• DocumentCode
    3411729
  • Title

    Design of Band-Style Lock-Unlock Mechanism for Space Arm

  • Author

    Wu, Binghui ; Deng, Zongquan

  • Author_Institution
    Harbin Inst. of Technol., Harbin
  • fYear
    2007
  • fDate
    5-8 Aug. 2007
  • Firstpage
    3537
  • Lastpage
    3542
  • Abstract
    A band-style lock-unlock mechanism for space-arms was proposed to assure locking of space-arms reliably. To light down mass of the whole mechanism, a centralized lock-unlock scheme was employed here. Several slider-crank mechanisms were driven by single crankshaft to accomplish the unlocking operation. Spiral spring was used to draw the clamp-band back due to its characteristics of storing much more energy in limited space. To assure normal operation of this lock-unlock mechanism, the kinematics and dynamics analysis of this crank-slider mechanism was presented. As the space arm will experience sever launching condition, the modal analysis of brackets, which are pivotal components in this mechanism, were accomplished with ANSYS. The simulative experimental results obtained on ground reveals that this lock-unlock mechanism can implement the objectives mentioned above.
  • Keywords
    aerospace robotics; manipulator dynamics; manipulator kinematics; shafts; ANSYS; band-style lock-unlock mechanism; centralized lock-unlock scheme; clamp-band back; crank-slider mechanism; dynamics analysis; kinematics analysis; single crankshaft; slider-crank mechanisms; space arm; spiral spring; Arm; Clamps; Connectors; Mechatronics; Satellites; Space technology; Space vehicles; Spirals; Springs; Turning; band-style; crank-slider mechanism; dynamics analysis; lock-unlock mechanism;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation, 2007. ICMA 2007. International Conference on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-0828-3
  • Electronic_ISBN
    978-1-4244-0828-3
  • Type

    conf

  • DOI
    10.1109/ICMA.2007.4304133
  • Filename
    4304133