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Effect of Framework in an Implant-Supported Full-Arch Fixed Prosthesis: 3D Finite Element Analysis
- Source :
- ResearcherID
- Publication Year :
- 2015
-
Abstract
- Purpose: The aim of this study was to analyze through a three-dimensional finite element analysis (3D-FEA) stress distribution on four implants supporting a fullarch implant-supported fixed prosthesis (FFP) using different prosthesis designs. Materials and Methods: A 3D edentulous maxillary model was created and four implants were virtually placed into the maxilla and splinted, simulating an FFP without framework, with a cast metal framework, and with a carbon fiber framework. An occlusal load of 150 N was applied, stresses were transmitted into peri-implant bone, and prosthodontic components were recorded. Results: 3D-FEA revealed higher stresses on the implants (up to +55.16%), on peri-implant bone (up to +56.93%), and in the prosthesis (up to +70.71%) when the full-acrylic prosthesis was simulated. The prosthesis with a carbon fiber framework showed an intermediate behavior between that of the other two configurations. Conclusion: This study suggests that the presence of a rigid framework in full-arch fixed prostheses provides a better load distribution that decreases the maximum values of stress at the levels of implants, prosthesis, and maxillary bone.
- Subjects :
- Materials science
implant
medicine.medical_treatment
Finite Element Analysis
Acrylic Resins
Dentistry
Prosthesis
Models, Biological
Bite Force
Stress (mechanics)
Dental Materials
User-Computer Interface
Imaging, Three-Dimensional
Carbon Fiber
framework
Materials Testing
medicine
Maxilla
Humans
Computer Simulation
Arch
Denture Design
Orthodontics
Dental Implants
Denture, Complete
business.industry
General Medicine
Finite element method
Carbon
Biomechanical Phenomena
Bite force quotient
immediate loading
Implant
Dental Prosthesis, Implant-Supported
Stress, Mechanical
Oral Surgery
business
3D-FEA
Dental Alloys
Subjects
Details
- Language :
- English
- Database :
- OpenAIRE
- Journal :
- ResearcherID
- Accession number :
- edsair.doi.dedup.....dba1123c1e0060b58a84d1eabce326f0