Thermal Expansion of Aluminum-Fly Ash Cenosphere Composites Synthesized by Pressure Infiltration Technique

¹ Department of Materials Engineering, University of Wisconsin-Milwaukee, 3200 N. Cramer St., Milwaukee, WI 53211, USA
² Department of Mechanical, Aerospace and Manufacturing Engineering, Polytechnic University, Brooklyn, NY 11201, USA
³ Department of Mechanical Engineering, Birzeit University, Birzeit, Palestine

^* To whom correspondence should be addressed.

	Abstract

The coefficients of thermal expansion (CTEs) of commercially available pure aluminum and aluminum alloy composites containing hollow fly ash particles (cenospheres) of average size 125 µm are measured using a dilatometer. Three types of composites are made using the pressure infiltration technique at applied pressures and infiltration times of 35 kPa for 3 min, 35 kPa for 7 min, and 62 kPa for 7 min. The volume fractions of the fly ash cenospheres in the composites are around 65%. The CTE of the composites is measured to be in the range of 13.1 x 10^-6-11 x 10^-6/°C, which is lower than that of pure aluminum (25.3 x 10^-6/°C). The infiltration processing conditions are found to influence the CTE of the composites. A higher applied pressure and a longer infiltration time lead to a lower CTE. The theoretical value of the CTE of fly ash cenospheres is estimated to be 6.1 x 10^-6/°C.

Key Words: aluminum, metal matrix composites, solidification, coefficient of thermal expansion

First published on September 20, 2005, doi:10.1177/0021998305057379

Journal of Composite Materials 2006;40:1163.

A more recent version of this article appeared on July 1, 2006


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