GB1584940A - Creación de Inventos y Patentes con Inteligencia Artificial

GB1584940A – Cooling assembly for metallurgical vessels
– Google Patents

GB1584940A – Cooling assembly for metallurgical vessels
– Google Patents
Cooling assembly for metallurgical vessels

Download PDF
Info

Publication number
GB1584940A

GB1584940A
GB24134/78A
GB2413478A
GB1584940A
GB 1584940 A
GB1584940 A
GB 1584940A
GB 24134/78 A
GB24134/78 A
GB 24134/78A
GB 2413478 A
GB2413478 A
GB 2413478A
GB 1584940 A
GB1584940 A
GB 1584940A
Authority
GB
United Kingdom
Prior art keywords
vessel
members
passages
flow
adjacent
Prior art date
1977-06-30
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

Application number
GB24134/78A
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.)

Pennsylvania Engineering Corp

Original Assignee
Pennsylvania Engineering Corp
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.)
1977-06-30
Filing date
1978-05-30
Publication date
1981-02-18

1978-05-30
Application filed by Pennsylvania Engineering Corp
filed
Critical
Pennsylvania Engineering Corp

1981-02-18
Publication of GB1584940A
publication
Critical
patent/GB1584940A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

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

C21C5/4646—Cooling arrangements

Description

PATENT SPECIFICATION
( 11) 1584940 ( 21) Application No 24134/78 ( 22) Filed 30 May 1978 ( 31) Convention Application No 811 571 ( 32) Filed 30 June 1977 in Cry ( 33) United States of America (US) I ( 44) Complete Specification published 18 Feb 1981 ef ( 51) INT CL 3 C 2 l C 5/42 ? ( 52) Index at acceptance F 4 B NB ( 54) COOLING ASSEMBLY FOR METALLURGICAL VESSELS ( 71) We, PENNSYLVANIA ENGINEERING CORPORATION, Thirty-Second Street, Pittsburgh, Pennsylvania, 15201, United States of America, a corporation organised under the laws of the State of Delaware, United States of America, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following
statement: –
This invention relates to cooling assemblies for metallurgical converter vessels.
Pneumatic type metallurgical converters commonly include a generally pear-shaped vessel which is open at its upper end Means are commonly provided for delivering oxygen to a molten charge contained within the vessel The oxygen delivery system may include, for example, a lance which extends through the open mouth of the vessel or tuyeres which extend through the vessels bottom or sides It is a common practice to cool the upper portion of such metallurgical vessels to minimize thermal deformation which would otherwise result from the high temperatures to which this portion of the vessel is exposed Such cooling arrangements commonly take the form of pipes or hollow panels affixed to or adjacent the vessel surface In addition, hollow means for receiving cooling fluid are often disposed in surrounding relation to the vessel mouth.
Water cooling of the areas of excessive elevated temperatures is desirable to stabilize external thermal distortion of the plates which define the outer metallic shell Such distortion results from overheating of a particular area in relation to adjacent areas while the entire shell is subjected to mechanical stress from the molten metal within the furnace, the support loads and the external pressure due to thermal expansion of the lining refractory Overheating can be caused by conductive heat transfer from the inside of the vessel and through the refractory, particularly when the refractory has been worn thin, intense radiant heat such as that experienced around the vessel tap nozzle, as well as external spills and slag spitting.
Where the cooling assembly is composed of pipe members, these generally include half pipes or angle members whose edges are affixed to the vessel surface This provides an uneven surface which renders the removal of slag and metal relatively more difficult.
According to the invention there is provided a metallurgical vessel having an upper end which defines a generally frusto-conical section and a top opening, cooling means disposed on the surface of said vessel adjacent to and disposed in a generally surrounding relation to said opening, said cooling means including a plurality of elongate members having first and second legs which are generally perpendicular on to the other in transverse section, said members being affixed to the surface of said vessel in a side-by-side relation and extending in axial planes of the frusto-conical section and having one end remote from said opening and another end proximate thereto to define a plurality of flow passages, wherein, in each member, first leg is affixed to the vessel and extends generally outwardly relative to the surface thereof and the second leg is intergral with the first leg is oriented generally parallel to the surface of the vessel, said second leg being affixed to the adjacent member whereby passages are defined between adjacent members and the surface of the vessel, the second legs of the members being configured such that all of the second legs when in abutment provide a generally smooth frusto-conical surface substantially parallel to the surface of said section, the first legs of at least a plurality of said members having openings formed therein for interconnecting the passages formed thereby, an inlet connected to the remote end of one of the passages and an outlet connected to the proximate end of another one of the passages.
