AU3264500A - Die coatings for gravity and low pressure die casting - Google Patents
Die coatings for gravity and low pressure die casting Download PDFInfo
- Publication number
- AU3264500A AU3264500A AU32645/00A AU3264500A AU3264500A AU 3264500 A AU3264500 A AU 3264500A AU 32645/00 A AU32645/00 A AU 32645/00A AU 3264500 A AU3264500 A AU 3264500A AU 3264500 A AU3264500 A AU 3264500A
- Authority
- AU
- Australia
- Prior art keywords
- die
- coating
- ceramic
- powder
- die coating
- Prior art date
- 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.)
- Granted
Links
- 238000007607 die coating method Methods 0.000 title claims description 57
- 238000004512 die casting Methods 0.000 title claims description 14
- 230000005484 gravity Effects 0.000 title claims description 12
- 239000000843 powder Substances 0.000 claims description 59
- 238000000576 coating method Methods 0.000 claims description 53
- 239000011248 coating agent Substances 0.000 claims description 48
- 239000000919 ceramic Substances 0.000 claims description 33
- 229910052751 metal Inorganic materials 0.000 claims description 33
- 239000002184 metal Substances 0.000 claims description 33
- 238000000034 method Methods 0.000 claims description 30
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims description 24
- 230000008569 process Effects 0.000 claims description 20
- 239000004793 Polystyrene Substances 0.000 claims description 19
- 229920002223 polystyrene Polymers 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 16
- 239000002245 particle Substances 0.000 claims description 15
- 229920000642 polymer Polymers 0.000 claims description 15
- 239000002861 polymer material Substances 0.000 claims description 14
- 229910010293 ceramic material Inorganic materials 0.000 claims description 11
- 241000876852 Scorias Species 0.000 claims description 10
- 238000000354 decomposition reaction Methods 0.000 claims description 7
- 229920000620 organic polymer Polymers 0.000 claims description 7
- 238000007751 thermal spraying Methods 0.000 claims description 7
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- 239000011435 rock Substances 0.000 claims description 5
- 238000010285 flame spraying Methods 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 4
- 229910052500 inorganic mineral Inorganic materials 0.000 claims description 4
- 239000011707 mineral Substances 0.000 claims description 4
- 238000007750 plasma spraying Methods 0.000 claims description 4
- -1 oxides Chemical class 0.000 claims description 3
- 238000005507 spraying Methods 0.000 claims description 3
- 229910052582 BN Inorganic materials 0.000 claims description 2
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 2
- 239000004952 Polyamide Substances 0.000 claims description 2
- 239000004962 Polyamide-imide Substances 0.000 claims description 2
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 2
- 239000002734 clay mineral Substances 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 claims description 2
- 238000010891 electric arc Methods 0.000 claims description 2
- YDZQQRWRVYGNER-UHFFFAOYSA-N iron;titanium;trihydrate Chemical compound O.O.O.[Ti].[Fe] YDZQQRWRVYGNER-UHFFFAOYSA-N 0.000 claims description 2
- 150000001247 metal acetylides Chemical class 0.000 claims description 2
- 150000002736 metal compounds Chemical class 0.000 claims description 2
- 150000004767 nitrides Chemical class 0.000 claims description 2
- 229920002647 polyamide Polymers 0.000 claims description 2
- 229920002312 polyamide-imide Polymers 0.000 claims description 2
- 229920000728 polyester Polymers 0.000 claims description 2
- 229920000193 polymethacrylate Polymers 0.000 claims description 2
- 239000004810 polytetrafluoroethylene Substances 0.000 claims description 2
- 229920001343 polytetrafluoroethylene Polymers 0.000 claims description 2
- SCUZVMOVTVSBLE-UHFFFAOYSA-N prop-2-enenitrile;styrene Chemical compound C=CC#N.C=CC1=CC=CC=C1 SCUZVMOVTVSBLE-UHFFFAOYSA-N 0.000 claims description 2
- 239000008262 pumice Substances 0.000 claims description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 2
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 2
- 239000000377 silicon dioxide Substances 0.000 claims description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 2
- 238000001228 spectrum Methods 0.000 claims description 2
- 229920000638 styrene acrylonitrile Polymers 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 2
