## Abstract The purpose of this study is to investigate the subcritical crack growth (SCG) behavior of alumina‐glass dental composites. Alumina‐glass composites were fabricated by infiltrating molten glass to porous alumina preforms. Rectangular bars of the composite were subject to dynamic loading
Subcritical crack growth behavior of dispersion oxide ceramics
✍ Scribed by Armin Kirsten; Sabine Begand; Thomas Oberbach; Rainer Telle; Horst Fischer
- Publisher
- John Wiley and Sons
- Year
- 2010
- Tongue
- English
- Weight
- 284 KB
- Volume
- 95B
- Category
- Article
- ISSN
- 1552-4973
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✦ Synopsis
Abstract
Zirconia (Y‐TZP) is used as material for components of implants and prostheses because of its high short‐term strength. The mechanical long‐term reliability, however, is limited for Y‐TZP because of hydrothermal aging effects and a pronounced tendency for subcritical crack growth. The hypothesis of this study was that a substantial amount of alumina in a zirconia matrix can help to significantly suppress subcritical crack growth and thereby improve the mechanical long‐term reliability. The Weibull parameters as well as the parameters of the subcritical crack growth were determined for Alumina, Y‐TZP, and two dispersion ceramics, that is Alumina Toughened Zirconia (ATZ, 20% alumina/80% Y‐TZP), and Zirconia Toughened Alumina (ZTA, 75% alumina/25% Y‐TZP). The long‐term failure probability as a function of service time was predicted for the four ceramics. The parameter n of the subcritical crack growth was approx. 80% higher for ATZ compared to Y‐TZP. In consequence, the estimated lifetime revealed a significant better mechanical long‐term reliability for ATZ. It can be concluded that tailored dispersion oxide ceramics can address the aging problem of monolithic zirconia. This makes ATZ very interesting for components of joint replacement as well as for dental prostheses and implants. © 2010 Wiley Periodicals, Inc. J Biomed Mater Res Part B: Appl Biomater, 2010.
📜 SIMILAR VOLUMES
The subcritical growth of semi-elliptical surface cracks in the front face of a cylindrical disk was calculated. The disk represents a part of a turbine rotor. The stress intensity factors, which are the basis for the calculations presented here, were given in a former paper [l]. The load steps cons