Abstract
The overall aim of the work reported in this paper is to explore whether a physics-based simulation approach has the potential to reduce the uncertainty & variability associated with both predicting & managing maintenance costs and improving engine design to optimise through-life economic performance. The main novelty in the paper is to demonstrate how an innovative Digital Geometry model can represent typical in-service component degradation and then support appropriate simulation meshes to permit degraded performance to be predicted. Two examples are given: blade erosion from particulates; and a simulated cooled blade burn-through event.
Volume Subject Area:
Aircraft Engine
Topics:
Gas turbines,
Physics,
Simulation,
Blades,
Engine design,
Erosion,
Geometry,
Maintenance,
Particulate matter,
Uncertainty
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