An embodiment of the invention will now be described by way of example with reference to the accompanying drawings in which: ( 19) 1,584,940 Figure 1 is an elevational view of the upper portion of a metallurgical converter vessel incorporating a cooling assembly; Figure 2 is a top plan view of the vessel and cooling assembly shown in Figure 1; Figure 3 is a view taken along lines 3-3 of Figure 2; Figure 4 is a view taken along lines 4-4 of Figure 3; Figure 5 is a view taken along lines 5-5 of Figure 3; and Figure 6 is a view taken along lines 6-6 of Figure 2.
FIGURE 1 shows the upper portion of a metallurgical vessel 10 of the type wherein oxygen is injected into a molten metallic charge for the purpose of oxidizing undesirable constituents While only a portion of the vessel is shown, it will be appreciated that it includes a refractory lining 11 and a metallic shell 12 In addition, the vessel is generally pear-shaped and has an opening 13 at its upper end for receiving a metallic charge The upper section 14 of the shell 12 tapers upwardly and inwardly toward the opening 13 and is commonly referred to as a nose cone.
Vessels of the type illustrated in FIGURE 1 are commonly mounted for pivotal movement about a horizontal axis so that they may be tilted for receiving a charge or for discharging metal through a tap nozzle 16.
Toward this end, the vessel 10 may be mounted on a trunnion ring 18 which has a pair of trunnion pins 20 extending from its opposite sides The vessel 10 may be affixed to trunnion ring 18 by suitable brackets which are not shown but are well known in the art The trunnion pins 20 may be supported by suitable bearings (not shown) and are coupled to a tilt mechanism (not shown).
The frusto-conical nose cone portion of the outer shell 14 is formed of steel plate and has a flange 22 at its lower end which permits attachment by means of bolts 24 to a mating flange 26 disposed at the upper end of the remaining portion of the furnace shell.
A cooling assembly 28 according to the present invention is affixed to the nose cone shell portion 14.
The cooling assembly 28 comprises a jacket portion 30 which consists of individual cooling segments 30 a, 30 b, 30 c and 30 d each of which is defined by a central angle of 900 Each segment includes a plurality of individual angle members 32 which are L-shaped in transverse cross-section and are affixed to the shell portion 14 As seen more particularly in FIGURE 4, the edge of the short leg portions 34 of each angle member 32 is suitably affixed such as by welding to the metal shell portion 14 and each leg portion 34 extends in the radial direction relative to shell portion 14 The edge of the long leg portions 36 of each angle member 32 is welded to the outer side portion of the leg 34 of the next adjacent angle member 32 As a result, the legs 34 of angle members 32 are generally normal to the surface of shell portion 14 and the other legs 36 there 70 of are generally parallel to said surface This defines a plurality of hollow water passages 38 extending generally in the axial direction along the outer surface of shell portion 14.
Secured to the shell 14 adjacent the upper 75 edges of each of the angle members 32 is an annular ring 40 which acts to close the upper end of substantially all of the passages 38.
A similar ring 42 is affixed to the vessel and the members 32 adjacent the lower end of 80 the assembly for enclosing substantially all of the lower ends of the passages 38 as will also be discussed below It will be appreciated that the rings 40 and 42 may be a single member or a plurality of segments 85 and may be affixed in any suitable manner such as by welding Also, while ring 40 is continuous, there is a gap in the member 42 adjacent the tap nozzle 16 as seen in FIGURE 6 Also, the members 32 above 90 nozzle 16 are shorter and their ends are closed by member 43 and a portion of the side of one member 32 is closed by a strip 44.
Affixed to the upper end of the shell por 95 tion 14 and extending radially relative to the axis of the vessel is a nose ring 45 As seen in FIGURE 3, the lower surface of the nose ring 45 is welded to the upper end of shell section 14 at a point displaced inwardly 100 from its outer periphery This defines a radially outwardly extending flange 46 which surrounds the upper end of shell portion 14 Also affixed to the upper surface of ring 45 is a second ring 47 having a smaller 105 diameter.
