• 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