- 229910052845 zircon Inorganic materials 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 2
- 150000001875 compounds Chemical class 0.000 claims 1
- 239000012815 thermoplastic material Substances 0.000 claims 1
- 238000000151 deposition Methods 0.000 description 11
- 239000000203 mixture Substances 0.000 description 10
- 230000003746 surface roughness Effects 0.000 description 9
- 230000004888 barrier function Effects 0.000 description 7
- 239000007789 gas Substances 0.000 description 7
- 238000007711 solidification Methods 0.000 description 7
- 230000008023 solidification Effects 0.000 description 7
- 239000007921 spray Substances 0.000 description 7
- 239000011230 binding agent Substances 0.000 description 6
- 239000004033 plastic Substances 0.000 description 6
- 229920003023 plastic Polymers 0.000 description 6
- 229910002076 stabilized zirconia Inorganic materials 0.000 description 6
- 239000004115 Sodium Silicate Substances 0.000 description 5
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 5
- 229910052911 sodium silicate Inorganic materials 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000011049 filling Methods 0.000 description 4
- 239000000395 magnesium oxide Substances 0.000 description 4
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 4
- 238000005299 abrasion Methods 0.000 description 3
- 238000007792 addition Methods 0.000 description 3
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 3
- 238000009413 insulation Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000011368 organic material Substances 0.000 description 3
- 239000000725 suspension Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000005253 cladding Methods 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 238000005979 thermal decomposition reaction Methods 0.000 description 2
- 229920001169 thermoplastic Polymers 0.000 description 2
- 239000004416 thermosoftening plastic Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 241000446313 Lamella Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 239000012766 organic filler Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000035484 reaction time Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000007873 sieving Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000012720 thermal barrier coating Substances 0.000 description 1
- 238000002207 thermal evaporation Methods 0.000 description 1
Landscapes
- Coating By Spraying Or Casting (AREA)
Description
WO 00/56481 PCT/AU00/00239 1 DIE COATINGS FOR GRAVITY AND LOW PRESSURE DIE CASTING Technical Field This invention relates to die coatings, to a process for providing 5 permanent mould or die components with an improved die coating, and to a die coating material for use in such process. Background In low pressure and gravity die casting, the surface of each metal mould 10 or die component, which is contacted by molten metal, is provided with a mould or die coating. Under current procedures, a ceramic-based coating is used at a thickness of from about 0.05 to 1.0mm. The main function of the coating is to provide a degree of insulation which is intended to prevent premature solidification of the molten metal, and thereby enable the complete filling of the 15 die cavity before solidification starts. However, the coating also is to protect the steel die surfaces from erosion or corrosion by impingement by or contact with molten metal. Current die coating technology involves the use of a water-based suspension of ceramic particles containing a water-based binder, most 20 commonly sodium silicate. Coating mixtures of this type need to be properly stored, while stirring and testing to prepare them for use often involves tedious procedures. The coating is applied to the sand or shot blasted surface of a die component using a pressurized air spray gun. For this, the component is preheated, typically from about 150 to 220 0 C, such that water is evaporated 25 from the die surface, enabling the binder to polymerize and bond the ceramic particles together and to the die surface. The die coatings produced with the current aqueous ceramic suspensions are highly porous. The level of porosity may range from about 30 to 60%, depending on the size and shape of the ceramic particles and the 30 amount of binder used. High porosity gives the coating very good insulating properties. However, the strength of the coatings is limited by the strength of the binder used (about 6.9 MPa in the case of sodium silicate) and the level of porosity of the coating.
