The paper presents the results of calculating the strength properties for the fan blades of a regional aircraft gas turbine engine under consideration of manufacturing deviations. The models of blades with different geometric deviations on the airfoil being analyzed, the design model of the fan assembly, the strength properties being estimated, and the design scheme for a set of blades are described. An example of the calculation results is given.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 62 , 4 ; 535-543


    Publication date :

    2019-10-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties

    Arkhipov, A. N. / Volgina, M. V. / Matushkin, A. A. et al. | Online Contents | 2019


    Compensation of geometric deviations in 5-axis-milling of gears

    Staudt,J. / Klocke,F. / Loepenhaus,C. et al. | Automotive engineering | 2015


    A Hybrid Propeller Blade Strength Analysis

    Deliporanides, G. / Royal Institution of Naval Architects | British Library Conference Proceedings | 2007


    Device for measuring geometric dimension of blade

    HAN DONGHUA / XU LIGUO / MA XINWEI et al. | European Patent Office | 2022

    Free access

    Compass deviations

    Ward, William C. | Engineering Index Backfile | 1910