Overview
ABSTRACT
This article gives an overview of the fracture mechanics through definitions and basic concepts to implement life analyzes, based on the existence of a defect ? assumed as a crack - and its propagation under the influence of thermomechanical loading, for structures and assemblies. It is also accompanied by informations regarding industry issues and certification regulations, especially in the field of aviation, which led engineers to integrate increasingly fracturemMechanics in its design cycles.
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Juan-Antonio RUIZ-SABARIEGO: ENS Cachan, Associate Professor of Mechanics - Doctorate in Mechanics and Materials - Head of "Advanced Mechanical Methods" unit, "Development Methodologies and Tools" department - Safran – Snecma , Villaroche site
INTRODUCTION
From the beginning of the industrial era to the end of the first half of the 20th century, engineers were confronted with unexplained rupture phenomena directly involving human safety. Boiler explosions, gas appliance explosions, sudden ruptures of liberty-ships during the Second World War, in-flight explosions of the first Comet commercial aircraft equipped with turbojet engines in the 1950s. These cases can be considered as the founders of fracture mechanics, whose theory, based on the presence of cracks, was developed in the first half of the 20th century, with the first applications in industry starting in the 1960s. Since then, fracture mechanics has gone from strength to strength, and the development of computer science has opened the way to numerical methods that can model complex cracks as closely as possible, with simulation times compatible with industrial design cycles.
In this article, we will review the principles that are important to know when dealing with fracture mechanics, then present the concepts of linear fracture mechanics, which enable engineers to deal with defect propagation via the concept of stress intensity factor and the laws describing cracking kinetics. Finally, a focus will be given on an industrial application in the aeronautics industry, with information on regulatory aspects and the implementation of a fatigue cracking study for a turbomachinery part.
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KEYWORDS
defects | cracking | energy | nuclear | aeronautics | transports
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Fracture mechanics
Bibliography
Software tools
MorfeoCrack (Cenaero)/plugin for Samcef (LMS-Samtech) http://www.cenaero.be/
DARWIN™ http://www.darwin.swri.org
ESACRACK http://www.esacrack.com
Events
International Conference on Fracture and Damage Mechanics
International Conference on Fatigue Damage of Structural Materials (Hyannis, USA)
Standards and norms
- Certification procedures for products and parts advisory circular – Damage tolerance for high energy turbine engine rotors US department of transportation – Federal aviation administration http://www.faa.gov/regulations_policies/advisory_cirulars/index.cfm/go/document.information/documentID/22920 - AC 33.14-1 -
- Amendment 1, European aviation safety agency http://www.easa.europa.eu/agency-measures/docs/agency-decisions/2010/2010-015-R/CS-E_amendment%203/pdf...
Directory
Manufacturers – Suppliers – Distributors (non-exhaustive list)
SAFRAN – Snecma Civil, military and aerospace engine manufacturer http://www.snecma.com
Organizations – Federations – Associations (non-exhaustive list)
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