• DocumentCode
    2353462
  • Title

    Analysis of movement and stability of the root lock mechanism of the space deployable mast

  • Author

    Liu, Heping ; Luo, Ani ; Zhang, Lixun

  • Author_Institution
    Harbin Eng. Univ., Harbin, China
  • fYear
    2010
  • fDate
    4-7 Aug. 2010
  • Firstpage
    1175
  • Lastpage
    1178
  • Abstract
    The root lock mechanism is a key component of the space deployable mast and influences the function of the mast directly. After analysis of the root lock mechanism, it is simplified as a kind of mechanism with two sliders and a spring. At first, when the mechanism carries out the lock actions, the vibration equation of the slider 2 is set up in the local coordinates, and then the displacement expression of the slider 2 is obtained in the whole coordinates by the coordinate transform. When the root lock mechanism is disturbed after the mast is locked, the vibration equation of the mechanism is set up. In the situation, stability of the root lock mechanism is analyzed, and relations and constraint conditions of the structural parameters are gotten. Actual values of these structural parameters are decided on further. Finally, numerical simulation is utilized to check up the movement of the root lock mechanism. After the analysis, selection of structural parameters is more reasonable and the design is more correct.
  • Keywords
    aerospace engineering; keys (locking); numerical analysis; springs (mechanical); supports; vibrations; coordinate transform; displacement expression; movement analysis; numerical simulation; root lock mechanism; sliders; space deployable mast; spring; stability analysis; structural parameters; vibration equation; Equations; Force; Frequency modulation; Mathematical model; Springs; Structural engineering; Vibrations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation (ICMA), 2010 International Conference on
  • Conference_Location
    Xi´an
  • ISSN
    2152-7431
  • Print_ISBN
    978-1-4244-5140-1
  • Electronic_ISBN
    2152-7431
  • Type

    conf

  • DOI
    10.1109/ICMA.2010.5588167
  • Filename
    5588167