## Abstract Today, specific material data, mainly from static material tests, are not sufficient to design parts of a product to assess lifetime behaviour, especially when local complex loading occurs like low cycle fatigue (LCF) and thermo mechanical fatigue (TMF). In this work, specimen tests are
Modelling and lifing of structural materials for future aeroengine components
β Scribed by G. F. Harrison; M. R. Winstone
- Book ID
- 104636595
- Publisher
- Springer
- Year
- 1996
- Tongue
- English
- Weight
- 922 KB
- Volume
- 3
- Category
- Article
- ISSN
- 0929-1881
No coin nor oath required. For personal study only.
β¦ Synopsis
This paper reports on some of the major research and development activities at the SMC into materials modelling of existing advanced high strength superalloys and the work in progress to understand the step change materials which will have to be introduced into future engines to meet the perceived performance requirements. These studies are aimed at developing appropriate lifing methodologies and ensuring safe service usage of these materials. Lifing models for dwell sensitive titanium alloys, powder metallurgy materials, single crystal alloys, metal matrix composites and intermetallic alloys are considered.
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There appear more critical requirements for special functions of components/products in various areas, which can be satisfied only by using heterogeneous materials and/or smart materials. The heterogeneous materials include composite materials, functionally graded materials, and heterogeneous materi