[0001] The invention relates to a gasket arrangement between two refractory pouring elements
on the spout of a metallurgical vessel, preferably between a collector nozzle and
a submerged nozzle, comprising a gasket element made of compressible material.
[0002] These types of gasket arrangement are used in particular when casting steel using
the continuous casting method. Here the collector nozzle forms the outlet of a slide
closure or the like on a metallurgical vessel. The submerged nozzle connected to the
said collector nozzle conveys the molten steel into a metallurgical vessel or mould
suitable for this purpose.
[0003] This gasket arrangement formed between the submerged nozzle and the collector nozzle
prevents ambient air from being sucked into the molten metal between the latter when
casting. In order to guarantee the tightness of the seat, inert gas, the gas pressure
of which counteracts the negative pressure produced here during casting, is delivered
to the annular space located concentrically to said seat.
[0004] This type of gasket arrangement is disclosed in publication
DE-A-40 24 520. Compressible sealing rings are arranged here above and below the annular space which,
in co-operation with the gas pressure of the inert gas in the annular space, should
prevent the outflowing molten steel from coming into contact with the ambient air
when being cast and from oxidising as a result. This gasket arrangement is additionally
equipped with a device intended to indicate whether the sealing rings have sprung
a leak and so that there is a risk of ambient air being sucked into the casting channel.
This type of display device requires a large amount of apparatus and can not independently
re-establish the tightness of the system.
[0005] Additionally, the disadvantage of those sealing rings exists in the fact, that they
are not sufficient fixed in the submerged nozzle. With the connection of the submerged
nozzle onto the collector nozzle the sealing ring can move a little bit and in the
consequence a correct sealing is possibly not anymore fulfilled.
[0006] The object underlying this invention is to avoid this disadvantage and to provide
a gasket arrangement of the type specified at the start which, with simple means guarantees
an improved sealing between the nozzles with the gasket element.
[0007] This object is achieved according to the invention in that holding means are assigned
to the submerged nozzle or to the collector nozzle and to the gasket element by means
of which the gasket element is positioned in the inlet opening of the submerged nozzle.
[0008] Very advantageously, at least one groove is assigned to the submerged nozzle in the
sealing region and at least one outer lip, which can be pressed into this groove,
is assigned to the gasket element as holding means.
[0009] According to the invention the groove provided as an annular groove for receiving
the lip is preferably located centrally between the annular space which can be exposed
to inert gas and the upstream face surface of the submerged nozzle.
[0010] Furthermore, the invention makes provision such that the annular space which can
be exposed to inert gas is formed by an annular groove located in the submerged nozzle
and which can be connected to an inert gas supply line via a gas channel of the submerged
nozzle.
[0011] In addition, the invention makes provision such that the gasket element is formed
by a ridged gasket comprising an upper and a lower sealing flange, the lip preferably
being positioned centrally between the upper sealing flange and the annular space
which can be exposed to inert gas. This type of configuration facilitates fitting
and production of the gasket element as a one-part component.
[0012] In order to facilitate the fitting of the ridged gasket the invention makes provision
such that the lip is elastic. It is also advantageous if it has a preferably rectangular
cross-section adapted to the annular groove receiving it, as seen from the external
dimensions.
[0013] In another version the invention also makes provision such that the ridged gasket
has an annular groove with a recess arranged around the circumference and which can
be exposed to inert gas in the region of the seat. Therefore, the corresponding annular
groove in the submerged nozzle may be dispensable. In this version too the ridged
gasket is made in one part.
[0014] In the following the invention is described in more detail by means of an exemplary
embodiment with reference to the drawings. These are showed as follows:
- Fig. 1
- a first version of a gasket arrangement according to the invention shown in section,
- Fig. 2
- a longitudinal section through a submerged nozzle with the gasket arrangement according
to Fig. 1,
- Fig. 3
- a second version of a gasket arrangement according to the invention, partially shown
diagrammatically, and
- Fig. 4
- a third version of a gasket arrangement shown partially in a cross section.
[0015] A refractory submerged nozzle 1 as the one pouring element according to Fig. 1 and
Fig. 2 serves as an immersion tube for a continuous casting plant with a means for
regulating the flow, e.g. slide closure or stopper rod (not illustrated) the collector
nozzle 2 of which can be connected as a second pouring element, gas-tight, to the
submerged nozzle 1.
[0016] Needless to say this gasket arrangement can be used for various refractory sleeve
connections, for example between a collector nozzle and a so-called shroud tube. Instead
of a slide closure, a refractory metering nozzle or the like fitted to the spout of
a tundish can also be provided.