WO 00/56481 PCT/AU00/00239 2 Important factors in a thermally insulating die coating are porosity and surface roughness. Also, wear resistance is important since a coating with an inadequate level of wear resistance is prone to damage in use, with a consequential reduction in its useful life-time. The sodium silicate bonded 5 coatings, produced with the current aqueous ceramic suspensions, have a low level of wear resistance which results in them having a productive life-time of not more than about two to four 8-hour shifts. However, even during such a short life-time, production needs to be stopped from time to time to enable repair of the coating by a "touch-up" operation. 10 In US patent 4,269,903 to Clingman et al, there is disclosed a ceramic seal coating formed on at least one of two relatively rotatable members, such as rotating air foils of an axial flow compressor. The process seeks to provide a seal coating as disclosed in US patent 4,055,705 to Stecura et al, which has improved abradability. The coating of US 4,055,705 comprises a bond coat of 15 NiCrAIY alloy applied to a substrate and a thermal barrier which is applied over the bond layer and comprises zirconia stabilized with another oxide. The advance provided by US 4,269,903 is in providing over that thermal barrier layer an abradable layer of porous stabilized zirconia. The porous layer is formed by thermal decomposition of organic filler material, which is co-deposited with 20 stabilized zirconia onto the barrier layer. The co-deposition, such as by plasma spray or thermal spray process, preferably uses separate streams of organic and zirconia powders, with the organic powder chosen from a range of suitable thermoplastics. After co-deposition, the organic material is decomposed by heating, to leave an abradable zirconia layer having a porosity of from about 20 25 to about 33% and, hence, a suitable level of abradability. The abradable layer enables wear of at least one of two relatively rotatable components in rubbing contact such that loss of a fluid seal between the components is avoided. In the process of US 4,269,903 the organic material is used because, after its co-deposition with zirconia, the organic material is able to be removed 30 by thermal decomposition to leave a porous, and hence abradable, layer of zirconia. An alternative purpose for co-deposition of organic powders with ceramic and/or metal powders is disclosed in US patent 5,718,970 to Longo. The process of US 5,718,970 is concerned with providing a substrate with a thermally sprayed duplex coating of a plastics material which is co- WO 00/56481 PCT/AU00/00239 3 deposited with a higher melting point ceramic material and/or metal. It is asserted that while metal and ceramic powders necessitate spraying with high temperature gas streams, such as plasma sprays or acetylene gas, plastic powders are usually sprayed with low temperature gas streams, such as 5 hydrogen or natural gas, to prevent superheating and oxidation of the plastic powder. The solution for achieving a duplex coating is to use a powder comprising particles having a core of plastic material and, on the core, a substantially continuous particulate cladding of ceramic and/or metal. The cladding may be adhered to the core as a consequence of heating to soften the 10 core, or by use of a suitable binder. The duplex coating produced by thermal spraying of such powders is able to exhibit characteristics of the ceramic and/or metal and of the polymer material, with the coating indicated as having particles of the plastic material dispersed in a continuous matrix of the ceramic and/or metal. 15 Disclosure of the Invention The present invention seeks to provide an improved die coating, a process for providing a permanent mould or die component with a an improved die coating and a die coating material for use in the process of the invention. 20 An improved die coating according to the present invention, for use on the surface of a mould or die component contacted by molten metal in low pressure or gravity die casting, includes a porous layer of ceramic material produced by co-deposition, using a thermal spraying procedure, of a powder of the material and a powder of a suitable organic polymer material and, after the 25 co-deposition, heating of the polymer material to cause its removal. The invention also provides a process for providing a die coating on such surface of a metal mould or die component, wherein an initial coating of organic polymer material and ceramic material is formed on the surface by co deposition of powders of the materials by a thermal spraying procedure, and the 30 initial coating is heated so as to remove the polymer material and leave a porous coating of the ceramic material. The polymer material may be heated so as to remove the polymer material by combustion and/or by decomposition, with decomposition generally being preferred.
