Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials

The Modal Analysis of Turbine Rotor Based on Application of ANSYS Software

Authors
Wenya Li, Yan Zheng
Corresponding Author
Wenya Li
Available Online July 2015.
DOI
10.2991/icimm-15.2015.276How to use a DOI?
Keywords
Modal analysis; ANSYS; Finite element model; Turbine Rotor.
Abstract

As the basis of dynamic analysis, modal analysis can be used to determine the vibration characteristics of mechanical institutions themselves, briefly expounds the basic principle of modal analysis and modal analysis under the environment of ANSYS, and the steps, and a specific example, for turbine rotor calculation of modal analysis shows that the method of modal analysis in ANSYS software, the results show that this method for determine the vibration characteristics of the mechanical structure works, can fully meet the requirements of structural 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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Volume Title
Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials
Series
Advances in Engineering Research
Publication Date
July 2015
ISBN
10.2991/icimm-15.2015.276
ISSN
2352-5401
DOI
10.2991/icimm-15.2015.276How to use a DOI?
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  - Wenya Li
AU  - Yan Zheng
PY  - 2015/07
DA  - 2015/07
TI  - The Modal Analysis of Turbine Rotor Based on Application of ANSYS Software
BT  - Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials
PB  - Atlantis Press
SP  - 1512
EP  - 1515
SN  - 2352-5401
UR  - https://doi.org/10.2991/icimm-15.2015.276
DO  - 10.2991/icimm-15.2015.276
ID  - Li2015/07
ER  -