August 17, 2025

Maintenance of Jet Engines: Robust Parametrisation and Reconstruction of Compressor and Turbine Blades

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Robust parametrisation methods enhance jet engine efficiency and reliability in inspections, reducing performance variability.
General-purpose methods for geometric analysis support both nominal and deteriorated compressor and turbine blades.
Developed methods focus on camber line determination, airfoil profile description, and accurate shape reconstruction at edges.
Reliable frameworks have fewer assumptions compared to tailored methods for specific turbine stages, improving analysis.

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Implication

Analysis enhances efficiency by improving geometric inspection of compressor and turbine blades, suggesting reliable methods for deterioration effects.

Cite This Study

Dammann et al. (2025) studied this question.

synapsesocial.com/papers/68c2368eb210217d647751f5 https://doi.org/10.1115/gt2025-151573

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Implication

Analysis enhances efficiency by improving geometric inspection of compressor and turbine blades, suggesting reliable methods for deterioration effects.

Maintenance of Jet Engines: Robust Parametrisation and Reconstruction of Compressor and Turbine Blades

Key Points

Discussion

Implication

Cite This Study

Maintenance of Jet Engines: Robust Parametrisation and Reconstruction of Compressor and Turbine Blades

Key Points

Discussion

Implication

Cite This Study

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