ALUMINIUM-BASED ARTICLE HAVING A PROTECTIVE CERAMIC COATING, AND A METHOD OF PRODUCING IT

Abstract: Aluminium-based article having a heat and corrosion protective coating, especially engine parts such as piston crown or cylinder head, and a method of preparing said article. The coating consists of an aluminium-based bonding layer, preferably having a thickness in the range 0.1-0.6 mm, and an outer top layer of stabilized or partially stabilized zirconium dioxide, preferably having a thickness in the range 0.5-2.5 mm, and optionally a cermet layer, comprising zirconium dioxide and an aluminium-based metal component, between the bonding layer and the outer zirconium dioxide top layer. The bonding layer is applied to the substrate by thermal spraying of a rapidly solidified powder, substantially consisting of 60-80% by weight of Al and 40-20% by weight of Si, the particles of the powder having a frozen unstable micro-structure. The cermet layer desirably is a layer consisting of zirconium dioxide and an aluminium-based alloy, the metal content of the cermet layer decreasing substantially uniformly in the direction towards the outer zirconium dioxide top layer. The cermet layer preferably has a thickness in the range 0.2-0.6 mm. Also the cermet and zirconium oxide layers are deposited by thermal spraying.

Description: ALUMINIUM-BASED ARTICLE HAVING A PROTECTIVE CERAMIC COATING, AND A METHOD OF PRODUCING IT. This invention relates to an aluminum-based article provided with a heat barrier coating, especially engine parts such as piston crown or cylinder head a method of producing it, and the use of such coatings on aluminum- based surfaces for the protection against the effect of high temperatures, especially heat shock, and against corrosion; and the use of a special bonding layer. It is known that metal articles can be coated with a heat barrier making the article more resistant to high temperatures. For instance, it is known to coat e.g. an engine piston with ceramic materials. More particularly, it is known to coat aluminum-based (silumin) engine pistons with a heat barrier in the form of a sandwich coating comprising alternate layers of ceramic material, such as ZrO-,, and cermet layers in which zirconium dioxide may be included. A known coating of this type comprises a Ni-Al bonding layer on the substrate, fol¬ lowed by a cermet layer (30% NiAl, 70% ceramics) , a ceramic layer, and thereafter several cermet layers (70% NiAl, 30% ceramics) alternating with ceramic layers, the outer layer being ceramic. Such a sandwich coating, having ZrO-, as ceramics, has been tested, by the present inventor among others, using a test generally accepted for such coatings. This "accelerated" test essentially consists in subjecting the coating to treatment cycles comprising heating and guenching, each cycle consisting in that the coating is exposed for fifteen seconds to a flame having a temperature of 1100 C, whereupon the coating is water cooled for fifteen seconds, followed by drying with pressurized air. It was found that said sandwich coating does not meet the usual requirements of heat resistance for coatings on aluminum alloy. Cracks/flakes arose, first in the cermet material, and then the ZrO-, top layer began to spall. To my knowledge it has not till now been reported that ceramic coatings have been made to adhere durably on aluminum alloys, tested in the above mentioned generally accepted way. For iron/steel substrates it is known to use a bonding layer of MCr A1Y, wherein M = Ni, Co, Fe or NiCo. For Al-based substrates it is known, as mentioned above, to use a bonding layer of nickel aluminide, i.e. nickel is the main metal. It was now found that heat barrier coatings in¬ cluding an outer top layer of stabilized or partially stabilized ZrO,. can advantageously be deposited on substrates of aluminum alloy, such as silu in, by means of a special bonding layer of aluminum alloy. Prefer¬ ably a cermet layer is used between the bonding layer and the outer ZrO- top layer. Thus, the invention relates to an aluminium-based article having a heat and corrosion protective, heat shock resistant coating/ especially engine parts such as piston head, cylinder head or cover, characterized in that it has a coating consisting of an aluminium- based bonding layer and an outer top layer of stabilized or partially stabilized zirconium dioxide, and option¬ ally a cermet layer, comprising