7-days of FREE Audio papers, translation & more with Prime
7-days of FREE Prime access
7-days of FREE Audio papers, translation & more with Prime
7-days of FREE Prime access
https://doi.org/10.14489/hb.2021.03.pp.039-046
Copy DOIJournal: Spravochnik. Inzhenernyi zhurnal | Publication Date: Mar 1, 2021 |
The article describes a possibility of airframe weight-saving structural technique during supporting rib development by design space tailoring. For scientific mission is given below the supporting rib, the loading pattern, the shearingforce and bending-moment diagrams. The researches are undertaken by structural calculation aimed to choosing of the supporting rib design space, web thickness, a number of supporting carrier gates. Herewith, it should be noted that requirements of structural availability without crippling and attainment of safety margin are achieved. Calculation and optimization of supporting rib design space held for supporting rib, which is made of different metallic materials. The article says, that usage of modern method of airframe assembly allows to optimize the design spaces of supporting rib and reduce the weight of it. According to researches, analysis of total resulting is done, and recommendations for use are given.
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.