[0017] In order to seal the connection a gasket arrangement 3 is provided with a ridged
gasket 4. It forms the seat of the collector nozzle 2 in the submerged nozzle 1. In
order to fulfil its sealing function, it is produced from compressible fibre material
with refractory properties.
[0018] In the submerged nozzle 1 there is a gas channel 5 for conveying inert gas to an
annular space 6 of the submerged nozzle located concentrically in the region of the
seat. The gas channel 5 leads to a connecting piece 7 which can be connected to an
inert gas supply line (not shown). The connecting piece 7 is clamped securely to the
submerged nozzle 1 with a steel band 8. If the annular space 6 is exposed to inert
gas, a sealing effect is then produced in the region of the seat by the gas pressure
which is established and which counteracts the suction effect applied here when casting.
This sealing effect supports the sealing effect of the ridged gasket 4 sealing the
seat.
[0019] According to the invention the ridged gasket 4 has as holding means a lip 9 which
can be pressed into an additional groove 10 of the submerged nozzle 1. This groove
10 in the form of an annular groove is located approximately centrally between the
annular space 6 and the face surface 11 of the submerged nozzle. It is thus guaranteed
that it does not cause any appreciable weakening of the submerged nozzle.
[0020] This groove 10 could also be formed by just part of the circumference of the inlet
opening 1' of the submerged nozzle 1 and the lip 9 would then also accordingly not
be provided round the whole circumference.
[0021] The submerged nozzle 1 at its inlet opening 1' and the collector nozzle 2 projecting
into the latter on its outer surface 2' is formed such as to taper conically. The
ridged gasket 4 located between the latter is also in the form of a truncated cone.
The taper here is for example approximately 5° to 45°. This is associated with a further
advantage within the framework of the invention in so far as this ridged gasket 4
can be placed manually, without any particular effort, into the inlet opening 1' of
the submerged nozzle 1 and its lip 9 lying on the outside can be pressed into the
groove 10.
[0022] Moreover, the ridged gasket 4 has an upper sealing flange 12 and a lower sealing
flange 13 which co-operate with the upper face surface of the submerged nozzle 1 and
with the lower collector nozzle 2 and strike against these face surfaces. For the
purpose of comprehensive sealing the axial distance between the sealing flanges 12
and 13 is matched to the axial length of the seat. Therefore, the ridged gasket 4
can be fitted such that it is pressed, gas-tight, against the face surfaces of the
submerged nozzle and the collector nozzle.
[0023] This ridged gasket 4 and with it the lip 9 are elastic and the latter preferably
has a rectangular or similar cross-section that, with its outer dimensions, corresponds
to the cross-section of the annular groove 10. However, depending for example on the
intended sealing effect, the lip 9 and the annular groove 10 can also have a cross-sectional
geometry different from a rectangle.
[0024] The lip 9 can increase the sealing effect of the ridged gasket 4 with simple means
which are automatically effective after establishing the connection between the submerged
nozzle and the collector nozzle.
[0025] In the described exemplary embodiment the lip 9 is disposed upstream of the inert
gas seal in the direction of casting. However, the lip can in principle also be positioned
downstream of the inert gas seal.
[0026] The gasket arrangement according to Fig. 3 only differs from the arrangement according
to Fig. 1 and Fig. 2 in that in Fig. 3 the annular space which can be exposed to inert
gas is formed by a corresponding annular groove 14 in the ridged gasket 4 which has
a recess arranged around the circumference. The annular groove 14 is located within
the ridged gasket 4 such that it is positioned relative to the submerged nozzle 1
at the same level as the annular groove 6 provided in the submerged nozzle according
to Fig. 2.
[0027] This embodiment of the gasket is associated with the fact that the annular groove
6 in the submerged nozzle is then dispensable. This results in easier handling of
the submerged nozzle. The ridged gasket 4 is also made in one part in this embodiment.
This is advantageous for the production and fitting of the ridged gasket.
[0028] Fig. 4 shows a gasket arrangement with a refractory nozzle 22 and below a refractory
nozzle 21 with a gasket element 23 there between. The nozzle 22 is provided with a
surrounding shell 22' or the like, in which the nozzle 22 is mortared.
[0029] With this gasket arrangement the holding means are assigned to the upper nozzle 22
as lip 29 on the circumference of the shell 22' resp. to the compressible gasket element
23 as corresponding groove 30, thus instead to the joining nozzle 21.