An arcuate plate 48 which is a segment of a frusto-conical section is secured above each cooling segment 30 a, 30 b, 30 c and 30 d to define a hollow passage 501 with the shell 110 portion 14, the member 32 and the ring 40.
More specifically, each member 48 is affixed at its upper end to the outer periphery of the nose ring 44 and at its lower end to the outer surfaces of the members 32 which 115 define its associated cooling segment and at a point adjacent their upper edges Thus, four passages 501 each intersecting a 90 central angle is defined by the outer surface of the shell portion 14, ring 40, members 120 32, the nose ring 45 and the plates 48.
A pair of substantially semi-circular members 50 and 52 are affixed to the surface of shell portion 14 and each is I-shaped in transverse cross-section The members 50 125 and 52 are generally equidistantly spaced apart and are parallel relative to each other and to the ring portion 42 A-first arcuate plate 54 which is substantially conexterisive with the member 50 is secured to the cool 130 1,584,940 ing segments 30 a-30 d and to member 50 and is oriented in spaced apart parallel relation relative to the surface portion 14 Similar member 56 is secured between members 50 and 52 and is also disposed in spaced apart parallel relation relative to shell portion 14 This defines a pair of substantially semi-annular passages 58 and 60 disposed below and arranged generally normally to the passages 38 of segments 30 a, 30 b, 30 c and 30 d The member 50 and 52 and the plates 54 and 56 span the cooling segments c and 30 d and overlap the edges of the other segments 30 a and 30 b Accordingly, the passages 58 and 60 are disposed adjacent at least some of the passages 38 of each cooling segment.
The cooling segments 30 a, 30 b, 30 c and d are substantially identical except for their relationship to the inlet and outlet passages as will be discussed below and except for the shortened portion of segment 30 b.
Accordingly, only one segment 30 b will be discussed in detail for the sake of brevity.
As seen in FIGURE 5, each of the angle members 32 of segment 30 b except those at the ends of each cooling segment 30 ad have a recessed portion 62 formed in one end of its respective leg 34 with the members 32 arranged such that the gaps 62 are at alternate ends of adjacent members 32 The members 32 ‘ which define the end of segment 30 b are ungapped to prevent flow of cooling water between segments 30 b and 30 a Similarly, the first member 32 of segment 30 c is ungapped to prevent cross water at the junction of segments 30 b and c Also, the member 32 » 1 at the opposite end of segment 32 b is imperforate to separate inflowing and outflowing water streams.
Member 40 has an opening 64 at each of the opposite ends of that portion within segment 30 b and corresponding to the flow passages 38 a and 38 b at the ends of the segment This provides communication between the passage 501 and the end passages 38 a and 38 b Wall members 65 separate the passage 501 into segments corresponding to each of the cooling segments 30 a, 30 b, 30 c and 30 d In addition, the lower end of one end passage 38 b in each cooling segment is connected by a shunt pipe 66 to the passage Member 42 also has an opening 70 formed therein at a point immediately below the passage 38 c which is immediately adjacent the passage 38 b Further, a cooling water inlet pipe 72 (FIGURE 2) is connected to member 54 at its approximate midpoint and a cooling water outlet pipe 74 is connected to the aproximate midpoint of member 56.
Referring now to FIGURES 2 and 5, it will be appreciated that when cooling water is delivered through inlet pipe 72 to the passage 58, it will flow into each of the segments 30 a, 30 b, 30 c and 30 d through the passages 38 c The cooling water will then traverse each of the passages 38 in each segment with the water in adjacent passages 38 flowing in opposite directions Upon reaching the upper end of passage 38 a, the water will exit through aperture 64, and then flow the entire length of the passage 50 ‘ after which it will flow downwardly through passage 38 b, continue through shunt pipe 66 and into the passage 60 for flow to the outlet pipe 74.
It can be seen from the foregoing that the cooling water will be flowing in all parts of the cooling assembly for cooling substantially the entire nose cone section 14 In addition, because the flow passages through which the cooling water traverses are relatively narrow, a high cooling water velocity can be maintained This provides the desired heat transfer and also retards nucleate boiling The configuration also provides a smooth outer surface on the cooling assembly 28 which facilitates the removal of solidified slag or skull and minimizes the external pipe connections.
While only a single embodiment of the present invention has been illustrated and described, it is not intended to be limited thereby but only by the scope of the appended claims.

