
Dynamics and reliability analysis of the deployment process of spring folding wing
Author(s) -
Yang Gao,
Ming Hu,
Deming Zhao,
Xingwen Gao,
Jia Chun Lin
Publication year - 2021
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/1043/5/052011
Subject(s) - wing , software deployment , kinematics , structural engineering , computer science , process (computing) , spring (device) , reliability (semiconductor) , engineering , stiffness , simulation , physics , classical mechanics , power (physics) , quantum mechanics , operating system
A “X” type spring folding wing is taken as the research object in this paper, and schematic diagrams of unfolding and locking process are drawn according to its structure and working principle. The theoretical model of kinematics and dynamics which considering the gravity moment is established by simplifying the geometric model of deployment mechanism of the folding wing, so the curve of deployment angle and angular velocity of the outer wing during the deployment process can be obtained. The pulley diameter, preload force and stiffness of the spring-actuated are taken as random variables, and the deployment time and angular velocity are regarded as evaluation indicators. The Monte Carlo method is used to analyse the reliability of deployment process of the folding wing, and the reliability of the deployment process is obtained. The results show that the reliability of the deployment process of the spring folding wing is high.