Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Xuande Yue"'
Publikováno v:
Advances in Mechanical Engineering, Vol 13 (2021)
Composite-aluminum structures exist in aircraft structures generally. It is easy to cause gap between mating surfaces in composite-aluminum assembled structures with the curing deformation of composite. The composite-aluminum, single-lap, single-bolt
Externí odkaz:
https://doaj.org/article/b005c593ae7641f9a37f282fa569cc87
Publikováno v:
International Journal of Aerospace Engineering, Vol 2020 (2020)
The composite-aluminum hybrid bolted structures are widely used in aircraft. Due to low molding accuracy of composite components, gaps always occur between components during assembly. In this case, the bolt connection can cause a complex strain and s
Externí odkaz:
https://doaj.org/article/4561ee521dde4bf09f527433cbc05e6d
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science (Sage Publications, Ltd.); Apr2024, Vol. 238 Issue 8, p3578-3601, 24p
Akademický článek
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Autor:
Pramanik, Sumit, Datta, Shubhabrata, Cheralathan, M., Xuande, Yue, Xiaogang, Dang, Tao, Geng, Honghao, Zhang, Ying, Xie
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science; April 2024, Vol. 238 Issue: 8 p3578-3601, 24p
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science (Sage Publications, Ltd.); Dec2023, Vol. 237 Issue 23, p5708-5733, 26p
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 236:1099-1118
The influence of both preload and the presence of shim types on the mechanical properties of composite-aluminium single-bolt, single-lap joints were studied in this paper. The load-displacement curve and surface strain field of joints in different sh
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. :095440622211493
There is bolt preload loss under vibration in the aircraft rudder, of which the connected parts are steel beam and CFRP panel, and the fastener is bolts and self-lock jet nuts. Based on the above phenomenon, this paper analyzes rotational loosening,
Publikováno v:
International Journal of Aerospace Engineering, Vol 2020 (2020)
The composite-aluminum hybrid bolted structures are widely used in aircraft. Due to low molding accuracy of composite components, gaps always occur between components during assembly. In this case, the bolt connection can cause a complex strain and s
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:851-860
The mechanical behaviors of composite assembly structures of aircraft might change due to filling the fit-up gap between two components with liquid shim or laminated shim. In order to investigate the change qualitatively and quantitatively, a kind of