Application of multi-scale modelling in aeroengine component life assessment

Autor:	D. P. Shepherd, G. F. Harrison, T. J. Ward, P.H Tranter
Rok vydání:	2004
Předmět:	Engineering Turbine blade Scale (ratio) business.industry Mechanical Engineering Metal matrix composite Turbojet Structural engineering Condensed Matter Physics Ceramic matrix composite law.invention Creep Mechanics of Materials law Component (UML) Service life General Materials Science business
Zdroj:	Materials Science and Engineering: A. 365:247-256
ISSN:	0921-5093
DOI:	10.1016/j.msea.2003.09.034
Popis:	The paper provides an overview of the procedures used to determine the safe service lives of aeroengine components, with particular reference to the role of scale in lifing models. It is shown how the volume of material tested influences the declared service life of fracture critical components. The development of a combined micromechanical–macromechanical model for the life assessment of the anisotropic behaviour of advanced single crystal turbine blade materials is discussed. The role of micro-scale modelling in predicting the low cycle fatigue (LCF) behaviour of long fibre metal matrix composite components is also discussed. The final case considered is that of al microstructural model used in the life assessment of ceramic matrix composites.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::b98fa7410dfaeb2d51bf46832deed849 https://doi.org/10.1016/j.msea.2003.09.034 Zobrazit plný text záznamu Full Text from ScienceDirect