Author： Hooker J.A. Doorbar P.J.
Publisher： Maney Publishing
ISSN： 1743-2847
Source： Materials Science and Technology, Vol.16, Iss.7-8, 2000-07, pp. : 725-731
Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.
Abstract
Metal matrix composites (MMCs) will play a significant role in the future of gas turbine aeroengine development. This paper outlines the benefits and some of the potential applications for Al and Ti MMCs and discusses issues involved in the introduction of this relatively new class of composite materials into engine components. The potential for cost savings and performance improvements which may be achieved by the introduction of silicon carbide particulate reinforced Al alloys (Al–SiCp MMC)are discussed, where the properties of the composite can be tailored to meet the requirements of a specific application. Some of the processing implications for Ti matrix composites (Ti MMCs) are explained for a range of component applications. Illustrations are given of how the manufacturing process can be controlled for a complex component. Finally, the influence of raw material, manufacturing, and component costs on the successful introduction of MMCs into aeroengines is discussed.
Related content
Toughness in metal matrix composites
By Friend C. M.
Materials Science and Technology, Vol. 5, Iss. 1, 1989-01 ,pp. :
Access to resources
Recommend
Design with metal matrix composites
By Shercliff H. R. Ashby M. F.
Materials Science and Technology, Vol. 10, Iss. 6, 1994-06 ,pp. :
By Harris S. J.
Materials Science and Technology, Vol. 4, Iss. 3, 1988-03 ,pp. :
By Baker Colin
Materials Science and Technology, Vol. 14, Iss. 9-10, 1998-09 ,pp. :
CORROSION OF ALUMINIUMBASED METAL MATRIX COMPOSITES,
Surface Engineering, Vol. 10, Iss. 3, 1994-01 ,pp. :