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
Link To Document :
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