WO 00/56481 PCT/AU00/00239 4 The thermal spraying procedure used in the present invention may be of any suitable type. Thus the co-deposition may be by flame spraying, plasma spraying or electric arc spraying. The die coating of the present invention and the process for its 5 production have some features which seemingly are similar to features of the disclosure of US patent 4,269,903 in relation to a porous abradable layer. However, as indicated above, the disclosure of 4,269,903 is concerned with an abradable ceramic seal coating on at least one of a pair of members, which move relative to each other in rubbing contact. That is, the disclosure is quite 10 unrelated to the context of a die coating for surfaces of metal mould or die components contacted by molten metal. Moreover, the disclosure of US patent 4,269,903 is limited to a porous layer of stabilized zirconia, which is abradable. In contrast, the die coating of the invention in addition to not being limited to the use of zirconia, has an enhanced level of wear resistance which enables a 15 substantially increased useful life-time relative to current die coating technology discussed above. There is little basis for correlating abradable in the context of US 4,269,903 with wear resistance in the context of a die coating. However, particularly as a die coating is required to have a high level of abrasion resistance in order to be able to withstand the impingement and flow of molten 20 metal at the high temperature levels prevailing in low pressure and gravity die casting, the benefits resulting from the die coating of the invention are surprising in view of the disclosure of US patent 4,269,903 which teaches an abradable, rather than an abrasion resistant, coating. The ceramic powders which are used in providing the die coating of the 25 present invention may be a processed powder conventionally used in the production of ceramic articles. Thus, the powder may be selected from at least one metal compound such as oxides, nitrides, carbides and borides. Suitable examples include alumina, titania, silica, stabilized zirconia, silicon nitride, boron nitride, silicon carbide, tungsten carbide, titanium borides and zirconium boride. 30 However, the ceramic powder may be of a suitable mineral origin such as clay minerals, hard rock ore and heavy mineral sands such as those of ilmenite, rutile and/or zircon. One particularly suitable powder is that obtained from scoria or pumice, since powder particles of these materials are internally porous and have the added benefit of being of angular form.
WO 00/56481 PCT/AU00/00239 5 A wide range of plastics and like materials can be used to provide the organic polymer powder. Important requirements for selection of these are availability in a suitable powder form and an ability to withstand sufficiently the temperatures to which they are exposed during thermal deposition. A further 5 requirement is an ability to be combusted or decomposed at practical temperatures and in practical reaction times. In large part, the materials comprise thermoplastics, such as polystyrene, styrene-acrylonitrile, polymethacrylates, polyesters, polyamides, polyamide-imides and PTFE. The respective powders, that is the ceramic powder and the polymer 10 powder, preferably are of a relatively narrow size spectrum. In general, they preferably are of particle sizes not more than about 60 pm and not less than about 1 p~m in the case of the ceramic and not less than about 5 pm in the case of the polymer material. The process of the invention can be used in a variety of forms. In one 15 form, a substantially uniform die coat is provided over all surfaces of mould or die components, which define a die cavity. The coating may, for example, have a thickness of from about 250 to 400 pm, such as from about 300 to about 400 pm. In that form, the coating provides insulation over all surfaces of the die cavity, enabling filling of the cavity before molten metal being cast commences 20 solidification. The die coating provided by the invention, because of its porosity, acts as a thermal barrier. In contrast, a non-porous coating of the same material will be less effective as a thermal barrier. This enables alternative useful forms of the invention in which use is made of a die coating according to the invention in 25 combination with a non-porous coating. In one alternative, one surface or part of the overall surface defining a die cavity is provided with a non-porous ceramic die coating which is less insulating, while other surfaces or parts of the surface are provided with a thermal barrier die coating according to the invention. This arrangement enables heat energy extraction, from molten metal 30 in the die cavity, to be at a higher rate through the non-porous coating than through the porous thermal barrier die coating. Thus, directional solidification is able to be facilitated, to achieve solidification of the molten metal in a direction away from the non-porous coating.
