Patent Application
20090221415
The invention relates to novel sintered refractory products exhibiting enhanced thermal shock resistance.
Among refractory products, fused-cast products and sintered products may be distinguished.
Contrary to sintered products, fused-cast products most often have an intergranular glassy phase linking the crystallized grains. The problems posed by sintered products and fused-cast products and the technical solutions for solving them are thus generally different. A mixture developed for manufacturing a fused-cast product therefore is not a priori usable as such for manufacturing a sintered product and vice versa.
Sintered products, depending on their chemical composition and mode of preparation, are intended to be used in a wide variety of industrial applications.
Examples of sintered products include, in particular, alumina-zirconia-silica products, usually referred to as AZS, as well as so-called aluminous products, which are used, in particular, in certain regions of glassmaking furnaces.
Products such are those described in patent FR 2 552 756 in the name of Emhart Industries are generally appropriate for such an application. Products such as BPAL, ZA33 or ZIRAL, which are manufactured and marketed by Saint-Gobain SefPro are also particularly well suited and presently widely used in certain regions of glassmaking furnaces.
Also known from EP 0 404 610 are refractory mixtures containing monoclinic zirconia, from which products exhibiting outstanding thermal shock resistance can be obtained.
However, glass or energy producing industries need refractory products exhibiting ever greater levels of performance.
The object of the present invention is therefore to provide a refractory product exhibiting enhanced thermal shock resistance and hot mechanical strength, corrosion resistance and porosity properties similar to or better than those of presently used refractory products.
According to the invention, this object is achieved by means of a sintered refractory product having the following average chemical composition, the percentages being by weight on the basis of the oxides:
20%<Al2O3<90%
2%<SiO2<30%
3%<ZrO2<50%
0%=Cr2O3<50%,
which is characterized in that it comprises, as a percentage by weight on the basis of the oxides, 17 to 85% of mullite-zirconia grains.
As shown below, the sintered refractory product of the invention exhibits surprisingly enhanced thermal shock resistance.
Preferably, the product according to the invention also has one or more of the optional following characteristics:
The invention also relates to the use of a refractory product according to the invention such as a shaped refractory part for shaping molten glass to be used as a consumable layer or a refractory lining, in particular in the combustion chamber of an industrial facility.
By “mullite-zirconia grain” is meant a refractory grain produced by sintering or fusing having a chemical composition containing, as its major constituents, alumina (Al2O3), silica (SiO2) and zirconia (ZrO2), wherein silica and alumina are present in the form of 2 SiO2-3 Al2O3 (mullite). Alumina (Al2O3), silica (SiO2) and zirconia (ZrO2) thus are the three main constituents, by weight, of a mullite-zirconia grain.
The “size of a grain” refers to its largest dimension. It is considered that, by definition, a “grain” has a size of less than 4 mm.
For manufacturing a refractory product according to the invention in the form of a sintered block, i.e. of a shaped part sintered before it is placed in its operational position, a manufacturing process comprising the following consecutive steps can be performed:
Steps a) to e) are steps conventionally carried out for the manufacture of sintered products.
In step a), the starting charge is made of a variety of raw materials, the chemical composition and granulometric distribution of which may vary. According to the invention, it contains, the percentages being by weight on the basis of the refractory oxides, 17 to 85% of mullite-zirconia grains, as well as any refractory material allowing the desired overall composition to be achieved, such as tabular alumina, electrofused corundum, zircon, chromium oxide, in particular sintered in the form of chamotte, electrofused materials, such as those based on Al2O3—ZrO2—SiO2, alumina, fumed silica, monoclinic and/or stabilized zirconia, chromium oxide pigment, and the like.
The starting charge is determined so that the product obtained after step e) conforms to the invention and further exhibits one or preferably several of the preferred characteristics of the product according to the invention.
