The effect of pressure on the Mg alloy-Alumina composite properties fabricated by infiltration casting

Subject Areas :

Bahman Eghtedari ¹ , Mahmoud Meratian ² , Ali Maleki ³ , Mohamad Khodaei ⁴

1 - کارشناسی ارشد، دانشکده مهندسی مواد، دانشگاه صنعتی اصفهان
2 - دانشیار، دانشکده مهندسی مواد، دانشگاه صنعتی اصفهان
3 - استادیار، پژوهشکده فولاد، دانشگاه صنعتی اصفهان
4 - استادیار، مرکز تحقیقاتی مهندسی پیشرفته، واحد شهر مجلسی، دانشگاه آزد اسلامی

Received: 2016-06-20 Accepted : 2016-06-20 Published : 2016-05-21

Keywords: Magnesium Based Composite, Alumina Reinforcement, Infiltration Casting, Wear behavior,

Abstract :

One of the advanced routes for manufacturing the magnesium-matrix composites is infiltration casting into ceramic foams. In this research, magnesium-matrix composite AZ91-Al2O3 production has been investigated. Therefore, AZ91 alloy molten is prepared by usage of torch furnace under protection of MAGREX flux, then, poured in preheated mold at 250°C with preheated alumina foam at 800 °C. For investigating the effect of pressure, pressures at 50, 75 and 100 MPa in 1 minute applied until solidification was completed. For comparison, similar experiments were done without applying pressure. The results showed that solidification under pressure reduced porosity noticeably in comparison with gravity casting to 60%. By addition the ceramic reinforcement to the base alloy, mechanical strength reduced due to formation of MgAl2O4 spinel phase at interface and formation of residual compression stresses because of thermal mismatch between matrix and reinforcement. The mechanical strength and ductility of the samples are increased by rising of applied pressure to (0-100 MPa) due to decrease grain size and better strength interface of alumina and alloy. Additionally, wear rate due of composite decreased in comparison to base alloy declined markedly (about 53%). This may be due to higher intrinsic alumina strength. Also, by applying pressure on molten metal during solidification, wear rate is noticeably lesser than similar gravity sample due to decreasing the grain size and markedly declining the porosity. The dominant mechanism for base alloy is adhesive wear and for composite is abrasive wear and delamination.

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