WO 00/56481 PCT/AU00/00239 6 In a further alternative, all surfaces defining a die cavity, or one or a part of such a surface, can be provided with successive die coatings which alternately are porous and non-porous. That is, the full thickness of at least part of the die coating may consist of at least two layers of a sandwich or lamella 5 form. As a consequence, the die coating will have a thermal conductivity intermediate that of corresponding coating thickness of non-porous and porous die coatings, respectively, of the same ceramic material. Thus, the range of differential control over heat energy extraction from molten metal being cast can be enhanced. 10 In each of those alternatives of the invention, the porous and non-porous regions or layers of the die coating may be of the same ceramic material or of a respective ceramic material. In order that the invention may more readily be understood, the description now is directed to the following Examples. 15 WO 00/56481 PCT/AU00/00239 7 Example 1 Ceramic powder and polymer powder were mixed and subjected to flame spraying to form a co-deposited coating on a die cavity defining the surface of a low pressure metal die cast component. The ceramic powder was Metco 210 5 grade zirconia stabilized by 24% magnesium oxide for which the data sheet indicated a particle size range of (-53) to (+10) tm, a melting point 21400C and a density of 4.2gcm 3 . The polymer powder was of polystyrene supplied by Huntsman Chemical Company Australia Pty. Ltd., which had been ground to 45pm under liquid nitrogen, using a SPEX Freezer mill. The powder mixture of 10 MgO(24%)ZrO 2 /polystyrene contained 15 volume percent (4wt%) of polystyrene. The co-deposition of the powder mixture was performed using a Metco Type 6P-ll Thermospray system, with a P7C-K nozzle and a 3 MPa powder feeder, under the following conditions: 15 Pressure: oxygen 2.07x 10-'MPa; acetylene 1.035x10 -1 MPa; Flow: oxygen 20 1/min; acetylene 24 1/min m 3
S
1 Carrier Gas: N 2 at 3.78 x10 -1 MPa and 18 1/min Powder Feeder: 15 (rpm) Spray Distance: 76 mm 20 Also, the system used an air jet, which operated at a pressure of 3.45x10 1 MPa and crossed at 63.5 mm from the nozzle. Following co-deposition of the blended powders, the deposited coating was heated to 450 0 C for one hour to cause the polystyrene to decompose. 25 Polystyrene decomposes fully at 320 to 3500C in nitrogen (DTA/TGA). The porous, stabilized zirconia coating resulting from removal of the polystyrene by decomposition was found to comprise an excellent die coating in having good abrasion resistance enabling it to withstand the impingement of molten metal during low pressure and gravity die casting. The die coating also exhibited a 30 low heat transfer coefficient, such that solidification of molten metal during such casting was able to be delayed until filling of the die cavity was complete.
