The results of the experimental study of the structural carbon fiber reinforced plastic (CFRP) erosion resistance applied to gas turbine engine structural elements are presented. A methodology for characterizing the process of gas abrasive wear of thin-walled structures made of polymer composite materials has been developed. The factors are found that determine the level of the abrasive effect of dust and gas mixture formed at the take-off and landing. A criterion for material erosion resistance assessment is presented.


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    Titel :

    Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 62 , 4 ; 696-703


    Erscheinungsdatum :

    2019-10-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow

    Zinin, A. V. / Dobrovol’skii, S. V. / Lebedev, A. K. et al. | Online Contents | 2019



    ABRASIVE WEAR

    SAE Technical Papers | 1966


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    A Composite Approach to Reducing Abrasive Wear

    Davies,B.J. / Wilding,D.H. / Canron,Foundry Div.,US | Kraftfahrwesen | 1983