An advanced (segmented) combustor liner supplied by Pratt and Whitney Aircraft was tested in the structural component test rig at Lewis Research Center. It was found that the segmented liner operated at much lower temperatures than the conventional liner (about 400 F lower) for the same heat flux. At the lower temperatures and low thermal gradients, little distortion to the segments was observed. The operating conditions were not severe enough to distort or damage the segmented liner.


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    Titel :

    Structural response of an advanced combustor liner: Test and analysis


    Beteiligte:
    Moorhead, Paul E. (Autor:in) / Thompson, Robert L. (Autor:in) / Tong, M. (Autor:in) / Higgins, M. (Autor:in)


    Erscheinungsdatum :

    01.10.1987


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :