Kei Yamamoto
Purdue University School of Materials Engineering
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Introduction
Carbon-carbon composites are made up of crystalline (graphitic) carbon fibers embedded in an amorphous carbon matrix. They have a very high melting point, low coefficient of thermal expansion, a great thermal shock resistance and they keep all these properties at temperatures of over 2000oC. They are used for a wide variety of applications, including brake friction materials for aircraft and for racing cars. Four aircraft brakes manufactured in different ways will be studied.
Project Objectives
- Develop techniques of microstructural inspection that are appropriate for this material system.
- Determine volume fraction of fiber, amorphous material and porosity.
- Study crystallinity of fibrous material
Approach
- Examine porosity and fiber alignment using the optical microscope
- Perform microtomy on specimen to prepare it for transmitted light microscopy
- Study the crystal structure of the specimens using X-Ray diffraction
- Examine the fiber surface using the scanning electron microscope
- Examine the amorphous carbon using the scanning electron microscope
Findings
- Amorphous carbon matrix and carbon fibers are not well bound together, thus matrix is not providing any benefits to the structure
- Crystallinity of the carbon fibers varies considerably between specimens
- Carbon was only deposited on the surface in one of the specimens: amorphous carbon nucleation is found only very rarely on the fiber surfaces in this specimen.
![]() Figure 1: Carbon fibers (magnification of 1500X). |
![]() Figure 2: Carbon fibers (magnification of 2000X). |