zirconium dioxide and an aluminum-based metal component, between the bonding layer and the outer zirconium dioxide top layer. The bonding layer preferably has a thickness in the range 0.1 - 0.6 mm, especially about 0.3 mm. The outer top layer of stabilized or partially stabilized zirconium dioxide perferably has a thickness in the range 0.5 - 2.5 mm, especially 1.0 - 1.5 mm. A preferred embodiment of the article according to the invention resides in that the bonding layer is applied by thermal spraying of a rapidly solidified powder. The particle sizes of the powder preferably lie in the range 5 μm - 60 /urn, especially 10 - 40 μm. According to a further, preferred embodiment the bonding layer substantially consists of 60 - 80% by weight of Al and 40 - 20% by weight of Si. Thus, said powder preferably has this composition. Another preferred embodiment resides in that the cermet layer is a layer substantially consisting of zirconium dioxide and an aluminum-based alloy, prefer¬ ably an alloy of 60 - 80% by weight of Al and 40 - 20% by weight of Si, and that the metal ratio of the cermet layer decreases substantially uniformly in the direction towards the outer zirconium dioxide top layer, the zirconium dioxide ratio of the cermet layer increasing from 0 farthest in to 100% zirconium dioxide at the • transition into the outer top layer. The cermet layer preferably has athickness in the range 0.2 - 0.6 mm. According to a further, preferred embodiment of the article according the invention the outer top layer of stabilized or partially stabilized r0 2 has a porosity in the range 5 - 15% by volume. The invention also includes a method of preparing an aluminum-based article having a heat and corrosion protective, heat shock resistant coating, especially engine parts such as piston head, cylinder head or cover, and the method is characterized by applying to the surface to be coated an Al-based bonding layer, preferably having a thickness in the range 0.1 - 0.6 mm, especially about 0.3 mm, and an outer top layer of stabilized or partially stabilized zirconium dioxide, preferably having a thickness in the range 0.5 - 2.5mm, especially 1.0 - 1.5 mm, and optionally a cermet layer, comprising zirconium dioxide and an aluminium-based metal component, between the bonding layer and the outer zirconium dioxide top layer. According to a preferred embodiment of the method of the invention the bonding layer is applied by thermal spraying of a rapidly solidified powder, preferably a powder having particle sizes in the range 5 urn - 60 jum, especially 10 - 40 /urn. According to a further, preferred embodiment of the method, an alloy substantially consisting of 60 - 80% by weight of Al and 40 - 20% by weight of Si is used as aluminum-based alloy for the bonding layer. According to another preferred embodiment of the method there is applied as cermet layer a layer substan¬ tially consisting of zirconium dioxide and an aluminium- based alloy, preferably an alloy of 60-80% by weight of Al and 40-20% by weight of Si, the cermet layer being applied having a substantially uniformly decreasing metallic proportion, considered in the direction to¬ wards the outer zirconium dioxide top layer, the zirconium dioxide proportion of the cermet layer in¬ creasing correspondingly from zero farthest in to 100% zirconium dioxide at the transition into the outer top layer. The cermet layer is preferably given a thickness in the range 0,2-0,6 mm. According to a further preferred embodiment of the method according to the invention the cermet layer is applied by thermal spraying, the substrate being main¬ tained at a temperature of about 300°C during spraying using gas cooling, for instance with a mixture of air and CO-,, the substrate being preferably maintained at about 300 C also during the spraying of the initial 100-200 /am of the ZrO-, layer, whereafter the remainder of the ZrO~ layer is sprayed using controlled cooling, preferably with CO- gas, such that the surface tem¬ perature of the work-piece gradually falls to about 100 C at the end of the ZrO- spraying. The zirconium dioxide layer can be applied by thermal spraying in a conventional manner. While a surface temperature of about 300°C is preferred for the substrate during spraying of the cermet layer, it has been found advantageous for the purposes of the inven¬ tion to cool the work-piece (the substrate, for instance piston crown) somewhat