Life extension of critical ‘Group A’ components with a view to implement robust process for protection of these components by introducing protective tooling & management of this tooling into the build process for Trent 900 engines at Rolls Royce Plc Derby’s civil aerospace operation
Attributed to the high engine operating temperatures and stresses at which the Trent 900 critical ‘Group A’ parts operate, the predicted damage tolerant life for a number of components is tending toward the engine shop-visit interval. This report provides an introduction to the issue, discusses the...
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| Format: | Dissertation (University of Nottingham only) |
| Language: | English |
| Published: |
2010
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| Online Access: | https://eprints.nottingham.ac.uk/23830/ |