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

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.

[1]  J. Lu,et al.  DSP-based thermal protection for brushless servo motor , 1992 .

[2]  Sheng-Hui Wang,et al.  Compressive residual stress introduced by shot peening , 1998 .

[3]  J. Koenderink Q… , 2014, Les noms officiels des communes de Wallonie, de Bruxelles-Capitale et de la communaute germanophone.

[4]  J. O. Vanvleet D-1A nose fairing separation fitting load test , 1976 .

[5]  J. Michael Pereira,et al.  Ballistics Analysis of Orion Crew Module Separation Bolt Cover , 2013 .