more strongly during the spraying of the zirconium dioxide layer, i.e. such that the sur¬ face temperature gradually falls to about 100°C at the end of the entire spraying operation. Most preferred, however, is the use of the modification of the cooling which resides in that the surface temperature of about 300 C is maintained also during the spraying of the initial 100-200 /urn, preferably about 150 μm, of the zirconium dioxide layer, whereupon a stronger cooling with gas is started. Control of the cooling is readily achieved by a suitable choice of cooling gas and.the temperature thereof. The expressions "stabilized" and "partially stabilized" , which are known to those skilled in the art, refer to the fact that the ZrO- lattice can be stabilized by means of other oxides, especially Y^^ i and MgO. Powders of so stabilized or partially sta¬ bilized ZrO- are commercially available. For the pur¬ poses of the invention there is preferably used a par¬ tially stabilized cubic ZrO-- containing up to 20% by weight of Y ? 0-, preferably about 8% by weight of Y--.0-, or up to 24% by weight of MgO. The expression "rapidly solidified metal powder" is well known to metallurgists. Rapid solidification is used to "freeze" a desired, unstable metal struc¬ ture which would not be obtained if for instance metal droplets are cooled slowly. Rapid solidification is especially applicable when it is desired to obtain an alloy having greater solubility for one or more alloy components, or in order to avoid segregation in the ma¬ terial, that is achieve greater homogeneity. The pro¬ duction of rapidly solidified metal powders is generally known. Such metal powders are usually produced using a cooling rate of the order of magnitude of 10 6 °C/minute. However, a cooling rate as high as 10 °C/minute is not always required in making powders suitable for use in this invention as a lower cooling rate may provide a micro-structure homogeneity which is sufficient for some applications. Ceramic coatings on combustion engine parts which are to be exposed to high temperatures must have good thermal shock and adherence properties, and good erosion and corrosion characteristics. The bonding layer which is used according to the invention has been found to be of decisive importance in order to obtain a success¬ ful total coating having a long life. It has been found that the bonding layer should have a thickness in the range of about 0.1-0.6 mm, pre¬ ferably about 0.3 mm. If the bonding layer is thinner than 0.1 mm it tends to be inadequate in its main function, which is to bond the underlying substrate to the overlying layer, and a bonding layer thicker than 0.6 mm has turned out to entail increased risk of material failure when the material is exposed to great temperature fluctuations. ' In any case it is unnecessary to make the bonding layer thicker than 0.6 mm, although this is not an upper limit. ! It will be understood that the bonding layer has no sharply defined minimum thickness as the latter de¬ pends on several factors, i.a. the grain sizes of the powder particles which are applied to the substrate to produce a good bonding to the ceramic material, and the quality (heat shock resistance, durability) re¬ quired in each case. Thus, in some cases it can be tolerated that, the bonding layer is spotwise pierced by for instance ZrO- particles. However, this is not preferred. Further, it will be understood that the bonding layer can merge gradually into the ceramics- containing layer, in fact this is just what is pre¬ ferred. It has been found that a uniform, gradual transition from the metal-based bonding layer to the outer ZrO- top layer provides the most reliable coatings, i.e. the ZrO- content increases substantially uniformly from the bonding layer towards the ZrO- top layer. The alloy which is used for the bonding layer is, as mentioned above, based on aluminium as the main constituent and, preferably, the alloy consists sub¬ stantially of 60-80% by weight of Al and 40-20% by weight of Si. However, the choice of alloy composition will to some extent depend on the chemical composition of the substrate. An optimalisation in this respect in a safe manner can only be made by thorough testing of the finished coating. Depending on the requirements which are made in each case, metals other than aluminium and silicon may be tolerated in minor amounts, for instance nickel and/or iron in