Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Shanyong Xuan"'
Publikováno v:
Journal of Intelligent Manufacturing and Special Equipment, Vol 4, Iss 1, Pp 64-81 (2023)
Purpose – Aircraft structures are mainly connected by riveting joints, whose quality and mechanical performance are directly determined by vertical accuracy of riveting holes. This paper proposed a combined vertical accuracy compensation method for
Externí odkaz:
https://doaj.org/article/43c8724b5dd04fc5a01894af0d1fe846
Publikováno v:
Materials, Vol 16, Iss 19, p 6361 (2023)
Composite patches are widely accepted as a useful practice for the repair of cracked aircraft components and the repair method is of vital importance to the final performance of the repaired structures. The present research experimentally studied the
Externí odkaz:
https://doaj.org/article/24ad51c276a7494baa2e3a2ebe80db3a
Publikováno v:
Materials Research Express, Vol 9, Iss 6, p 066301 (2022)
To obtain tunable microwave absorption, a strategy of constructing a frequency selective surface (FSS) on a two-layer composite is proposed. The designed FSS loaded two-layer composite is composed of a FSS constructed by evenly spaced circular copper
Externí odkaz:
https://doaj.org/article/d288afbab5424d0aa41776506063949d
Publikováno v:
Materials, Vol 14, Iss 15, p 4210 (2021)
The glass fiber reinforced polypropylene/AA2024 hybrid laminates (short for Al/Gf/PP laminates) as structural materials were prepared and formed by hot pressing. The synergistic effects of temperature and loading speed on the laminate deformation und
Externí odkaz:
https://doaj.org/article/47ca54a2dcfc4ae8bf8186991a33ec90
Publikováno v:
In Heliyon August 2023 9(8)
Publikováno v:
The International Journal of Advanced Manufacturing Technology. 126:4475-4494
Publikováno v:
Journal of Composite Materials. 57:393-407
This paper reports an experimental study on the forming mechanism and bearing behavior of single-lap composite riveted joints with different hole diameters (4.82 mm and 4.9 mm) and squeeze forces (15 KN, 18 KN, 20 KN, and 23 KN). Pressure riveting an
Publikováno v:
Assembly Automation. 42:293-305
Purpose Aerospace assembly demands high drilling position accuracy for fastener holes. Hole position error correction is a key issue to meet the required hole position accuracy. This paper aims to propose a combined hole position error correction met
Publikováno v:
Composite Structures. 311:116852
Publikováno v:
Materials
Volume 14
Issue 15
Materials, Vol 14, Iss 4210, p 4210 (2021)
Volume 14
Issue 15
Materials, Vol 14, Iss 4210, p 4210 (2021)
The glass fiber reinforced polypropylene/AA2024 hybrid laminates (short for Al/Gf/PP laminates) as structural materials were prepared and formed by hot pressing. The synergistic effects of temperature and loading speed on the laminate deformation und