The invention relates to a device for heat treating metallic webs in-line, i.e. said webs pass the treatment device continuously, in particular for operation with a low-density protective gas, such as for example a nitrogen-hydrogen mixture with a high proportion of hydrogen.
In-line plants are very important in heat treating webs of both ferrous and non-ferrous metal alloys, such as for example copper alloys. In the case of webs whose surface can oxidise during heat treatment, in-line heat treatment is usually performed using a protective gas. This protective gas can consist mainly of nitrogen. For some heat treatment processes, however, it is useful to use a protective gas with a high proportion of hydrogen, or even pure hydrogen.
Using pure hydrogen as the protective gas affords the advantage of better heat transfer, such that for the same length of the plant, a substantially higher throughput can be achieved than with nitrogen.
Since high demands are generally made on the quality of the surface of webs of both ferrous alloys and non-ferrous metal alloys, the modern prior art is to guide said webs in a non-contact process. This is achieved by hanging the web vertically in a tower furnace, or in a horizontal furnace by assuming a catenary which is set by the effect of gravity.
A particular disadvantage of the catenary is that, for larger web lengths in the heat treatment portion, both high web sagging and high web tension occur. This greatly limits the throughput of such plants.
In order to avoid these disadvantages, plants with horizontally guided webs have been developed in which the web is stabilised and supported in its horizontal position in the treatment portion by means of suspension nozzles. A precondition of such plants, however, is that a sufficiently high load capacity can be achieved, which at high temperatures, with low-density protective gas such as for example a nitrogen-hydrogen mixture with a high proportion of hydrogen, and heavy webs causes major problems. Therefore, when a decision has been made to advantageously use a protective gas with a high proportion of hydrogen, one is often forced to use the aforementioned tower furnaces plants or plants which guide the web in accordance with a catenary.
It is an object of the invention to provide a device which combines the advantages of guiding the web by means of stabilising suspension nozzles with the advantages of tower furnaces plants and plants which guide the web in accordance with a catenary, without having to accept the disadvantages of the known plant.
This is achieved by a combination of the features listed in the characterising portion of the main claim.
Expedient embodiments are defined by the sub-claims.
In the following, the invention is explained in more detail by way of example embodiments and by referring to the enclosed, schematic drawings.
There is shown:
In the embodiment of the device in accordance with
Nozzle systems 8u and 8o for the heating portion 4 and 9u and 9o for the cooling portion 5, shown schematically, are provided above and below the web 1. With the aid of these blowing systems, which are embodied as suspension nozzles which support and simultaneously positionally stabilise the web, preferably as known from EP 0 864 518 B1, the web 1 is held in a particular position, such that the web tension required can be reduced due to the supporting effect of the nozzle systems 8 and 9. The device is therefore also capable of guiding comparatively heavy metal webs of high-density metal with relatively little sagging, since a portion of the weight is supported by the stabilising suspension nozzle system. These nozzle systems can also simultaneously exert a particularly pronounced laterally stabilising effect on the web in the area of greatest concave curvature. In the case of thin webs, the web can be guided in the same form using the same system with no appreciable tensile forces, since in this position the web finds a stable position, such as between gas springs, due to the stabilising suspension nozzle systems.
A sensor 10 serves to monitor the position of the web and is arranged in the vicinity of the trough of the course of the web. Said sensor can for example be a sensor 10 which operates using microwaves in accordance with the principle of radar. It is advantageous to arrange a number of sensors over the width of the web, since the width of the web can be varied during operation for one and the same device. In this way, a number of sensors are available with wide webs 1, while at least one sensor 10 always reliably detects the position of the web in the case of the narrowest web 1.
In the descending run of the web, the web 1 passes first through the heating portion 4 and then through the first area of the cooling portion 5. The stabilising blowing nozzle systems 8l, 8r for the heating portion and 9l, 9r for the cooling portion are situated on both sides of the web 1.
At the lower end, the web's course has a concave curvature (as viewed from above). This course is situated in a fluid 12, e.g. water. This fluid 12, generally a suitable liquid, simultaneously demarcates the inner space of the encasing 6 against the outer atmosphere and thus separates the protective gas from the ambient air.
In the fluid basin, nozzle systems 9i, 9a are situated on both the inner curvature and the outer curvature and act in a similar way to the systems 8 and 9 which operate in the gas atmosphere, but are specially adapted to and designed for operating with confirming fluid, and direct the fluid, in particular water, onto the web 1. The jets of these fluid nozzles 9i, 9a exert stabilising forces onto the web which also guide thin webs 1, which would otherwise deviate, in the desired concave form. In a particularly advantageous embodiment, these nozzle systems also have a positionally stabilising effect in the direction perpendicular to the run of the web, similar to a web centring control. It is, however, also possible to arrange such stabilising nozzles only in the area of the vertical legs of the run of the web, which localise the area which is curved concave, such that the run of the web in between can be freely set and only the position in the lowest area is monitored by the sensor 10.
The position of the run of the web is detected and controlled at the trough of the concave curvature by means of at least one sensor 10, such that the desired form is maintained in all operational conditions. In a liquid as the confirming fluid, the altitude of the web is advantageously detected in accordance with the principle of echo-location.
