초록 ▼

The invention relates to cylinder liners for internal combustion engines comprising a matrix based on aluminum alloys of high mechanical strength, obtained by powder metallurgy, and methods of producing them. The liners comprise a dispersion of grains of an added intermetallic compound, apart from t

The invention relates to cylinder liners for internal combustion engines comprising a matrix based on aluminum alloys of high mechanical strength, obtained by powder metallurgy, and methods of producing them. The liners comprise a dispersion of grains of an added intermetallic compound, apart from the dispersion of such intermetallic compounds as may exist in the alloy, the added compound having a melting temperature of over 700° C. The liners are obtained by extruding or sintering a mixture of powders. The liners of the invention may be used particularly in the automobile industry and in any kind of industry where liner-piston units of good compatibility must be obtained from aluminum alloys.

대표청구항 ▼

1. Engine cylinder liners comprising: (1) a matrix comprising an aluminum alloy produced by powder metallurgy, said alloy being selected from the group consisting of A--S 12 UG alloys and series 7,000 alloys containing from 1 to 12% by weight added silicon, and (2) a dispersion of grains distrib

1. Engine cylinder liners comprising: (1) a matrix comprising an aluminum alloy produced by powder metallurgy, said alloy being selected from the group consisting of A--S 12 UG alloys and series 7,000 alloys containing from 1 to 12% by weight added silicon, and (2) a dispersion of grains distributed within said matrix comprising at least one added intermetallic compound having a melting point of more than 700° C., said grains being distinct and not forming part of the actual alloy structure. 2. The liners of claim 1, wherein the intermetallic compound is Ni 3 Sn. 3. The liners of claim 1, wherein the intermetallic compound is in the form of calibrated grains of dimensions from 5 to 50 μm. 4. The liners of claim 1, wherein the grains of intermetallic compound comprise 5 to 15% of the weight of the liner. 5. The liners of claim 1, wherein the grains of intermetallic compound comprise particles resulting from grinding. 6. The liners of claim 1, wherein the grains of intermetallic compound comprise particles resulting from solidification of an atomized liquid. 7. The liners of claim 1, additionally comprising graphite. 8. The liners of claim 7, wherein the amount of graphite in the liner is from 3 to 10% by weight. 9. In a method of producing engine cylinder liners, comprising: (1) converting an aluminum alloy from the liquid state to a powder of particle dimensions from 60 to 400 μm; (2) shaping said powder by cold compression; and (3) sintering said shaped powder in a controlled atmosphere, the improvement comprising mixing the powder prior to shaping with grains of an intermetallic compound having a grain size of 5 to 50 μm and a melting point of more than 700° C., the grains being added in such quantity that they comprise 5 to 15% by weight of the liners. 10. In a method of producing engine cylinder liners, comprising: (1) converting an aluminum alloy from the liquid state to a powder of particle dimensions from 60 to 400 μm; (2) shaping by extruding said powder in a press selected from the group consisting of floating needle presses and bridge machinery presses, and; (3) trimming the extruded product obtained and cutting up said extruded product to the desired length, the improvement comprising mixing the powder prior to shaping with grains of an intermetallic compound having a grain size of 5 to 50 μm and a melting point of more than 700° C., the grains being added in such quantity that they comprise 5 to 15% by weight of the liners. 11. The method of claim 10, wherein the extruded product is quenched on leaving the press, then subjected to a heat treatment, prior to being trimmed and cut up. 12. The method of claim 10, wherein the powder is initially compressed in the form of blanks, then subjected to backward extrusion to form a cup, the bottom and opposed edge of which are cut up to produce a liner which is subsequently machined. 13. The method of claim 12, wherein direct quenching of the cup is carried out after extrusion, prior to being cut up. 14. The method of claim 9, wherein 3 to 10% by weight of graphite powder is added to the mixture.