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Moulded AL-SI-CU aluminium alloy component with high hot-process resistance

Inactive Publication Date: 2006-06-22
ALUMINUM PECHINEY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0020] The purpose of this invention is to further improve the mechanical strength and creep resistance within the 230-380°

Problems solved by technology

These two major alloy families lead to different compromises between different usage properties: mechanical strength, ductility, resistance to creep and fatigue.

Method used

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Examples

Experimental program
Comparison scheme
Effect test

example

[0049] Ten alloys with the composition (% by weight) indicated in Table 1 were produced in a silicon carbide crucible in a 100 kg electric furnace. These compositions were measured by spark emission spectrometry, except for copper and zirconium that where measured by induced plasma emission spectrometry.

TABLE 1AlloySiFeCuMgMnZrVTi150.153.10.300.10250.153.10.300.140.250.10370.150.300.10470.150.300.120.140.150.10570.150.50.380.10670.150.50.380.140.10750.154.10.150.140.250.14870.153.00.200.140.250.14970.152.40.190.140.250.14

[0050] AFNOR permanent mold tensile test pieces were cast for each alloy. These test pieces were subjected to a heat treatment including solution heat treatment under conditions defined in Table 2, quenching in cold water, maturing at ambient temperature for 24 h and annealing for 5 h at 160° C. or 200° C.

[0051] These test pieces were used to machine tensile test pieces and creep test pieces so as to measure mechanical characteristics (resistance to failure Rm in...

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Abstract

A cast component with high hot-process mechanical strength and high creep strength in the 230-380° C. temperature range, made of aluminum alloy containing, in wt %: Mg<0.1, and preferably <0.03; Si: 4.5-10; Cu: 2.0-5.0 and preferably 3.0-4.0; Ni<0.4 and preferably <0.1; Ti: 0.05-0.25 and preferably 0.08-0.20; Zr: 0.05-0.25 and preferably 0.12-0.20; Fe: <0.9 and preferably <0.3; Zn<0.3 and preferably <0.1; optionally V: 0.02-0.30 preferably 0.04-0.20; Mn: 0.1-0.5 preferably 0.15-0.40; Hf, Nb, Ta, Cr, Mo and / or W: 0.03-0.30; other elements <0.10 each and <0.30 in total, the rest being aluminum. The alloy is used for the manufacture of internal combustion engine cylinder heads.

Description

TECHNICAL DOMAIN [0001] This invention relates to cast parts made from aluminium alloy subject to high thermal and mechanical stresses, particularly cylinder heads for internal combustion engines, and more particularly turbo-charged engines running on gasoline or diesel fuel. STATE OF THE ART [0002] Two families of aluminium alloys are usually used for the manufacture of engine cylinder heads: [0003] 1) Alloys containing from 5% to 9% of silicon, from 3% to 4% of copper and magnesium. These are usually secondary alloys, with iron contents of between 0.5% and 1%, and fairly high contents of impurities, particularly manganese, zinc, lead, tin or nickel. These alloys are usually used without heat treatment (temper F) or are simply stabilized (temper T5). They are used more particularly for the manufacture of cylinder heads for gasoline engines with fairly low thermal stresses. First melt alloys with an iron content of less than 0.3% are used for parts with greater stresses intended for...

Claims

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Application Information

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IPC IPC(8): C22C21/02
CPCC22C21/02F16J10/00C22C21/04F02F1/24
Inventor LASLAZ, GERARD
Owner ALUMINUM PECHINEY
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