amounts which preferably do not exceed 5% by weight, but which can be substantially higher depending on the chemical composition of the substrate. However, it is important that the bonding layer is compatible with the substrate. The bonding layer should also be as corrosion resistant as possible in the environment of use. Thus, the abovementioned preferred percentage ranges, 60-80% Al and 40-20% Si, apply when impurities are absent, or left out of account, 'in addition to iron and/or other metallic components or impurities, the Al-Si alloy used for the bonding layer can contain metal oxides in an amount up to 8% by weight. Unless special measures are taken to avoid oxide formation, such as the use of vacuum or inert gas, the bonding layer will usually contain a fe.w percent of metal oxides formed due to the high temperature environment during thermal spraying of the Al-Si alloy powder. The use of a bonding layer as herein described has been found to be the key- to achieving a heat resistant, durable ceramic coating on an Al-based alloy substrate. Apparently, such bonding layer of rapidly solidified Al-Si based alloy effectively minimises the thermal/mechanical stress and strain caused by great temperature fluctuations or thermal shock. Thus, the use of such bonding layer con¬ stitutes an essential part of the present invention. The cermet layer serves to provide a gradual transition between the metallic bonding layer and the ceramic zirconium dioxide top layer, whereby mechanical stresses during highly varying temperatures (heat shock) are reduced. However, for some application purposes the cermet layer can be omitted, as the quality of the total coating in use may. still be found satisfactory. For especially demanding applications, such as in the case of engine parts to be exposed to high temperatures, it will generally be necessary or desirable to use a cermet layer between the bonding layer and the ceramic top layer. However, it will not always be necessary to use a cermet layer of the above described preferred type, i.e. in which the cermet layer content of ceramic component is increased gradually in the direction towards the outer zirconium dioxide top layer. The in¬ vention is not limited to the use of this preferred embodiment of the cermet layer, as any other embodiments of the cermet layer, used in conjunction with the de¬ scribed bonding layer, are considered to fall within the scope of the invention. Thus, for many applications it may be satisfactory, for instance, to use a cermet layer in which the content of the ceramic component in¬ creases non-uniformly, such as incrementally or stepwise, in the direction towards the zirconium dioxide top layer. However, it should be noted that, preferably, the pro¬ tective coating provided accordinq- to the invention includes a cermet layer between the bonding layer and the zirconium dioxide top layer. The preferred cermet layer is suitably applied by thermal spraying, and a preferred embodiment of the method according to the invention resides in that the cermet layer is sprayed using two powder feeders, one for the metallic component and the other for the ceramic component, both powder types being introduced simultane¬ ously into the heat zone of the spray gun. Equipment suitable for powder spraying will be described below. The substrate (for instance an engine piston) to be coated can be cleaned in a conventional manner, and this operation preferably includes grit blasting with aluminium oxide particles, although other par- ticula-te materials can be used if desired, preferably then particles having properties similar to those of aluminium oxide particles. A preferred embodiment of the method according to the invention resides in that the substrate surface to be coated is cleaned by grit blasting with coarse grain aluminium oxide, preferably having grain sizes in the range 0.5-1.7 mm. It has been found that one will then achieve a suitably coarse substrate surface structure, and it is believed that stresses arise in the surface which because of a higher energy level in the surface serve to improve the adherence of the bonding layer (possibly a metallurgical bonding is achieved) . Said coarse structure is also ad¬ vantageous in that it permits spraying of relatively thick coatingswhen this is desired. The spraying of the final zirconium dioxide top layer has been described above. Therefore, it is here only