Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)

Feasibility Study of HHT Method on Helicopter Rotor Imbalance Fault Feature Extraction

Authors
Wen Cao, Zhen-hong Xing, Yi Yao, Meng Zhang
Corresponding Author
Wen Cao
Available Online August 2015.
DOI
10.2991/icmeis-15.2015.70How to use a DOI?
Keywords
HHT; EMD; Helicopter Rotor imbalance fault; Feature extraction
Abstract

Firstly, using the Hilbert-Huang Transform (HTT) methods of data for the empirical mode decomposition (EMD), so as to extract the Intrinsic mode function (IMF) of the signal , and then do Hilbert transform to get the Hilbert spectrum of the signal. The method has great advantages to non-linear and non-stationary data signal. For helicopter rotor imbalance fault causes the body to the vibration characteristics of the data, the marginal spectrum analysis its, can get the valid fault feature.

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 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
Series
Advances in Engineering Research
Publication Date
August 2015
ISBN
978-94-62520-98-1
ISSN
2352-5401
DOI
10.2991/icmeis-15.2015.70How 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  - Wen Cao
AU  - Zhen-hong Xing
AU  - Yi Yao
AU  - Meng Zhang
PY  - 2015/08
DA  - 2015/08
TI  - Feasibility Study of HHT Method on Helicopter Rotor Imbalance Fault Feature Extraction
BT  - Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
PB  - Atlantis Press
SP  - 382
EP  - 386
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmeis-15.2015.70
DO  - 10.2991/icmeis-15.2015.70
ID  - Cao2015/08
ER  -