tip assembly
US20080230632A1 (en) * 2004-02-24 2008-09-25 Marcus Brian Mayhall Fenton Method and Apparatus for Generating a Mist
US20080310970A1 (en) * 2004-07-29 2008-12-18 Pursuit Dynamics Plc Jet Pump
US20090240088A1 (en) * 2007-05-02 2009-09-24 Marcus Brian Mayhall Fenton Biomass treatment process and system
US20090314500A1 (en) * 2006-09-15 2009-12-24 Marcus Brian Mayhall Fenton Mist generating apparatus and method
US20100129888A1 (en) * 2004-07-29 2010-05-27 Jens Havn Thorup Liquefaction of starch-based biomass
CN110081716A (zh) * 2018-01-26 2019-08-02 中国瑞林工程技术股份有限公司 用于电子废料冶炼装置的顶吹喷枪
US10507480B2 (en) 2004-02-26 2019-12-17 Tyco Fire Products Lp Method and apparatus for generating a mist

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1103449A (en) * 1977-05-09 1981-06-23 William W. Berry Oxygen lance assembly
ZA786675B (en) * 1978-11-28 1980-02-27 W Bleloch Apparatus for the production of steel and iron alloys
JPH0420812Y2 (ja) * 1986-12-03 1992-05-13
JP4853326B2 (ja) * 2007-02-26 2012-01-11 Ｊｆｅスチール株式会社 精錬用上吹きランス及び精錬用上吹きランスの破孔検知方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1070049A (en) * 1966-05-05 1967-05-24 Dorman Long Steel Ltd Improvements in or relating to burners for the combustion of liquid fuels with oxygen

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1070049A (en) * 1966-05-05 1967-05-24 Dorman Long Steel Ltd Improvements in or relating to burners for the combustion of liquid fuels with oxygen

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4245824A (en) * 1978-12-28 1981-01-20 Pullman Berry Chute for charging vessels
US4809911A (en) * 1987-08-20 1989-03-07 John Ryan High pressure mixing and spray nozzle apparatus and method
US5635130A (en) * 1995-06-07 1997-06-03 Berry Metal Co. Combined oxygen blowing/fuel burner lance assembly
US6217824B1 (en) 1999-05-20 2001-04-17 Berry Metal Company Combined forged and cast lance tip assembly
US20080230632A1 (en) * 2004-02-24 2008-09-25 Marcus Brian Mayhall Fenton Method and Apparatus for Generating a Mist
US20070210186A1 (en) * 2004-02-26 2007-09-13 Fenton Marcus B M Method and Apparatus for Generating a Mist
US10507480B2 (en) 2004-02-26 2019-12-17 Tyco Fire Products Lp Method and apparatus for generating a mist
US9010663B2 (en) * 2004-02-26 2015-04-21 Tyco Fire & Security Gmbh Method and apparatus for generating a mist
US9004375B2 (en) * 2004-02-26 2015-04-14 Tyco Fire & Security Gmbh Method and apparatus for generating a mist
US8419378B2 (en) 2004-07-29 2013-04-16 Pursuit Dynamics Plc Jet pump
US20080310970A1 (en) * 2004-07-29 2008-12-18 Pursuit Dynamics Plc Jet Pump
US9239063B2 (en) 2004-07-29 2016-01-19 Pursuit Marine Drive Limited Jet pump
US20100129888A1 (en) * 2004-07-29 2010-05-27 Jens Havn Thorup Liquefaction of starch-based biomass
US20070246869A1 (en) * 2006-04-21 2007-10-25 Berry Metal Company Metal making lance tip assembly
US8789769B2 (en) 2006-09-15 2014-07-29 Tyco Fire & Security Gmbh Mist generating apparatus and method
US20090314500A1 (en) * 2006-09-15 2009-12-24 Marcus Brian Mayhall Fenton Mist generating apparatus and method
US9931648B2 (en) 2006-09-15 2018-04-03 Tyco Fire & Security Gmbh Mist generating apparatus and method
US8513004B2 (en) 2007-05-02 2013-08-20 Pursuit Dynamics Plc Biomass treatment process
US8193395B2 (en) 2007-05-02 2012-06-05 Pursuit Dynamics Plc Biomass treatment process and system
US20100233769A1 (en) * 2007-05-02 2010-09-16 John Gervase Mark Heathcote Biomass treatment process
US20090240088A1 (en) * 2007-05-02 2009-09-24 Marcus Brian Mayhall Fenton Biomass treatment process and system
CN110081716A (zh) * 2018-01-26 2019-08-02 中国瑞林工程技术股份有限公司 用于电子废料冶炼装置的顶吹喷枪
CN110081716B (zh) * 2018-01-26 2024-04-23 中国瑞林工程技术股份有限公司 用于电子废料冶炼装置的顶吹喷枪

Also Published As

Publication number Publication date
AU6541074A (en) 1975-08-14
BR7405645D0 (pt) 1975-07-08
FR2243999B1 (ja) 1978-08-04
FR2243999A1 (ja) 1975-04-11
JPS535962B2 (ja) 1978-03-03
DE2420444A1 (de) 1975-03-27
CA1002314A (en) 1976-12-28
GB1477390A (en) 1977-06-22
DE7414810U (de) 1979-04-05
BE811113A (fr) 1974-05-29
NL7401854A (ja) 1975-03-17
DE2420444B2 (de) 1978-06-01
DE2420444C3 (de) 1979-01-18
JPS5055508A (ja) 1975-05-15

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