[0030] Therewith, before the mounting of the lower onto the upper nozzle 21, 22 the gasket
element 23 can be put over that tapered circumference of the nozzle 22 and it is then
fixed suitable by these holding means. As a consequence it is again ensured, that
the gasket element 23 is not being moved at the moment when the lower nozzle 21 is
pressed to the upper.
[0031] The gasket arrangement according to the invention can also be used, as mentioned
above, in other similarly co-operating refractory pouring elements of metallurgical
devices, such as for example shroud pipes, immersion spouts and similar components.
[0032] The invention is sufficiently demonstrated by the exemplary embodiments described.
It could however also be made in other versions. Thus, conversely, on the submerged
nozzle a projecting lip to the inside and on the sealing element a corresponding groove
could be provided as holding means. In addition, the gasket element could also be
made without or with just one flange.
[0033] Theoretically, a groove could also be provided in the submerged nozzle in the sealing
region before and/or after the annular space as seen in the direction of casting,
into which a respective lip of the gasket element could be pressed. Just two grooves
without this annular space could also be provided.
[0034] Moreover there could be arranged as holding means vice versa a groove circumference
the collector nozzle and a lip protrudes inside of the gasket element. This groove
could be provided on the shell 22' or directly on the refractory nozzle, when at least
no shell would extend to the sealing region.
1. Gasket arrangement between two refractory pouring elements on the spout of a metallurgical
vessel, preferably between a collector nozzle (2) and a submerged nozzle (1), comprising
a gasket element (4) in the inlet opening (1') of the submerged nozzle, characterised in that there are provided for the submerged nozzle (1) or for the collector nozzle and the
gasket element (4) holding means by means of which the gasket element (4) is suitably
positioned.
2. Gasket arrangement according to Claim 1, characterised in that at least one groove (10) is assigned to the submerged nozzle (1) in the sealing region
and at least one lip (9), which can be pressed into this groove (10), is assigned
to the gasket element (4) as holding means, by means of which the gasket element (4)
is additionally positioned in the inlet opening (1') of the submerged nozzle (1).
3. Gasket arrangement according to Claim 2, characterised in that the groove (10) on the submerged nozzle (1) is in the form of an annular groove and
the outer lip (9) on the gasket element (4) is in the form of a ring.
4. Gasket element according to Claim 3, characterised in that the lip (9) is elastic and has a preferably rectangular cross-section which is made
in approximately the same form as this receiving groove (10).
5. Gasket arrangement according to any of the preceding Claims 1 to 4, characterised in that the submerged nozzle (1) at its inlet opening (1') and the collector nozzle (2) projecting
into the latter taper conically on their outer surface (2') and the gasket element
(4) located between the latter is also in the form of a truncated cone.
6. Gasket arrangement according to any of the preceding Claims 1 to 5, characterised in that the submerged nozzle (1) is provided with means for conveying inert gas into the
sealing region and with a corresponding annular space (6 and 14), the groove (10)
preferably being located centrally between the annular space (6 and 14) and the upper
face surface (11) of the submerged nozzle.
7. Gasket element for a gasket arrangement according to Claim 6, characterised in that the gasket element (4) is formed by a ridged gasket, the annular lip (9) preferably
being positioned above the annular space (6 and 14) which can be exposed to inert
gas.
8. Gasket element according to Claim 7, characterised in that the ridged gasket is formed by a lower and an upper radially outwardly extending
sealing flange (12, 13).
9. Gasket element according to Claim 8, characterised in that the two end side sealing flanges (12, 13) co-operate with the upper face surface
of the submerged nozzle (1) and with the lower face surface of the collector nozzle
(2).
10. Gasket element according to any of the preceding Claims 7 to 9, characterised in that the ridged gasket (4) in the region of the seat has an annular groove (14) which
can be exposed to inert gas and with a recess arranged around the circumference.
11. Gasket element according to any of the preceding Claims 7 to 10, characterised in that the ridged gasket (4) is made of refractory compressible fibre material.
12. Submerged nozzle, with an inlet opening (1'), characterised in that at least one groove (10) is assigned to the inlet opening (1') in the sealing region.
13. Submerged nozzle according to Claim 12, characterised in that the groove (10) is in the form of an annular groove in the tapered inlet opening
(1').
14. Refractory nozzle, in particular a collector nozzle, characterised in that holding means are assigned to the lower sealing region of the circumference.
15. Refractory nozzle, characterised in that as holding means one or more lips (29) are provided on the circumference of a shell
(22') encasing the nozzle (22).