mentioned that the desired porosity of the ceramic top layer can be controlled in a conventional manner, for instance by adjusting the distance between the spraying equipment and the surface to be coated. As men¬ tioned above, a porosity of 5-15% by volume is aimed at according to the invention. It has been found that a certain porosity in the ceramic top layer is important for top layer toughness. A high number of tests have been carried out in which coatings comprising bonding layer, cermet layer and ZrO- top layer were sprayed on engine parts to be exposed to high temperatures. Plasma spray equipment known as Eutronic Plasma (from Castolin + Eutectic, Switzerland) was used. The drawing illustrates the tem¬ perature of the surface of the workpiece in typical experiments, as the protective coating was being built up. The start of the spraying is at 0/um coating thick¬ ness in the drawing. The thicknesses of the three layers were varied. The drawing shows typical thick¬ nesses. The substrate was cleaned and roughened by grit blasting with aluminium oxide. ("Metσolite" C) , grain sizes 0.5-1.7 mm. The aluminium oxide grit was heated to 60-80 C before use so that is was free from moisture. The bonding layer was sprayed without preheating of the substrate, and the surface temperature of the latter rose to about 300°C during the spraying. During the spraying of the cermet layer the work-piece was cooled with air or a mixture of air and carbon dioxide and thereby maintained at about 300°C. The drawing illustrates that this temperature was also maintained during the spraying of the initial 150 /urn of the zir¬ conium dioxide layer, whereafter cooling with CO- gas was used and controlled such that the surface temperature of the work-piece decreased gradually to 100 C at the end of the spraying. As a rule the whole protective coating was sprayed virtually without stop between layers. Especially W hen the same metallic component is used in the cermet layer as in the bonding layer, this is readily feasible by using two adjustable separate powder feeders, for the metallic component and the ceramic component, respectively. Table 1 shows spraying parameters as generally used for the bonding layer, using the abovementioned Eutronic Plasma equipment (Model 85) . These parameters are designed for spraying a rapidly solidified Al-35 Si powder (i.e. a powder in which the Si content is 35% by weight) onto a substrate of a size similar to that of an automobile engine piston crown. Desirably, slight adjustments should be made to the spraying parameters when powders of different Si contents are to be sprayed. The spraying parameters usually should also be adjusted to the size of the substrate to be coated. It is within the reach of the art-skilled to make such adjustments. TABLE 1 Spraying parameters Nozzle diameter 6 mm Primary gas , argon 3.4 bar Secondary gas, hydrogen 4 bar Powder tube distance 4-6 mm Driving gas, argon 40 ml/min. Powder 39 g/min. Ampere 600 Volt 54 Spraying distance 115 mm Rotation velocity (perimeter) 50 m/min. Feeding (per revolution) 5 mm Number of passes 6 Thickness per pass ■025 mm Table 2 shows the yield strength, tensile strength and Vickers hardness of test specimens made by extruding well mixed Al and Si powders of various compositions. Specimens 1 to 4 were made from powders of particle sizes in the range of 40-70 Aim and speci¬ mens 5 to 12 were made from powders of particle sizes in the range 10 to 40 um. The mechanical properties of such an extruded specimen are indicative of the pro¬ perties of a coating produced by thermal spraying of the rapidly solidified Al-Si powder made from the ex¬ truded specimen. As the data obtained for specimens 1 to 11 indicated that a rapidly solidified Al-Si pow¬ der containing a little less than 40% Si might give the best results, test 12 was run using an Al-35Si alloy. ' The right hand side column of Table 2 shows the results obtained when the complete, ZrO--finished coating was tested using the initially described accelerated test comprising heating/quenching cycles, the standard re- - quirement in this test being 2000 cycles before failure. As can be seen from Table 2, the heat and thermo- shock resistance properties of the coating according to the invention were found to meet the requirements when the Si content of the rapidly solidified Al-Si powder used was above 20% by weight. A Si dontent of 40% is not considered to be an upper limit, cf. test No. 4. However, so far a supply of rapidly, solidified metal powders containing more than 40% Si has not been avail¬ able for testing. In the heating/quenching test, the judgement of the coating ' was made by microscopic examination. An amount of spalling exceeding 5% of the surface area of the coating was taken as a limit, i.e. >5% meaning failure. TABLE 2 Test Alloy Rpθ.2 ss Thermo-shock test, No. wt% m Hardne HV5/30 number of cycles. 