Research on aircraft components assembly tolerance design and simulation technology
- DOI
- 10.2991/ic3me-15.2015.410How to use a DOI?
- Keywords
- Aircraft assembly, Tolerance design, Simulated analysis
- Abstract
With the rapid development of aircraft industry, manufacturing department needs to put forward higher requirements for the accuracy of aircraft assembly. It not only affects the overall quality of the aircraft but it also affects the cost of aircraft manufacturing. This paper introduces the ways about the improvement of the assembly accuracy and guarantee of the quality of assembly, based on the conventional tolerance design, using 3DCS tolerance analysis software. It also elaborates on the tolerance design modeling technology and shows the simulation model of how tolerance analysis is set up. The VSA and 3DCS software are compared and the application methods that could be used in the design of aircraft assembly of the 3DCS tolerance simulation analysis software are discussed. The simulation of how the tolerance design is carried out for the assembly of aft fuselage and hatch door.The results are gained about the analysis of the assembly tolerance accordingly with the distribution, it directly analyses the aft hatch door dimensions under coordination of assembling.The necessary improvement and comprehensive optimization about dimensions ensure the quality and efficiency of the assembly of aft aircraft hatch door.
- Copyright
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Wei Wang AU - Hongjun Yu AU - Ahmed Shafeeu AU - Tianhui Gu PY - 2015/08 DA - 2015/08 TI - Research on aircraft components assembly tolerance design and simulation technology BT - Proceedings of the 3rd International Conference on Material, Mechanical and Manufacturing Engineering PB - Atlantis Press SP - 2140 EP - 2146 SN - 2352-5401 UR - https://doi.org/10.2991/ic3me-15.2015.410 DO - 10.2991/ic3me-15.2015.410 ID - Wang2015/08 ER -