The Design of Bolts Tighting Test System for Launch Vehicle Based on PLC and Servo Motor

Tao Wang; Ming Li Zhang; Yong Kun Chen; Jin Yun Sun

doi:10.4028/www.scientific.net/AMM.631-632.732

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 631-632The Design of Bolts Tighting Test System for...

The Design of Bolts Tighting Test System for Launch Vehicle Based on PLC and Servo Motor

Abstract:

Bolts are widely used in Launch Vehicle. This paper presented a design of bolts tighting test system for launch vehicle based on PLC and Servo Motor. PLC controller and Servo Motor were selected. The stress and displacement of the main load-bearing component was checked by the finite element method (FEM). PID closed-loop control was employed; the influence of PID parameters on the response curve was discussed.

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Periodical:

Applied Mechanics and Materials (Volumes 631-632)

Pages:

732-736

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.631-632.732

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Online since:

September 2014

Authors:

Tao Wang*, Ming Li Zhang, Yong Kun Chen, Jin Yun Sun

Keywords:

Bolts Tighting, Launch Vehicle, PLC, Servo Motor

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* - Corresponding Author

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