Research on the Folding and Deploying Mechanism with Analysis of Frictional Coefficient of Steel and Aerodynamic Resistance

Yao Yao Li; Chun Lan Jiang

doi:10.4028/www.scientific.net/AMR.675.121

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Experimental Study on Turning Vibration Responses of Cutting Tool Surface Based on the Self-Power Spectral Density
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Research on the Folding and Deploying Mechanism with Analysis of Frictional Coefficient of Steel and Aerodynamic Resistance
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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 675Research on the Folding and Deploying Mechanism...

Research on the Folding and Deploying Mechanism with Analysis of Frictional Coefficient of Steel and Aerodynamic Resistance

Abstract:

In this article the folding and deploying mechanism is researched, the equivalent dynamical model is built, and the configuration of the folding and deploying mechanism is designed including the folding mechanism, the deploying mechanism and the locked mechanism. This paper obtains the athletic rule of folding and deploying mechanism, then analyses the dynamic time of the folding and deploying mechanism and the reliability of the locked mechanism, also analyses of frictional coefficient of the steel and aerodynamic resistance of the mechanics.

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Periodical:

Advanced Materials Research (Volume 675)

Pages:

121-124

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.675.121

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Online since:

March 2013

Authors:

Yao Yao Li, Chun Lan Jiang

Keywords:

Deploying Mechanism, Folding Mechanism, Lock Mechanism

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References

[1] A M Law, W D Kelton. Simulation Modeling and Analysis. 3rd. Ed [M]. (2003).

Google Scholar

[2] Garon K D, Faminu O. Aeroballistic range tests of missle configurations with non-circular cross-sections and aeroprediction comparison results [R]. AIAA 2003. 1243.

DOI: 10.2514/6.2003-1243

Google Scholar

[3] WANG Shan, HE Jian. Missile structure Reliability [M]. Harbin: Harbin Engineering University Press, 2002; 236-243.

Google Scholar

[4] LIU Ying-wei, HOU Jun-ping, Reliability analysis for the deploying mechanism of missile wing [J], Hong du Science and Technology, 2001(1): 1-5.

Google Scholar

[5] NI Jian, LU Kai, ZHANG Duo. Movement function reliability of mechanism of deployable folded wings of missile [J]. Aerospace Shanghai, 2001(5): 1-5.

Google Scholar