Claims (9)

WHAT WE CLAIM IS – 1 A metallurgical vessel having an upper end which defines a generally frusto-conical 100 section and a top opening, cooling means disposed on the surface of said vessel adjacent to and disposed in a generally surrounding relation to said opening, said cooling means including a plurality of elongate 105 members having first and second legs which are generally perpendicular one to the other in transverse section, said members being affixed to the surface of said vessel in a side-by-side relation and extending in axial 110 planes of the frusto-conical section and having one end remote from said opening and another end proximate thereto to define a plurality of flow passages, wherein, in each member, the first leg is affixed to the vessel 115 and extends generally outwardly relative to the surface thereof and the second leg is integral with the first leg and is oriented generally parallel to the surface of the vessel, said second leg being affixed to the adjacent 120 member whereby passages are defined between adjacent members and the surface of the vessel the second legs of the members being configured such that all of the second legs when in abutment provide a generally 125 smooth frusto-conical surface substantially parallel to the surface of said section, the first legs of at least a plurality of said members having openings formed therein for interconnecting the passages formed thereby, 130 3.

1,584,94 PO an inlet connected to the remote end of one of the passages and an outlet connected to the proximate end of another one of the passages.

2 A vessel as claimed in claim 1, wherein first and second elongate means are disposed respectively adjacent the one and opposite ends of said flow passages for defining elongate flow passageways generally normal to said flow passages, an opening formed in the first legs of a plurality of said members so that the flow passages defined by said members are interconnected, closure means disposed at the opposite ends of said members for closing the same, said closure means having openings adjacent the ends of certain ones of said flow passages for connecting the same to said flow passageways, said first elongate means being generally annular and surrounding the open top of said vessel to provide a cooling ring therefor, one of said flow passageways being connected to a drain and the other to an inlet.

3 A vessel as claimed in any of claims 1 or 2, wherein one of said elongate flow passageways is in communication with one end of a first and second spaced apart ones of said plurality of flow passages, said flow passageway at least partially surrounding said vesssel top opening, the other end of one of said first and second flow passages being connected to a drain, one end of a flow passage adjacent one of said first and second flow passages being connected to an inlet, first and second spaced apart apertures formed in the first closure and adjacent the ends of the first and second spaced apart ones of the plurality of flow passages, the second closure having a third aperture for connecting the other end of one of the first flow passages to the inlet, a fourth aperture formed in one of the members disposed adjacent the first flow passage for connecting the passage defined by said one member to a cooling fluid outlet.

4 A vessel as claimed in any of claims 1-3, wherein in that the vessel includes a nose ring disposed in surrounding relation to the vessel opening and having a peripheral margin which extends outwardly from the surface of said vessel, the flow passageway being defined by an arcuate plate affixed at one end to the periphery of said nose ring and at its other edge to the surface defined by the second legs of said members.

A vessel as claimed in any of claims 1-4, wherein said vessel has a substantially frusto-conical upper end, said cooling means being frusto-conical and engaging frustoconical portion of said vessel in surrounding relation and disposed beyow the vessel opening.

6 A vessel as claimed in any of claims 1-5, wherein a plurality of said members have recesses formed in the first leg portions thereof for communication with adjacent passages, spaced apart ones of said members being imperforate to define isolated cooling segments spaced around said vessel, each of said cooling segments having passages at the opposite ends thereof communicating with the elongate flow passageway and one of said end passages communicating with said drain, another one of the passages of each segment communicating with said inlet.

