Based on Bionic Optimization Design and Strength Analysis of The Tie Rod of Aircraft Landing Gear. Issue 1 (March 2020)

• Record Type: Journal Article
• Authors: Tang, M T; Wang, Q; He, G Y; Liu, R P
• Is Part Of: IOP conference series. Volume 816:Issue 1(2020)
• Publication Date: 2020-03
• Subjects: Materials science -- Periodicals; 620.1105
• DOI: 10.1088/1757-899X/816/1/012007
• Languages: English
• ISSNs: 1757-8981

Abstract

Abstract: Based on the three-dimensional model of the cross-type tie rod in the landing gear of an aircraft, the mechanical analysis and solution are carried out, and the stress nephogram as well as the maximum position are obtained. Based on the analysis of bamboo microstructure, two kinds of imitated bamboo tie rod has been designed, one is the imitated bamboo without knots, the other is added knots. The three-dimensional modeling is carried out. The static analysis of finite element is carried out under the same working condition, and the stress nephogram and the position of the maximum value are obtained. The results of two kinds of simulated bamboo tie rod and cross-type tie rod are compared and analyzed. The results show that the mechanical properties of the whole simulated bamboo tie rod are superior to the cross-type tie rod.