Research on Multi-Excitation Source United Controlling Test Method Based on Distributed Actuation

Jun Yao; Yan Fei Wu; Ming Ge Xu

doi:10.4028/www.scientific.net/AMR.291-294.2168

Paper Titles

Based the GM Reliability on the Application of Mechanical Product Evaluation
p.2149

Reliability of Cermet Cladding Parts Based on the Failure Tree Series
p.2153

The Study of Fuzzy Reliability of Concrete Durability after Corrosion of Steel-Bars
p.2159

Reliability Assessment of a Certain Diesel Engine with Multi-Parameter Degradation Based on SVDD
p.2164

Research on Multi-Excitation Source United Controlling Test Method Based on Distributed Actuation
p.2168

Stress Conditions for Surface Analysis of Butyl Rubber Lining
p.2175

An Approach to Fatigue Reliability Analysis Based on the Hybrid Model of Probability and Non-Probability
p.2179

Local Monte Carlo Simulation for the Reliability Sensitivity Analysis
p.2183

Important Sampling for Structural Reliability Based on Radial Basis Function Neural Network
p.2189

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 291-294Research on Multi-Excitation Source United...

Research on Multi-Excitation Source United Controlling Test Method Based on Distributed Actuation

Abstract:

In view of the questions of high-speed aircraft withstanding complicated vibration environment, their vibration durability could not being plenary examined by existing vibration test technology, a vibration test technique integrating piezoelectric element, vibrating table, exciter is proposed. The vibration environment dimension of high-speed aircraft and its influence to the failures of high-speed aircraft are analysed. Based on the research on the material and actuation dimension of the piezoelectric element, the feasibility of piezoelectric element used as the distributed excitation source in vibration test is analysed. Last, a test demonstration system is constituted and a serials of test items are carried out. The rationality and the extensive engineering application potential of this technique are verified by the test results.

You might also be interested in these eBooks

Materials Processing Technology, AEMT2011

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 291-294)

Pages:

2168-2174

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.291-294.2168

Citation:

Cite this paper

Online since:

July 2011

Authors:

Jun Yao, Yan Fei Wu, Ming Ge Xu

Keywords:

Distributed Excitation, Piezoelectric Element, United Loading, Vibration Test

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Crawley E.F., "Intelligent Structures for Aerospace: A Technology Overview and Assessment", AIAA Journal, 1994, Vol.32, No.8 Aug. pp.1689-1699.

DOI: 10.2514/3.12161

Google Scholar

[2] Crawley E F, and Luis J. "Use of Piezoelectric Actuators as Elements of Intelligent Structures", AIAA J. 1987, Vol.25, No.1, pp.1373-1385.

DOI: 10.2514/3.9792

Google Scholar

[3] Forward R. L., "Electronic Damping of Resonance in global Structures", AIAA Paper No.81-0556, 1981.

Google Scholar

[4] Hubbard J. E. and Burke, S. E. "Distributed Transducer Design for Intelligent Structural Components", Intelligent Structural System, Edited by H. S Tzou, Kluwer Academic, Norwell, Mar,n 1992.

Google Scholar

[5] Im S, and Atluri S N. "Effect of Piezo-Actuators on a Finitely Defermationed Beam Subjected to General Loading". AIAA J., Vol.27, 1989, pp.1801-1807.

DOI: 10.2514/3.10337

Google Scholar