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Conventional Processing |
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3. Heat the compact , usually in a protective atmosphere, at a temperature below the melting point of the main constituent so that the powder particles weld together and confer sufficient strength to the object for the intended use. This process is called sintering hence the term sintered parts. In certain cases a minor constituent becomes molten at the sintering temperature in which case the process is referred to as liquid phase sintering. The amount of liquid phase must be limited so that the part retains its shape. In certain special cases stages 2 and 3 are combined i.e. compaction is done at an elevated temperature such that sintering occurs during the process. This is termed hot pressing, or pressure sintering. In many cases the sintered part is subjected to additional processing - repressing, plating etc. and these will be dealt with in the appropriate sections below. In certain special cases, e.g. in the manufacture of filter elements from spherical bronze powder, no pressure is used, the powder being placed in a suitably shaped mould in which it is sintered. This process is known as loose powder sintering.
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Sintering is the means whereby the powder particles are welded together and a strong finished part produced
Even with the best control that is feasible in practice, there will inevitably be some variation in the dimensions of parts produced from a given material in a given die set. Typically, it is possible for parts 'as-sintered' to be accurate to a tolerance of -0.0508mm per mm, in the direction at right angles to the pressing -direction, and 0.1016mm per mm parallel to the pressing direction. Dimensional accuracy can be greatly improved by re-pressing the part after sintering. This operation is called sizing. Sizing may be done in the die that was used for compacting the powder in those cases where the dimensional change on sintering is controlled at or very near to zero, but commonly separate sizing tools are used. Re-pressing is used also to imprint or emboss the face(s) of the component in contact with the punch(es), in which case the process is referred to, for obvious reasons, as coining. During re-pressing the density of the part is generally increased, especially if the as-sintered density is low.
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An alternative method of improving the strength of inherently porous sintered parts is to fill the surface connected pores with a liquid metal having a lower melting point. Pressure is not required:
The process is used quite extensively with ferrous parts using copper as infiltrant but to avoid erosion, an alloy of copper containing iron and manganese, is often used. Clearly if the molten copper is already saturated with iron its ability to erode the surface is lost. Other proprietary infiltrant compositions are also on the market. However, as we saw in the section on dimensional change during sintering, the diffusion of copper into iron can lead to growth. Infiltration is also used to make composite electrical contact material such as tungsten/copper and molybdenum/silver; the lower melting point metal being melted in contact with an already sintered skeleton of W or Mo. |
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Although many, perhaps the bulk of sintered structural parts are used in the as-sintered or sintered and sized condition, large quantities of iron-based parts, correctly steels, are supplied in the hardened and tempered conditions. Conventional hardening processes are used, but because of the porosity inherent in sintered parts, they should not be immersed in corrosive liquids - salt baths, water, or brine - since it is difficult to remove such materials from the pores . Heating should be in a gas atmosphere followed by oil-quenching. These restrictions may not apply to very high density parts 7.2 g/cc nor to parts that have been infiltrated.
Carburizing and carbonitriding of PM parts is extensively used, and again gaseous media are indicated. Because of the porosity of the 'case' is generally deeper and less sharply defined than with fully dense steels, but this is generally an advantage rather than the revers.
A process peculiar to PM parts is steam-treatment which involves exposing the part at a temperature around 500°C to high pressure steam. This leads to the formation of a layer of magnetite (iron oxide) on all accessible surfaces and a number of desirable property changes result.
The treatment is not generally applicable to hardened and tempered parts because the exposure to the high temperature would undo the hardening. |
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A large percentage of hardmetal cutting tool inserts are now coated using chemical vapour deposition (CVD) or physical vapour deposition (PVD). The lower temperature PVD process also allows steels to be given a wear resistant layer of TiC, TiN, Al2O3 or a combination of these materials and sintered high speed steel tools are also now being coated.
Although a major attraction of PM parts is that they can be produced accurately to the required dimensions, there are limitations to the geometry that can be pressed in rigid dies, and subsequent machining, for example of transverse holes or re-entrants at an angle to the pressing direction is not uncommon. The existence of porosity alters the machining characteristics and in general tool wear is greater than with the same composition in the fully dense form. Carbide tools are recommended, and lower cutting speeds may be necessary. The machinability can be improved by incorporating certain additions in the powder mix - e.g. lead, copper, graphite, sulphur or a metal sulphide such as manganese sulphide, and, as already indicated, by infiltration or resin impregnation. If these points are borne in mind all the traditional machining processes - turning, milling, drilling, tapping, grinding, etc. - can be done quite readily. |
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Another class of wrought sintered material that is beginning to make an impact is based on particulate material - powder or chopped ribbon - that has been solidified and cooled at a very high rate such that metastable non-equilibrium microstructures result. They may be microcrystalline or amorphous. The process is applicable only to certain alloys, and one important feature is that the matrix metal can retain in solid solution a much higher than the equilibrium percentage of the alloying element. Providing that the densification and mechanical working is carried out at a temperature low enough to avoid destroying the non-equilibrium structure, remarkably enhanced mechanical properties can be achieved. A major development programme is underway with alloys of aluminium, titanium, and magnesium, the hope being that their use in aircraft structures will significantly reduce the weight and increase the payload. |
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