• DocumentCode
    569245
  • Title

    Research on Simulation Calculation of Kinematic Accuracy Reliability for Folding and Deploying Mechanism Considering Gaps of Kinematic Pair

  • Author

    Ping, Qian ; Wenhua, Chen ; Bingbin, Zhu ; Jun, Pan ; Ming, Hu

  • Author_Institution
    Zhejiang Province Key Lab. of Mech. & Electr. Product Reliability Technol. Res., Zhejiang Sci-Tech Univ., Hangzhou, China
  • fYear
    2012
  • fDate
    July 31 2012-Aug. 2 2012
  • Firstpage
    703
  • Lastpage
    706
  • Abstract
    For evaluation problems of kinematic accuracy reliability for folding and deploying mechanism under the condition of small sample, the continuous contact effective coupling model considering gaps of kinematic pair is built by using "effective length model" theory; Based on the proposed kinematics model of folding and deploying mechanism, simulation calculation method of mechanism kinematic accuracy reliability is proposed by the Monte-Carlo method, kinematic accuracy reliability for folding and deploying mechanism of certain type missile wing is calculated, the attained reliability is 4.87% lower than that under condition of not considering gaps of kinematic pair. The calculation result shows that the reliability obtained by the method proposed in this paper is more closely to the engineering practice.
  • Keywords
    Monte Carlo methods; aerospace components; kinematics; missiles; Monte-Carlo method; continuous contact effective coupling model; deploying mechanism; effective length model theory; folding mechanism; kinematic accuracy reliability calculation; kinematic pair gaps; kinematics model; missile wing; Accuracy; Couplings; Fasteners; Kinematics; Mathematical model; Missiles; Reliability; effective coupling model; folding and deploying mechanism; gaps of kinematic pair; kinematic accuracy; simulation evaluation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Manufacturing and Automation (ICDMA), 2012 Third International Conference on
  • Conference_Location
    GuiLin
  • Print_ISBN
    978-1-4673-2217-1
  • Type

    conf

  • DOI
    10.1109/ICDMA.2012.166
  • Filename
    6298614