The starting charge preferably contains, as a percentage by weight on the basis of the oxides, at least 1%, preferably at least 1.5% of mullite-zirconia grains having a size of 0.3 mm or less. These grains may be added in any appropriate granulometric class, such as, without any limitation thereto, 0-0.7 mm, 0-0.3 mm or 0-0.15 mm.
The starting charge may also contain one or more additives in a particulate form so as to provide the starting charge with sufficient plasticity during the shaping step b) and for providing the preform obtained at the end of step d) with sufficient mechanical strength. The amounts of additives are non-limiting. In particular, the amounts conventionally used in known sintering processes are appropriate.
Certain oxides may be introduced via the additives.
Non-limiting examples of usable additives include:
These additions introduce alumina and silica and a few alkali or alkaline earth metal oxides, or even iron oxide, according to the type of clay.
In cases where the refractory mixture contains a chemical or hydraulic binder, it is then a concrete, which, for example, may be used in practice via vibration casting.
Preferably, the starting charge contains less than 1% MgO, by weight on the basis of the oxides, and more preferably, contains no MgO, except in the form of impurities, i.e. in amounts of 0.5% or less, preferably less than 0.2%. The process is thus made simpler.
In order to obtain a refractory product according to the invention at the end of step e), the starting charge exhibits the following average chemical composition, as percentages by weight on the basis of the refractory oxides:
20%<Al2O3<90%
2%<SiO2<30%
3%<ZrO2<50%
0%=Cr2O3<50%
and comprises 17 to 85% of mullite-zirconia grains, the percentages being by weight on the basis of refractory oxides.
Water is also conventionally added to the starting charge.
The mixture of the various starting charge constituents is continued until a substantially homogeneous starting charge is obtained.
In step b), the charge is shaped and placed in a mold.
In case the shaping is performed by pressing, a specific pressure of 400 to 800 kg/cm2 is appropriate for a non-plastic paste. Pressing is preferably carried out uniaxally or isostatically, for example using a hydraulic press. It may advantageously be preceded by a manual or pneumatic and/or vibrational ramming operation.
Drying in step d) can be carried out at a moderately high temperature. Preferably, it is carried out at a temperature in the range of room temperature to 200° C. It conventionally lasts between 10 hours and one week, depending on the format of the preform, until the residual moisture content of the preform is less than 0.5%.
The dried preform is then fired (step e)) in order to sinter it. The sintering operation is well known to those skilled in the art. Sintering corresponds to a thermal consolidation of the material. It is generally accompanied by a decrease in porosity and by a dimensional shrinkage.
The sintering temperature depends on the starting mixture composition, but a temperature between 1300 and 1800° C. is appropriate in most cases. Sintering is preferably carried out in an oxidizing atmosphere, and more preferably in air, preferably at atmospheric pressure. The firing period, between about 1 and 15 days cold to cold, depends on the materials and also on the size and shape of the refractory products to be manufactured.
Step e) transforms the preform into a refractory product according to the invention, which is particularly useful as a shaped refractory part used for shaping molten glass or as a refractory tile in the combustion chamber of an industrial facility.
Conventionally, the preform is fired in a firing furnace.
As opposed to products sintered in situ, i.e. sintered after having been placed in their operational position, for example after having been projected onto a wall to be protected, the block according to the invention results from a sintering within a firing furnace, so that each of its sides is heated in substantially the same manner, before being placed in its operational position. Therefore, this prevents any dependence of the temperature gradient on the position of a given point on the outer surface of the block. As opposed to in situ sintered products, the product according to the invention thus exhibits a homogeneous density and microstructure throughout, thus resulting in improved resistance to thermal shock, to corrosion by water vapor, and to corrosion by molten glass.
The refractory products according to the invention may then be used directly or after having been assembled by means of appropriate expansion joints, according to techniques well known to those skilled in the art.