7 A vessel as claimed in any of claims 1-6, wherein first and second plates are affixed to said vessel surface in general parallelism with the surface defined by the second legs of said members, said plates overlapping at least a portion of each of said cooling segments and defining the inlet and drain passages.

8 A vessel as claimed in any of claims 1-7, wherein the opening is provided in a first leg of at least a plurality of each of said members with the opening disposed at the opposite ends of adjacent members whereby cooling fluid will pass between adjacent members at the ends thereof and wherein said cooling fluid will flow in opposite directions and adjacent members.

9 A metallurgical vessel substantially as herein described with reference to and as shown in the accompanying drawings.
For the Applicants:
RAWORTH, MOSS & COOK, Chartered Patent Agents, 36 Sydenham Road, Croydon, Surrey CR O 2 EF, and 6 Buckingham Gate, Westminster, London SW 1 E 6 JP.
Printed for Her Majesty’s Stationery Office by Burgess & Son (Abingdon), Ltd -1981.
Published at The Patent Office, 25 Southampton Buildings, London, WC 2 A l AY, from which copies may be obtained.

GB24134/78A
1977-06-30
1978-05-30
Cooling assembly for metallurgical vessels

Expired

GB1584940A
(en)

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

US05/811,571

US4128232A
(en)

1977-06-30
1977-06-30
Cooling assembly for metallurgical vessels

Publications (1)

Publication Number
Publication Date

GB1584940A
true

GB1584940A
(en)

1981-02-18

Family
ID=25206921
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB24134/78A
Expired

GB1584940A
(en)

1977-06-30
1978-05-30
Cooling assembly for metallurgical vessels

Country Status (8)

Country
Link

US
(1)

US4128232A
(en)

CA
(1)

CA1095709A
(en)

DE
(1)

DE2828895A1
(en)

ES
(1)

ES470907A1
(en)

GB
(1)

GB1584940A
(en)

IT
(1)

IT1096877B
(en)

MX
(1)

MX146739A
(en)

ZA
(1)

ZA783728B
(en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

DE19730250C1
(en)

1997-07-08
1998-08-06
Mannesmann Ag
Steelworks converter with cap cooling

CA2427409C
(en)

2003-05-01
2007-03-20
Whiting Equipment Canada Inc.
Cooling system for a trunnion ring and metallurgical furnace vessel

WO2011044676A1
(en)

2009-10-14
2011-04-21
Absolute Combustion International Inc.
Cooling jacket, heat transfer apparatus and heat recovery apparatus

US8268233B2
(en)

2009-10-16
2012-09-18
Macrae Allan J
Eddy-free high velocity cooler

Family Cites Families (3)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US3679195A
(en)

1970-08-21
1972-07-25
Dravo Corp
Nose ring for metallurgical processing vessels

US3682460A
(en)

1971-02-03
1972-08-08
Chicago Bridge & Iron Co
Converter vessel with heat shield about its tap hole

AT338307B
(en)

1973-07-23
1977-08-25
Voest Ag

METALLURGICAL VESSEL, IN PARTICULAR CONVERTER

1977

1977-06-30
US
US05/811,571
patent/US4128232A/en
not_active
Expired – Lifetime

1978

1978-05-26
CA
CA304,192A
patent/CA1095709A/en
not_active
Expired

1978-05-30
GB
GB24134/78A
patent/GB1584940A/en
not_active
Expired

1978-06-19
ES
ES470907A
patent/ES470907A1/en
not_active
Expired

1978-06-29
ZA
ZA00783728A
patent/ZA783728B/en
unknown

1978-06-29
IT
IT25150/78A
patent/IT1096877B/en
active

1978-06-30
DE
DE19782828895
patent/DE2828895A1/en
not_active
Withdrawn

1978-06-30
MX
MX174018A
patent/MX146739A/en
unknown

Also Published As

Publication number
Publication date

DE2828895A1
(en)

1979-01-18

CA1095709A
(en)

1981-02-17

US4128232A
(en)

1978-12-05

ES470907A1
(en)

1979-10-01

ZA783728B
(en)

1979-08-29

IT7825150D0
(en)

1978-06-29

IT1096877B
(en)

1985-08-26

MX146739A
(en)

1982-08-04

Información de contacto