Zobrazeno 1 - 10
of 88
pro vyhledávání: '"Lianyu Zheng"'
Publikováno v:
Applied Sciences, Vol 13, Iss 8, p 4999 (2023)
As a satellite’s critical load-bearing structure, the large-scale space deployable mechanism (LSDM) is currently assembled using ground precision constraints, which ignores the difference between the ground and space environments. This has resulted
Externí odkaz:
https://doaj.org/article/e7fab936a5ad43689fd273d7abf28f88
Publikováno v:
Virtual Reality & Intelligent Hardware, Vol 2, Iss 1, Pp 12-27 (2020)
Background: Assembly guided by paper documents is the most widespread type used in the process of aircraft cable assembly. This process is very complicated and requires assembly workers with high-level skills. The technologies of wearable Augmented R
Externí odkaz:
https://doaj.org/article/c9d4b8ae9e484bda84f291b23174ee14
Publikováno v:
Applied Sciences, Vol 12, Iss 22, p 11729 (2022)
The ultrasonic vibration extrusion process is a widely used surface treatment process of stainless steel, e.g., 304 stainless steel, to improve the surface quality and increase hardness and wear resistance. However, for high-hardness 304 stainless st
Externí odkaz:
https://doaj.org/article/17a7a9a343584f27a4aabb0af507ef2c
Publikováno v:
Sensors, Vol 22, Iss 5, p 1991 (2022)
Monitoring surface quality during machining has considerable practical significance for the performance of high-value products, particularly for their assembly interfaces. Surface roughness is the most important metric of surface quality. Currently,
Externí odkaz:
https://doaj.org/article/9cb3cbf9ad9948d4b4f151e7458a6248
Publikováno v:
Medžiagotyra, Vol 21, Iss 4, Pp 568-573 (2015)
Materials of satellite integration truss frame are required to withstand temperature that range from about – 250 °C ~ + 150 °C. In order to reduce structural components deformation caused by such temperature change, material of truss frame mostly
Externí odkaz:
https://doaj.org/article/e465b50e8dfe448894a889abf4d93797
Publikováno v:
In Procedia CIRP 2022 109:526-531
Publikováno v:
The International Journal of Advanced Manufacturing Technology. 126:1261-1278
Publikováno v:
Robotics and Computer-Integrated Manufacturing. 84:102590
Publikováno v:
Journal of Intelligent Manufacturing.
Publikováno v:
Chinese Journal of Aeronautics. 35:441-454
Assembly interfaces, the joint surfaces between the vertical tail and rear fuselage of a large aircraft, are thin-wall components. Their machining quality are seriously restricted by the machining vibration. To address this problem, an in-process ada