The way the amounts of constituents are determined in the refractory product is well known to a person skilled in the art. In particular, a person skilled in the art is aware that the mullite-zirconia grains as well as the oxides Al2O3, SiO2, ZrO2 and Cr2O3 present in the starting charge are also found in the sintered refractory product. For the same quantity of constituents in the sintered refractory product, the starting charge composition may however change, depending on those quantities and on the nature of the additives present in said charge.
To further illustrate the invention, the following non-limiting examples are given.
In these examples, the raw materials employed were chosen from:
In step a), raw materials were metered in such a way that the starting charge had the desired average mineral chemical composition by weight, and then mixed in the presence of water and at least one dispersant, such as sodium phosphate.
The starting charge was then cast in a mold to form a green preform having sufficient mechanical strength to be manipulated. It was then dried for 12 hours at 110° C. The preform was finally sintered at a temperature of 1350° C. or 1630° C. so as to form a refractory block.
Samples were taken from the various block examples in order to prepare specimens in the form of 125×25×25 mm bars.
In order to measure thermal shock resistance properties, a standardized test known as PRE III. 26/PRE/R.5.1/78 was adopted. This test allows the thermal shock behaviour to be assessed using the relative loss of flexural strength (DELTA MOR) after one or more cycles, each consisting in heating the test specimen from room temperature (20° C.) up to a maximum temperature T of 1200° C., keeping the specimen at this temperature T for 30 minutes and then plunging the specimen into cold water.
The MOR is the modulus of rupture.
In the following tables, MOR20 corresponds to the MOR value of the sample at 20° C. before any thermal shock cycle, and MoRxcycle corresponds to the MOR value after “x” cycle(s) of thermal shock.
The compositions of the tested products as well as their characteristics are shown in Table 1.
The results show that an amount of more than 17% of mullite-zirconia grains is required in the starting charge refractory mixture so as to obtain a significant improvement in thermal shock resistance.
This is because, beyond this limit, it may be noted that the loss of MOR is limited and/or the MOR value at 20° C. is larger.
Further, tests have been carried out in order to assess the thermal shock resistance after water vapor corrosion.
Thus, samples were previously maintained in a furnace under a constant water vapor flow rate. After this treatment, they underwent the aforementioned thermal shock resistance test. The results are listed in Table 2, where MORcve is the MOR value of samples after water vapor corrosion, before any thermal shock cycle.
It is noted that the products according to the invention result in an enhancement of thermal shock resistance even after they have undergone water vapor corrosion.
Further, the products of examples 11 to 17 exhibit a molten glass corrosion resistance at least equivalent to that of the reference products.
The following Table 3 illustrates the benefit of the presence of grains having sizes smaller than 0.7 mm.
Comparison of examples A, B, C and D demonstrates the positive effect of a fine granulometric range (0-0.7 mm) on the modulus of rupture after a thermal shock and on the delta MOR, in particular after quenching. Examples E and F confirm this observation, and a content of 5% of said granulometric range is preferred.
The used mullite-zirconia grain mixtures in the 0-0.7 mm range contain generally between 30 and 50% by weight of grains smaller than 0.3 mm. Thus, example F contains between 1.5 and 2.5% of mullite-zirconia grains relative to the total composition weight, with a size of less than 0.3 mm. Preferably, the product according to the invention also contains at least 1%, preferably at least 1.5%, of mullite-zirconia grains having a size of 0.3 mm or less, the percentages being by weight on the basis of the oxides.
Furthermore, other tests have shown that the beneficial effect of adding mullite-zirconia grains is not affected by the presence of at least 50% of Cr2O3 (see examples 20 and 21). Although not preferred, the product according to the invention therefore advantageously and surprisingly tolerates high contents of Cr2O3. Furthermore, adding Cr2O3 advantageously improves resistance to corrosion by molten glass.
Of course, the aforementioned embodiments are merely examples that may be modified, in particular by substituting technical equivalents while still remaining within the scope of the present invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 05 09814 | Sep 2005 | FR | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/FR06/02180 | 9/25/2006 | WO | 00 | 6/3/2008 |
