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