Below the second turning roller 2, which localises the treatment area of the web, there is situated a shutter means 43 which consists of two shutters which move perpendicular to the web. The web input opening, which is formed by the input collar 44—which is advantageously water-cooled and provided with thermal insulation—and opens into the heating portion 4 which can also be operated at a significant temperature of for example approx. 950° C., is shut with the aid of said shutter means 43, such that no heat can emerge upwards from the heat treatment portion 4 while the web is stalled, where it may result in damage to the turning roller 42 and/or its coating.
Another cooling device (not shown) can be provided between the turning roller 42 and the entrance 7 of the web into the heat treatment portion 4, said cooling device ruling out unacceptably high roller temperatures. Such a cooling means can for example operate by blowing the web with low-temperature protective gas. It can also be advantageous to arrange the combination of rollers 40, for reducing the web traction to the lower value in the treatment portion, directly before the entrance of the web into the same, such that the roller 2 is unnecessary.
The heat treatment portion 4 and the first area of the cooling portion situated below it are indicated in
The stabilising nozzle fields 23 are arranged on the outer side of the leg of the U facing the web 1. In the space enclosed by the legs of the U, jet heating pipes 25 are situated in the heating zones 4 and coolers 28, in particular heat exchangers, are situated in the cooling zone 5. Radial fans 21 serve to drive the flow and are inserted into the outer wall by means of bucklers filled with insulation material. The flow casings 20 are connected via crown-like structures 22 to the supporting structure of the fan 21 and thereby in turn to the supporting structure of the outer casing 6. Force is transferred at the tips of the crown teeth.
Embodying this attachment in the form of crowns ensures that no dents, fractures or similar difficulties can occur due to thermal tension and thermal expansion.
The zones are demarcated from each other in the heating portion by means of trapezium sheet metal bases 26. In the case of the first base 26, another layer of insulation material 27 is situated below said trapezium sheet metal, such that a temperature difference can be set and maintained between the first zone and the second zone. This embodiment of the intermediate base 26 in conjunction with thermal insulation 27 is of course possible between all the zones.
The wall design shown in
A further film 33 made of highly refractory material serves to cover the wall, onto which relatively small-format sheet metal elements 35, preferably made of perforated sheet metal, are layered as mechanical protection. All the layers are held by platelets 36 which are slid onto the pins 31. In order to be able to easily exchange the outer fibre layers, it is expedient to also apply such platelets, preferably produced from thin sheet metal, to the first film layer, as an intermediate attachment.
As may be gathered from the above description, the web 1 is blown with impact jets of heating and/or cooling fluid, in particular a gas, e.g. pure hydrogen or a hydrogen-nitrogen mixture with a high proportion of hydrogen, which exert a planar force on the web 1 which, similar to a spring, increases with decreasing distance between the web 1 and the nozzle field; this results in a positionally stabilising effect on the web, the magnitude of said stabilising force depending on the dynamic pressure of the blowing fluid at the nozzle output of the impact jets.
The distance between the nozzle fields, arranged on both sides of the web 1 in the heat treatment portion, is substantially constant in each of the two areas, i.e. heating 4 and cooling 5, meaning that the change in distance is ±10% at most.
A suitable nozzle system for achieving the desired effect is described in EP 0 864 518 B1 and has nozzle panes which are consecutive in the direction of the run of the web and comprise nozzle openings made of round holes and/or slit nozzles, wherein the width of the nozzle panes—measured parallel to the direction of the run of the web—changes over the width of the nozzle field—measured perpendicular to the direction of the run of the web. The nozzle panes are at least partially bordered at their circumference by slit nozzles.
This stabilising nozzle system can be embodied and operated such that the web 1 is also stabilised perpendicular to the run of the web by the nozzle system, said laterally stabilising effect being particularly pronounced in the area of the run of the web having a concave curvature (as viewed from above).
Any suitable fluid can be used as the confining fluid for the area 12, wherein a liquid is preferably used. A suitable liquid can be selected by taking into account its chemical compatibility with the material of the metallic webs.
Using this device, both ferrous and/or steel webs and webs of non-ferrous metals can be treated.
Number | Date | Country | Kind |
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103 03 228 | Jan 2003 | DE | national |
Number | Name | Date | Kind |
---|---|---|---|
3590495 | Tyson et al. | Jul 1971 | A |
3834040 | Russell et al. | Sep 1974 | A |
5070627 | Zagar | Dec 1991 | A |
5172844 | Mueller | Dec 1992 | A |
6049995 | Rogne et al. | Apr 2000 | A |
6088930 | Robin et al. | Jul 2000 | A |
Number | Date | Country |
---|---|---|
0 864 519 | Sep 1998 | EP |
55047326 | Apr 1980 | JP |
57039133 | Mar 1982 | JP |
58045334 | Mar 1983 | JP |
58048641 | Mar 1983 | JP |
58048641 | Mar 1983 | JP |
58193351 | Nov 1983 | JP |
63277165 | Nov 1988 | JP |
02061011 | Mar 1990 | JP |
07090618 | Apr 1995 | JP |
Number | Date | Country | |
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20040154182 A1 | Aug 2004 | US |