WO 00/56481 PCT/AU00/00239 8 Example 2 The overall procedure of Example 1 was repeated, with scoria powder used instead of stabilized zirconia. The scoria powder was produced by drying scoria rocks in an oven at 100 0 C, crushing the dried rocks using a ring mill, and 5 sieving the crushed rock using a shaker and several screens of decreasing size to separate the powder. The scoria powder used had a size range of 45 to 75 pm and a density of 2.9gcm -3 . It was blended with polystyrene powder, as produced and characterized in Example 1, to achieve a blend having 15 volume percent of polystyrene. 10 The conditions of flame spraying and decomposition of the co-deposited polystyrene were as detailed in Example 1. The resultant porous, scoria die coating was of similar characteristics to the zirconia coating produced in Example 1, but was more effective as a thermal barrier coating due to it having a lower heat transfer co-efficient than zirconia. 15 Example 3 Three powder blends with 15 vol% polystyrene were produced in the manner detailed in Example 1. Each of these differed from Example 1 in that the size range of the polystyrene powder blended with the MgO (24%) stabilized 20 ZrO 2 was 45 to 75 pm, 75 to 106 pm and 106 to 150 pm, respectively. In contrast to Example 1, each of the three powder blends was co deposited by plasma-spraying, using a spray gun designated as a SG100 subsonic having a power rating of 40 kw, an anode setting of 185 volts, a cathode setting of 129 volts and a gas injector, Miller 113. Operating 25 parameters used were: Power: open circuit 160V, operating power at 33V and 800A Arc/Primary gas: argon, critical orifice No. 56 (flow rate 47 30 1/min), pressure reg. 3.45 x10 -1 ' MPa Auxiliary/Secondary gas: helium, critical orifice No. 80 (flow rate 12 I/min), pressure reg. 3.45 x 101 MPa WO 00/56481 PCT/AU00/00239 9 Powder gas/carrier: argon, critical orifice No. 77 (6 1/min), pressure reg. 2.76 x 101 MPa, hopper 2.8 rpm Spray distance: 96 mm 5 Following co-deposition of each of the three powder blends, the deposited coating was heated as detailed in Example 1. The porous, stabilised zirconia coatings resulting from the removal of polystyrene by decomposition were of similar characteristics to the coating produced in Example 1. 10 Example 4 The overall procedure of Example 3 was repeated, using a blend of scoria powder produced as in Example 2 and -45 pm polystyrene powder 15 produced as in Example 1. The condition of plasma spraying of the scoria/15 vol% polystyrene powder blend, and decomposition of co-deposited polystyrene, was the same as in Example 3. The resultant porous scoria die coating was of similar characteristics to that produced in Example 2. The process of die coating using the current technology is considered as 20 an art in which the control of coating quality and thickness are highly operator dependent. The bond between ceramic particles provided by polymerized sodium silicate is not very strong. Therefore, sodium silicate bonded coatings are fragile and not wear resistant. On the other hand, in the new die coating system of the present 25 invention, there is no separate binder. The ceramic particles are partially melted and then bonded together which provides stronger bonding system. Changing the percentage of the porosity of the coating can alter the heat transfer coefficient properties of the die coating of the present invention. This can be easily achieved by changing the percentage of the polymer used in producing 30 the die coating. This gives the advantage to tailor directional solidification for the die casting part to minimize the occurrence of shrinkage related defects. Use of the present invention is very flexible. Changing the polymer size can change the surface roughness of the coating. For the purpose of good adhesion a first layer of the coating can be applied without addition of polymer.
WO 00/56481 PCT/AU00/00239 10 A second layer can contain polymer particles to provide porosity to improve insulating properties of the coating. A final layer can be also without polymer if very smooth surface is required. Low pressure and gravity die casting processes require that the molten 5 metal flow readily in the complicated die cavity in order to create the die casting. Low pressure die casting in particular involves the movement of molten metal against gravity in order to fill the die cavity completely. Often the molten metal is transported through narrow sections and the insulation provided by the die coating is found to be critical in these areas. The surface roughness of the 10 coating affects the ability of the molten metal to flow into the die cavity by creating minute pockets of air between the peaks of the coating and where it contacts the molten metal. The molten metal does not completely wet the total surface area of the coating, and these pockets of air are an important factor influencing fluidity and therefore the filling of the die cavity in order to produce 15 sound castings. The addition of evaporable components, specifically polymer powders creates a high degree of porosity as well as affecting the surface profile of the resultant coating. This surface roughness can be changed by changing the size of the polymer particles added to the ceramic powder mix for plasma sprayed 20 coatings. The flexibility of changing the surface roughness also has applications in influencing the surface finish of the final casting. The variation in surface roughness with polymer particle size can be illustrated with reference to Example 3. A die coating produced with the MgO(24%) stabilized ZrO 2 of that Example, without added polymer, was found 25 to have a surface roughness of Ra of 4.5pm. The die coating produced using the zirconia and 15 vol% of 45 to 75 pm polystyrene had a surface roughness Ra of 10 pm, while that produced with 15 vol% of 75 to 106pm polystyrene had a surface roughness of 25pm.
