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Fracture of Turbine Blades under Self-Exciting Modes

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Fracture of Nano and Engineering Materials and Structures

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Abstract

Failure of blades of a turbo-compressor occurred during operation. Three different typical failure geometries were observed repeatedly. One mode was clearly identifiable as the first bending mode. The other two (Figs. 1–2) could not be directly identified.

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Authors and Affiliations

  1. Dipartimento di Ingegneria Meccanica e Gestionale, Politecnico di Bari, Viale Japigia 182, Bari, Italy

    C. A. Sciammarella, C. Casavola, L. Lamberti & C. Pappalettere

Authors
  1. C. A. Sciammarella
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  2. C. Casavola
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  3. L. Lamberti
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  4. C. Pappalettere
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Editor information

Editors and Affiliations

  1. Dept of Civil Engineering, Democritus University of Thrace, Xanthi, Greece

    E. E. Gdoutos

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© 2006 Springer

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Sciammarella, C.A., Casavola, C., Lamberti, L., Pappalettere, C. (2006). Fracture of Turbine Blades under Self-Exciting Modes. In: Gdoutos, E.E. (eds) Fracture of Nano and Engineering Materials and Structures. Springer, Dordrecht. https://doi.org/10.1007/1-4020-4972-2_212

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  • DOI: https://doi.org/10.1007/1-4020-4972-2_212

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-4020-4971-2

  • Online ISBN: 978-1-4020-4972-9

  • eBook Packages: EngineeringEngineering (R0)

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