This paper aims at dealing with the deployment vibration problem of the rigid-links deployable mechanism caused by mobility bifurcation. A triangular prismoid deployable mechanism with mobility bifurcation is employed as an example to demonstrate the design and analysis process. First, the mobility of the triangular prismoid deployable mechanism is analyzed, which shows that there exists mobility bifurcation and the possibility of deployment vibration. Second, the revolute joints that introduce mobility bifurcation are analyzed, which shows that they can be replaced by the elastic joints without changing its mobility. Third, a detailed design procedure for this type of elastic joints is discussed; the main parameters of the elastic joints can then be determined based on the mobility and motion range of the deployable mechanism. Physical prototypes of both the rigid-links prismoid deployable mechanism and the corresponding improved mechanism with elastic joints are fabricated, and the deployment experiments of both mechanisms are conducted to show improvement in the latter mechanism.
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Shenzhen 518055,
Harbin 150001,
e-mail: huanghailin@hit.edu.cn
Harbin 150001,
Shenzhen 518052,
Shenzhen 518055,
e-mail: Libing.sgs@hit.edu.cn
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September 2019
Research-Article
Singularity Avoidance for a Deployable Mechanism Using Elastic Joints
Hailin Huang,
Shenzhen 518055,
Harbin 150001,
e-mail: huanghailin@hit.edu.cn
Hailin Huang
1
Harbin Institute of Technology
,Shenzhen 518055,
China
;State Key Laboratory of Robotics and System (HIT)
,Harbin 150001,
China
e-mail: huanghailin@hit.edu.cn
1Corresponding authors.
Search for other works by this author on:
Bing Li
Harbin 150001,
Shenzhen 518052,
Shenzhen 518055,
e-mail: Libing.sgs@hit.edu.cn
Bing Li
1
State Key Laboratory of Robotics and System (HIT)
,Harbin 150001,
China
;Harbin Institute of Technology
,Shenzhen 518052,
China
;Shenzhen Key Lab of Mechanisms and Control in Aerospace
,Shenzhen 518055,
China
e-mail: Libing.sgs@hit.edu.cn
1Corresponding authors.
Search for other works by this author on:
Tieshan Zhang
Hailin Huang
Harbin Institute of Technology
,Shenzhen 518055,
China
;State Key Laboratory of Robotics and System (HIT)
,Harbin 150001,
China
e-mail: huanghailin@hit.edu.cn
Hongwei Guo
Bing Li
State Key Laboratory of Robotics and System (HIT)
,Harbin 150001,
China
;Harbin Institute of Technology
,Shenzhen 518052,
China
;Shenzhen Key Lab of Mechanisms and Control in Aerospace
,Shenzhen 518055,
China
e-mail: Libing.sgs@hit.edu.cn
1Corresponding authors.
Contributed by the Mechanisms and Robotics Committee of ASME for publication in the Journal of Mechanical Design. Manuscript received October 14, 2018; final manuscript received January 9, 2019; published online April 18, 2019. Assoc. Editor: Dar-Zen Chen.
J. Mech. Des. Sep 2019, 141(9): 094501 (5 pages)
Published Online: April 18, 2019
Article history
Received:
October 14, 2018
Revision Received:
January 9, 2019
Accepted:
January 11, 2019
Citation
Zhang, T., Huang, H., Guo, H., and Li, B. (April 18, 2019). "Singularity Avoidance for a Deployable Mechanism Using Elastic Joints." ASME. J. Mech. Des. September 2019; 141(9): 094501. https://doi.org/10.1115/1.4042619
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