Influence of Heat Treatment on the Mechanical Properties and Damage Development in a SiC/Ti-15-3 MMC
Author:
Miller David A.1, Lagoudas Dimitris C.1
Affiliation:
1. Department of Aerospace Engineering, Center for Mechanics of Composites, Texas A&M University, College Station, TX 77843-3141
Abstract
Titanium alloys are commonly heat-treated to meet specific design requirements. In an effort to possibly create a better composite, the influence of heat treatments on the damage evolution and strength of a SiC/Ti-15-3 metal matrix composite (MMC) was studied. Heat treatments of 450°C and 700°C for 24 hours were performed on axial and transverse unidirectional specimens. These specimens, in addition to specimens in the as-received condition, were tested under nonproportional loading paths and then microstructurally analyzed to determine the induced damage. The axial composite with the 450°C heat treatment showed the highest elastic modulus and the lowest stiffness reduction than the other heat treatment conditions. The transverse composite in the as-received condition showed the highest room temperature elastic modulus and the lowest stiffness reduction compared with other heat treatment conditions. Typical damage modes of Ti MMC’s, such as fiber/matrix debonding and matrix microcracking, were seen in all heat treatments. A micromechanics model based on the Mori-Tanaka averaging scheme was implemented to simulate the effects of micro-cracking induced damage on composite stiffness reduction. [S0094-4289(00)01101-4]
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Reference17 articles.
1. Johnson, W. S., 1992, NASA Technical Memorandum 107597, Lewis Research Center. 2. Lissenden Herakovich, C. T., and Pindera, M. J., 1995, “Response of SiC/Ti under Combined Loading Part I: Theory and Experiment for Imperfect Bonding,” J. Compos. Mater., 29, No. 2, pp. 130–155. 3. Majumdar, B. S., and Newaz, G. M., 1992a, 1992b, 1993, NASA Contractor Report 189095, 189096, 191181, Lewis Research Center. 4. Lagoudas, D. C., Ma, X., Miller, D. A., and Allen, D. H., 1995, “Modeling of Oxidation in Metal Matrix Composites,” Int. J. Eng. Sci., 33, pp. 2327–2343. 5. Newaz, G. M., Majumdar, B. S., and Brust, F. W., 1992, “Thermal Cycling Response of Quasi-Isotropic Metal Matrix Composites,” ASME J. Eng. Mater. Technol., 114, pp. 156–161.
Cited by
7 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
|
|