The work is devoted to assessing the reliability of the attachment to the fuselage of aircraft engines, which directly determines the safety and reliability of the aircraft. To do this, the choice was made of the rational design of the front span. Comparison of design options and the selection of the most preferred of them were based on the chosen criterion. The choice of the variant of the scheme was carried out in order to minimize the weight of the optimized unit. The criterion function value was calculated using the End Elements Method (ICE) in the COSMOS program in SolidWorks (CAE). Tensions, loads and deformations were calculated. The results of calculations for the spangot were also verified using COSMOS. As a result, the divergence of the results of theoretical calculations and calculations COSMOS was no more than 1.2%.


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    Titel :

    Choosing a Rational Design of the Engine Fastening Span


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Radionov, Andrey A. (Herausgeber:in) / Gasiyarov, Vadim R. (Herausgeber:in) / Tereshonkov, V. A. (Autor:in) / Shavelkin, D. S. (Autor:in) / Pocebneva, I. V. (Autor:in)

    Kongress:

    International Russian Automation Conference ; 2021 ; Sochi, Russia September 05, 2021 - September 11, 2021



    Erscheinungsdatum :

    2022-01-18


    Format / Umfang :

    16 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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