@inproceedings{10750d08006c410fbeac5a81cc890814,
title = "Analysis of dynamic behavior of zigzag groove setback arming device with two degree of freedom",
abstract = "Focusing on the requirements of safety and reliability of fuze setback arming device of rocket-assisted projectile, a zigzag groove setback device with two degree of freedom was designed with Inventor 6. The dynamic simulation is developed under environment of VisualNastran. The optimum parameters of up inertia-cylinder mass, down inertia-cylinder mass, up inertia-spring rigidity and down inertia-spring rigidity were tested by orthogonal method and simulated. The results indicate that this setback device can effectively differentiate setback overload in launch and impact overload at service handling; credible arming time of fuze is about 128ms when the even overload of the rocket engine is 100g; the optimum mass of up inertia-cylinder and down inertia-cylinder are respectively 3.19g and 1.41g, the optimum rigidity of up inertia-spring and down inertia-spring are respectively 32.7 N/m and 21.8 N/m.",
keywords = "Dynamic simulation, Mathematical model, Orthogonal test, Two degree of freedom system, Zigzag groove",
author = "Guanglin He and Hefei Tian",
year = "2011",
doi = "10.4028/www.scientific.net/AMR.317-319.1739",
language = "English",
isbn = "9783037852163",
series = "Advanced Materials Research",
pages = "1739--1744",
booktitle = "Equipment Manufacturing Technology and Automation",
note = "2011 International Conference on Advanced Design and Manufacturing Engineering, ADME 2011 ; Conference date: 16-09-2011 Through 18-09-2011",
}