Microstructural Differences between Woven Mat and Acrylic Binder TMC and their Relationship to Fatigue Damage Modes

Author:

Harmon D.1,Jerina K. L.2,Sastry S. M. L.2

Affiliation:

1. McDonnell Douglas Aerospace, PO. Box 516, Mailcode 1021322, St. Louis, MO 63166

2. Washington University, Campus Box 1087, One Brookings Drive, St. Louis, MO 63130

Abstract

Extensive microstructural evaluations were performed on two titanium matrix composite (TMC) materials to examine any chemical and/or physical differences which explain fatigue crack growth patterns observed in these materials. These examinations included optical microscopy, scanning electron microscopy (SEM), energy dispersive X-ray (EDX) and Auger analysis. The results of these studies indicate that fatigue damage modes, in addition to being affected by obvious parameters like load and temperature are also affected by the process in which the TMC is consolidated. Fiber surface damage is visible on one of the two TMC systems which may have influenced the observed fatigue damage mode. The fiber surface damage can be traced back to the pressure applied to the laminate during consolidation. This paper provides a detailed explanation for the occurrence of the different fatigue damage modes and, therefore, provides an explanation for the significant difference in fatigue life of the two materials.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Cited by 3 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

1. Titanium matrix reinforced composites produced by hot pressing of plasma-sprayed preforms;Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications;2003-10-01

2. Titanium matrix reinforced composites produced by hot pressing of plasma-sprayed preforms;P I MECH ENG L-J MAT;2003

3. Effect of in situ material properties on fatigue damage modes in titanium matrix composites;Metallurgical and Materials Transactions A;1999-02

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