A new reverse educing method (REM) is presented to estimate the vibrational stress on rotating aeroengine blades from the actual fracture section. This method does not conform to the traditional calculating method, but involves the reverse solution idea. The value of the crack propagation ratio da/dN can be obtained from the actual fracture section of the blade, and then the vibrational stress on rotating blades can be calculated through static computation, modal analysis and crack stress intensity factor calculation. The result is very significant for fault diagnosing and shooting of aeroengine blades.


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    Title :

    A new method to calculate the vibrational stress of rotating blades


    Contributors:
    Li, Hai-Yan (author) / Zhang, Xue-Ren (author) / Yan, Xiao-Jun (author) / Nie, Jing-Xu (author)


    Publication date :

    2001-02-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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