Fundamentals of Materials Science and Engineering: An Integrated Approach, 3e

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GTBL042-15 GTBL042-Callister-v2 August 29, 2007 8:52


646 • Chapter 15 / Composites

Crack

(a) (b)
Tetragonal
ZrO 2
particles

Tetragonal
ZrO 2
particles

Monoclinic
ZrO 2
particles

Crack

Stress
field
region

Figure 15.12
Schematic
demonstration of
transformation
toughening. (a)A
crack prior to
inducement of the
ZrO 2 particle phase
transformation. (b)
Crack arrestment
due to the
stress-induced phase
transformation.

by (1) deflecting crack tips, (2) forming bridges across crack faces, (3) absorbing en-
ergy during pull-out as the whiskers debond from the matrix, and/or (4) causing a
redistribution of stresses in regions adjacent to the crack tips.
In general, increasing fiber content improves strength and fracture toughness;
this is demonstrated in Table 15.10 for SiC whisker-reinforced alumina. Furthermore,
there is a considerable reduction in the scatter of fracture strengths for whisker-
reinforced ceramics relative to their unreinforced counterparts. In addition, these
CMCs exhibit improved high-temperature creep behavior and resistance to thermal
shock (i.e., failure resulting from sudden changes in temperature).
Ceramic-matrix composites may be fabricated using hot pressing, hot isostatic
pressing, and liquid phase sintering techniques. Relative to applications, SiC whisker-
reinforced aluminas are being utilized as cutting tool inserts for machining hard metal
alloys; tool lives for these materials are greater than for cemented carbides (Section
15.2).

15.11 CARBON–CARBON COMPOSITES
One of the most advanced and promising engineering material is the carbon fiber-
carbon–carbon reinforced carbon-matrix composite, often termed acarbon–carbon composite;as
composite the name implies, both reinforcement and matrix are carbon. These materials are

Table 15.10 Room-Temperature Fracture Strengths and
Fracture Toughnesses for Various SiC Whisker
Contents in Al 2 O 3

Whisker Content Fracture Strength Fracture Toughness
(vol%)(MPa)(MPa


m)
0 — 4.5
10 455 ± 55 7.1
20 655 ± 135 7.5–9.0
40 850 ± 130 6.0
Source:Adapted fromEngineered Materials Handbook,Vol. 1,
Composites,C. A. Dostal (Senior Editor), ASM International, Materials
Park, OH, 1987.
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