1 Al 10 Si 143 244 70 about 200 2 Al 20 Si 186 295 95 about 2000 3 Al 30 Si 215 123 > 2000 4 Al 40 Si 153 > 2000 5 Al 15 Si 173 297 92 < 2000 6 Al 20 Si 190 306 94 about 2000 7 Al 25 Si 230 341 114 > 2000 8 Al 30 Si 229 358 125 > 2000 9 Al 25 Si 252 372 121 > 2000 10 Al 25 Si 250 382 121 > 2000 11 Al 25 Si 277 404 133 > 2000 12 Al 35 Si 235 362 128 > 2000 The substrates coated were Al alloys of the type commonly used for ' automobile engine pistons, such as silumin. Several coatings have been produced and tested using each of the Al-Si powders listed in Table 2, and the results were reasonably well reproducible. The use of a top layer of stabilized or parti¬ ally stabilized ZrO- and the production of such top layer by thermal spraying are well known per se. It is also known that zirconium silicate can be used in place of zirconium oxide, and such modification should be understood to be within the scope of the present in¬ vention. Zirconium oxide is, however, superior to the silicate for the purposes of this invention, mainly due to the higher thermal conductivity of the latter. Table 3 shows spraying parameters generally used for the ZrO- top layer. The intermediate cermet layer was sprayed using similar parameters, gradually changing (some of the ) parameters from that of Table 1 to that of Table 3, note for instance 4 bar versus 7.4 bar for the secondary gas. TABLE 3 Spraying parameters Nozzle diameter 7 mm Primary gas, argon 3.4 bar Secondary gas, hydrogen 7, 4 bar Powder tube distance 4 mm Driving gas, argon 2, 3 bar Powder 40 g/min. Ampere 700 Volt 58 Spraying distance 100 mm Rotation velocity (perimeter) 50 m/min, Feeding (per revolution) 6 mm Number of passes 30 Similar tests have been carried out to see the effect of omitting the intermediate cermet layer, and it turned out that useful coatings could be produced, enduring more than 2000 cycles in the heating/quenching test. However, comparison tests showed superior results when the preferred intermediate cermet layer was in¬ cluded in the coating. Preferred embodiments of the protective coatings according to the invention have also been tested in actual practice by being used on engine pistons and cylinder heads and have proved to endure the stresses very well. The testing has included both small and large articles (engine parts for marine diesel engines as well as for automobile engines, especially pistons and cylinder heads) , and the re¬ sults have been highly satisfactory. For instance, pistons coated with the herein described preferred protective coatings have been used in the automobile engines, and the automobiles have now been running more than 15000 km (for the Al-35Si bonding layer) with said coatings without damages to the coatings having been observed.

Claims: CLAIMS 1. An aluminium-based article having a heat and corrosion protective coating, especially engine parts such as piston crown or cylinder head, characterized in that it has a coating consisting of an aluminium-based bonding layer, preferably having a thickness in the range 0.1-0.6 mm, especially 0.3 mm, and an outer top layer of stabi¬ lized or partially stabilized zirconium dioxide, prefer¬ ably having a thickness in the range 0.5-2.5 mm, especi¬ ally 1.0-1.5 mm, and optionally a cermet layer, comprising zirconium dioxide and an aluminium-based metal component, between the bonding layer and the outer zirconium dioxide top layer. 