DocumentCode :
3359429
Title :
Vibration analysis and structural optimization of multifunctional structures on airborne electronic equipment
Author :
Qiao, Feng ; Huang, Dagui ; Feng, Wenjian
Author_Institution :
Sch. of Mechatron. Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
fYear :
2009
fDate :
9-12 Aug. 2009
Firstpage :
308
Lastpage :
312
Abstract :
The finite element method was utilized in this paper to analyze multifunctional structures on airborne electronic equipment. The results of this analysis show that the strengthened tendons can improve the inherent frequency of the structure, the density of screws arrangement can also affect its inherent frequency, and the circuit of elements should be placed symmetrically. Finally a new type of multifunctional structure with high inherent frequency was designed which had a better anti-vibration performance than the old one.
Keywords :
finite element analysis; optimisation; space vehicle electronics; vibrations; airborne electronic equipment; antivibration performance; finite element method; multifunctional structures; structural optimization; vibration analysis; Electronic equipment; Multifunctional structures; Structural Optimization; Vibration analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location :
Changchun
Print_ISBN :
978-1-4244-2692-8
Electronic_ISBN :
978-1-4244-2693-5
Type :
conf
DOI :
10.1109/ICMA.2009.5246028
Filename :
5246028
Link To Document :
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