WO 00/56481 PCT/AU00/00239 11 Finally, it is to be understood that various alterations, modifications and/or additions may be introduced into the constructions and arrangements of parts previously described without departing from the spirit or ambit of the invention. 5
Claims (17)
1. A die coating for use on the surface of a mould or die component contacted by molten metal in low pressure or gravity die casting, said die coating including a porous 5 layer of ceramic material produced by co-deposition, using a thermal spraying procedure, of a powder of said ceramic material and a powder of a suitable organic polymer material and, after the co-deposition, heating of said polymer material to cause its removal. 10
2. A die coating according to claim 1, said ceramic powder being selected from at least one metal compound such as oxides, nitrides, carbides and borides, preferably from the group comprising alumina, titania, silica, stabilised zirconia, silicon nitride, boron nitride, silicon carbide, tungsten carbide, titanium borides and zirconium boride. 15
3. A die coating according to claim 1, said ceramic powder being selected from at least one mineral compound such as clay minerals, hard rock ore and heavy mineral sands such as those of ilmenite, rutile and/or zircon.
4. A die coating according to claim 3, said ceramics powder being obtained from 20 scoria or pumice.
5. A die coating according to any preceding claim, said organic polymer powder being formed from a thermoplastic material, such as polystyrene, styrene-acrylonitrile, polymethacrylates, polyesters, polyamides, polyamide-imides and PTFE. 25
6. A die coating according to any preceding claim, each of said ceramic and polymer powders being of relatively narrow size spectrum.
7. A die coating according to claim 6, said ceramic and polymer particles being of 30 particle sizes not more than about 60 pm and not less than about 1 pm in the case of said ceramic powder and not less than about 5 [tm in the case of the polymer powder.
8. A process for providing a die coating on the surface of a mould or die component, wherein an initial coating of organic polymer material and ceramic 35 material is formed on the surface by co-deposition of powders of the materials by a thermal spraying procedure, and the initial coating is heated so as to WO 00/56481 PCT/AU00/00239 13 remove the polymer material and leave a porous coating of the ceramic material.
9. A process according to claim 8, said polymer material being heated for 5 removal by combustion and/or decomposition.
10. A process according to claim 8 or 9, said thermal spraying procedure being either flame spraying, plasma spraying or electric arc spraying. 10
11. A process according to any one of claims 8 to 10, wherein a substantially uniform die coat is provided over all surfaces of the mould or die components, which define a die cavity.
