## Abstract A three‐dimensional finite element analysis (FEA) has been used to determine the effect of implant elastic modulus on stresses in tissues around LTI carbon and aluminium oxide dental implants. The finite element model was constructed to represent a baboon mandible containing a blade typ
Parameters affecting the stress distribution around LTI carbon and aluminum oxide dental implants
✍ Scribed by Cook, S. D. ;Weinstein, A. M. ;Klawitter, J. J.
- Publisher
- John Wiley and Sons
- Year
- 1982
- Tongue
- English
- Weight
- 478 KB
- Volume
- 16
- Category
- Article
- ISSN
- 0021-9304
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✦ Synopsis
Abstract
Three‐dimensional finite element stress analysis was used to study the effects that implant neck geometry and the tissue properties at the implant‐bone interface have on the stress distribution around freestanding blade‐ and post‐type LTI carbon and aluminum oxide dental implants. Implants having neck flares of 13° and 26° were studied. In addition, to simulate fibrous encapsulation of the implant as opposed to a direct bone apposition retention mechanism, a soft tissue interposing layer between implant and bone was also modeled. The results of the study indicate that a reduction in neck flare from 26° to 13° was a positive design change for blade‐ and post‐type LTI carbon implants and blade‐type aluminum oxide implant but not for post‐type aluminum oxide implant. The results of the study indicate the presence of fibrous tissue surrounding the implants may be indicative of a failing system and may be the result of either hypophysiological stress (aluminum oxide implants) or hyperphysiological stress (LTI carbon implants).
📜 SIMILAR VOLUMES
The in vitro mechanical behavior of identical geometry LTI carbon, carbon-coated aluminum oxide, and uncoated aluminum oxide blade-type dental implants has been evaluated using rosette type strain gauges and a LVDT system. The implants served as a distal abutment for a three-unit fixed prosthesis an
## Abstract A three‐dimensional finite element stress analysis has been used to investigate the influence that variations in the infrastructural geometry of a blade‐type dental implant have on the stress distribution around LTI carbon and aluminum oxide implants. The finite element model was constr