Title: Modal analysis of flying shear crankshaft system architecture
Authors: Chunming Xu; Qiang Yin; Bowen Luo; Chao Xu
Addresses: Key Laboratory of Metallurgical Equipment and Control Technology, Wuhan University of Science and Technology, Ministry of Education, Wuhan 430081, Hubei, China; Hubei Key Laboratory of Mechanical Transmission and Manufacturing Engineering, Wuhan University of Science and Technology, Ministry of Education, Wuhan 430081, Hubei, China ' Wuhan Polytechnic University, Wuhan 430023, Hubei, China ' Key Laboratory of Metallurgical Equipment and Control Technology, Wuhan University of Science and Technology, Ministry of Education, Wuhan 430081, Hubei, China ' Key Laboratory of Metallurgical Equipment and Control Technology, Wuhan University of Science and Technology, Ministry of Education, Wuhan 430081, Hubei, China
Abstract: When flying shear works, the crankshaft will bear periodic load. If the size of the crankshaft is unreasonable, flying shear will produce strong resonance, which will lead to structural damage of the crankshaft system and flying shear failure. Through the dynamic analysis of the flying shear crankshaft structure, the natural frequency of the crankshaft is obtained, and the stress distribution cloud of the crankshaft under four stages is analysed. Finally, the weak links of the crankshaft are obtained through static analysis, and the solutions are put forward. The research in this paper is of great significance for improving the service life of flying shear crankshaft structure, and provides a basis for further theoretical research.
Keywords: flying shears; crankshaft; modal analysis.
DOI: 10.1504/IJWMC.2019.103118
International Journal of Wireless and Mobile Computing, 2019 Vol.17 No.4, pp.393 - 398
Received: 19 Dec 2018
Accepted: 10 Jul 2019
Published online: 15 Oct 2019 *