To consider the corrosive effects on aircraft structural life under natural environments, we have the calendric life to represent its impact. A new concept of Aircraft Structural Life Envelope (ASLE) to consider the combined effects of fatigue loads and corrosive conditions is developed and the sketch of ASLE is presented, then the basic determining methods of ASLE under different corrosive conditions are obtained too. Finally the linear damage cumulative rules are employed to analyze the usage of aircraft in different corrosive conditions, and the residual fatigue life and calendric life of aircraft structures can be predicted and supervised.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Fatigue Life Supervision of Aircraft Structures under Corrosive Conditions



    Published in:

    Key Engineering Materials ; 324-325 ; 703-706


    Publication date :

    2006-11-15


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Service life supervision for aircraft structures under corrosive environment

    Xiaofan, H. / Wenting, L. / Dongbin, J. | British Library Online Contents | 2003


    Evaluation of fatigue lives for civil aircraft structures under corrosive condition

    Wenting, L. / Hongyuan, Y. / Xiaofan, H. | British Library Online Contents | 2004




    Influence of Corrosive Environment on the Fatigue Life of an Aging Aircraft Structure

    Labeas, G. / Kermanidis, T. / Pantelakis, S. et al. | British Library Conference Proceedings | 1999