2. An article according to claim 1, characterized in that the bonding layer is applied by thermal spraying of a rapidly solidified powder, the particle sizes therof being preferably in the range 5 μm - 60 μ , especially 10 - 40 μm. 3. An article according to claim 1 or 2, characterized in that the bonding layer substantially consists of 60-80% by weight of Al and 40-20% by weight of Si. 4. An article according to any one of the preceding claims, characterized in that the cermed layer is a layer substantially consisting of zirconium dioxide and an aluminium-based alloy, preferably an alloy of substanti¬ ally 60-80% by weight of Al and 40-20% by weight of Si, and that the metal ratio of the cermet layer decreases substantially uniformly in the direction towards the outer zirconium dioxide top layer, the zirconium dioxide ratio of the cermet layer increasing from 0 farthest in to 100% zirconium dioxide at the transition into the outer top layer, the cermet layer preferably having a thickness in the range 0.2-0.6 mm. 5. An article according to any one of the preceding claims, characterized in that the outer top layer of stabilized or partially stabilized ZrO- has a porosity in the range 5-15% by volume. 6. A method of preparing an aluminium-based article having a heat and corrosion protective coating, especially engine parts such as piston crown or cylinder head, characterized by applying to the surface to be coated an Al-based bonding layer, preferably having a thickness in the range 0.1-0.6 mm, especially about 0.3 mm, and an outer top layer of stabilized or partially stabilized zirconium dioxide, preferably having a thickness in the range 0.5-2.5 mm, especially 1.0-1.5 mm, and optionally a cermet layer, comprising zirconium dioxide and an aluminium-based metal component, between the bonding layer and the outer zirconium dioxide top layer. 7. A method according to claim 6, characterized in that the bonding layer is applied by thermal spraying of a rapidly solidified powder, preferably a powder having particle sizes in the range 5 μm - 60 μm, especially 10 - 40 μm. 8. A method according to claim 6 or 7, characterized in that an alloy substantially consisting of 60-80% by weight of Al and 40-20% by weight of Si is used as aluminiumbased alloy for the bonding layer. 9. A method according to claim 6, 7 or 8, characterized in that there is applied as cermet layer a layer substantially consisting of zirconium dioxide and an aluminiumbased alloy, preferably an alloy of substan¬ tially 60-80% by weight of Al and 40-20% by weight of Si, the cermet layer being applied having a substan¬ tially uniformly decreasing metallic proportion, considered in the direction towards the outer zirconium dioxide top layer, the zirconium dioxide proportion of the cermet layer increasing correspondingly from zero farthest in to 100% zirconium dioxide at the transition into the outer top layer, which cermet layer is preferably given a thickness in the range 0.2-0.6 mm. 10. A method according to any one of claims 6 to 9, characterized in that the cermet layer is applied by thermal spraying, the substrate being maintained at a temperature of about 300 C during spraying using gas cooling, for instance with a mixture of air and CO~, the substrate being preferably maintained at about 300°C during the spraying of the initial 100-200 μm of the ZrO- layer, whereafter the remainder of the ZrO- layer is sprayed using controlled cooling, preferably with CO- gas, such that the surface temperature of the work—piece gradually falls to about 100 C at the end of the ZrO_ spraying. 11. A method according to any one of claims 6 to 10, characterized in that the surface to be coated is cleaned by grit blasting with coarse grain aluminium oxide, preferably having grain sizes in the range 0.5-1.7 mm. 12. A method according to any one of claims 6 to 11, characterized in that the cermet layer is applied by thermal powder spraying using two powder feeders, one for the metal component and the other for the ceramic component, simultaneously feeding both of the powder types into the hot zone of the spray gun. 13. The use of an Al-Si-based alloy bonding layer on the surface of an aluminium-based alloy substrate to be given a heat resistant protective coating, said bonding layer being applied as a rapidly solidified powder the particles of which have a frozen unstable microstructure. 14. The use according to claim 13 wherein said powder is applied to the substrate by thermal spraying. 15. The use according to claim 13 or 14 wherein the bonding layer consists of 60-80% by weight of Al and 40-20% by weight of Si, apart from impurities and metal oxides. 16. The use according to claim 15 wherein the bonding layer comprises up to 8% by weight of metal oxides.

Inventors: KVERNES INGARD, KVERNES, INGARD
Applicants: KVERNES INGARD, KVERNES, INGARD
Application year: 1986
Main classification: C23C4
IPC codes: B05D1, B05D7, B32B15, C23C4, C23C28, F02F1