12. A process according to claim 11, said coating having a thickness of 15 from about 250 to 400 pm.
13. A process according to claim 12, said coating having a thickness of from about 300 to about 400 pm. 20
14. A mould or die component having a surface for contact by molten metal in low pressure or gravity die casting, said surface being coated fully, or in a section or sections thereof, by a die coating according to any one of claims 1 to 7. 25
15. A mould or die component having a surface for contact by molten metal in low pressure or gravity die casting, said surface being coated in a section or sections thereof with a non-porous ceramic die coating and in another section or sections thereof, with a die coating according to any one of claims 1 to 7. 30
16. A metal mould or die component having a surface for contact by molten metal in low pressure or gravity die casting, said surface being coated fully, or in a section or sections thereof, by alternating layers of a non-porous ceramic die coating and a die coating according to any one of claims 1 to 7. WO 00/56481 PCT/AU00/00239 14
17. A die coating material for use in the process of any one of claims 8 to 13, said material being formed from a powder of a ceramic material and a powder of an organic polymer material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU32645/00A AU770448B2 (en) | 1999-03-23 | 2000-03-23 | Die coatings for gravity and low pressure die casting |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AUPP9390A AUPP939099A0 (en) | 1999-03-23 | 1999-03-23 | Die coatings for gravity and low pressure diecasting |
| AUPP9390 | 1999-03-23 | ||
| PCT/AU2000/000239 WO2000056481A1 (en) | 1999-03-23 | 2000-03-23 | Die coatings for gravity and low pressure die casting |
| AU32645/00A AU770448B2 (en) | 1999-03-23 | 2000-03-23 | Die coatings for gravity and low pressure die casting |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU3264500A true AU3264500A (en) | 2000-10-09 |
| AU770448B2 AU770448B2 (en) | 2004-02-19 |
Family
ID=25622194
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU32645/00A Ceased AU770448B2 (en) | 1999-03-23 | 2000-03-23 | Die coatings for gravity and low pressure die casting |
Country Status (1)
| Country | Link |
|---|---|
| AU (1) | AU770448B2 (en) |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5277831A (en) * | 1991-03-06 | 1994-01-11 | Hanano Commercial Co., Ltd. | Method for low pressure die casting with low pressure die casting powdery mold releasing agent |
-
2000
- 2000-03-23 AU AU32645/00A patent/AU770448B2/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| AU770448B2 (en) | 2004-02-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1171253B1 (en) | Die coatings for gravity and low pressure die casting | |
| CA2039240C (en) | Composite thermal spray powder of metal and non-metal | |
| US3607343A (en) | Flame spray powders and process with alumina having titanium dioxide bonded to the surface thereof | |
| Herman et al. | Thermal spray: current status and future trends | |
| CN101914767B (en) | Preparation process and device of nano-particle reinforced bimetal composite | |
| Wirojanupatump et al. | The influence of HVOF powder feedstock characteristics on the abrasive wear behaviour of CrxCy–NiCr coatings | |
| JP6768513B2 (en) | Heat shield coating and coating method | |
| CA2576319C (en) | Partially-alloyed zirconia powder | |
| US20080113105A1 (en) | Coating Formed By Thermal Spraying And Methods For The Formation Thereof | |
| WO1995023877A1 (en) | Thermal spray nozzle for producing rough thermal spray coatings, method for producing rough thermal spray coatings, and thermal spray coatings produced therewith | |
| JP2988281B2 (en) | Ceramic / metal composite powder for thermal spraying and method for forming thermal spray coating | |
| US5014768A (en) | Chill plate having high heat conductivity and wear resistance | |
| JP2003531298A (en) | Improved thermal spray powder | |
| AU770448B2 (en) | Die coatings for gravity and low pressure die casting | |
| Alonso et al. | Erosion protection of carbon—epoxy composites by plasma-sprayed coatings | |
| MXPA05000176A (en) | Coatings for articles used with molten metal. | |
| US20090258214A1 (en) | Vapor-deposited coating and thermally stressable component having such a coating, and also a process and apparatus for producing such a coating | |
| KR100743188B1 (en) | Manufacturing method of high hardness BCC coating of nanostructures | |
| CN111996481B (en) | Preparation method of YSZ/Cu metal ceramic composite coating | |
| Wang et al. | Mullite coatings produced by APS and SPS: effect of powder morphology and spray processing on the microstructure, crystallinity and mechanical properties | |
| CA2122063A1 (en) | Method of producing temperature-resistant plastic films on diaphragm-gland surfaces | |
| Fussell et al. | Steel-Based Sprayed Metal Tooling | |
| WO2004002655A1 (en) | Sealer coating for use on porous layers | |
| Xie | Thermal Spray Methods and Splat Formation | |
| Pandit et al. | Plasma Sprayed Ceramic Coatings on Metallic Substrates |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| DA3 | Amendments made section 104 |
Free format text: THE NATURE OF THE AMENDMENT IS: AMEND THE INVENTORS TO ADD: STEFAN GULIZIA |
|
| FGA | Letters patent sealed or granted (standard patent) |