A series of neutron diffraction measurements have been carried out to determine the elastic residual strains deep within a large, 40-cm-diameter, forged and water-quenched IN718 aeroengine compressor disc. Neutron path lengths of up to 6 cm were necessary to probe the thickest parts of the forging, and three-dimensional strain and stress components have been derived for the first time in such a large superalloy specimen. Measurements have been compared with the results from a coupled thermal-mechanical finite-element model of the quenching process, based on appropriate temperature-dependent material properties, with some success. The general residual stress state in the disc is one of near-surface compression, balanced by tension within the disc interior. The steepest stress and strain gradients occur in the transition region from compression to tension, about 1 cm below the surface all around the disc. The largest stress component is in the disc tangential direction and reaches a magnitude of 400 to 500 MPa near the disc surface and at its core. This exceeds the effective yield stress because of the presence of significant hydrostatic stress.


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    Title :

    Residual stresses in a quenched superalloy turbine disc: Measurements and modeling


    Additional title:

    Eigenspannungen in einer abgeschreckten Turbinenscheibe aus einer Superlegierung: Messungen und Modellierung


    Contributors:
    Rist, M.A. (author) / Tin, S. (author) / Roder, B.A. (author) / James, J.A. (author) / Daymond, M.R. (author)


    Publication date :

    2006


    Size :

    9 Seiten, 11 Bilder, 26 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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