The Design of Quadcopter Frame Based On Finite Element Analysis

DOI

10.2991/icmra-15.2015.260How to use a DOI?

Keywords

Quadcopter Ansys Static and model analysis

Abstract

The frame is an important basis for aircraft structural the design improvements and innovation as a whole frame bearing member. Early in the design stage, a large number of samples are used in the collision and reliability test, which not only causes a waste of resources, but also puts a lot of manpower and resources. So the development cycle is quite lengthy. With the continuing development of computer technology and scientific calculations, the introduction of the finite element method greatly shorten the development cycle frame. More and more machinery and aerospace companies have seen finite element structural analysis as a necessary part of the mechanical development. Using the finite element method, optimization of key parts of the machine and the machine has become an indispensable part of the development process. This paper will analyze the static and modal frame, in order to reflect the important role of finite element analysis in the frame design.

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/).

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TY  - CONF
AU  - Pan Wei
AU  - Zijian Yang
AU  - Quanzi Wang
PY  - 2015/04
DA  - 2015/04
TI  - The Design of Quadcopter Frame Based On Finite Element Analysis
BT  - Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation
PB  - Atlantis Press
SP  - 1353
EP  - 1356
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmra-15.2015.260
DO  - 10.2991/icmra-15.2015.260
ID  - Wei2015/04
ER  -