Effect of radial compliance mechanism on rotor system and bearing load for scroll compressor

doi:10.4028/www.scientific.net/AMR.614-615.600

CORC > 兰州理工大学 > 兰州理工大学 > 石油化工学院

	Effect of radial compliance mechanism on rotor system and bearing load for scroll compressor
	Zhao, Man; Li, Chao; Yu, Shurong; Yu, Yang
	2013
会议日期	October 12, 2012 - October 14, 2012
会议地点	Jilin, China
关键词	Bearings (machine parts) Compliant mechanisms Compressors Electrical engineering Loading Mechanisms Scroll compressors Bearing loads Compressor rotors Correlated parameters Eccentric weights Inertia force Mechanical model Mechanism structure Radial compliance Rotor systems Working principles
卷号	614-615
DOI	10.4028/www.scientific.net/AMR.614-615.600
页码	600-603
英文摘要	The imbalance caused by eccentric sleeve radial compliance mechanism rotor system is a main issue in scroll compressor. In this study, the mechanical model of the structure with the eccentric sleeve behind the orbiting scroll is established, the offset level of the main and second balance weight inertia force action line and inertia force action line of the eccentric weight, as well as the effect of this deviation on the second balance and the main and second bearing loads were investigated in terms of working principle, structure and loading. The results show that the structure has great influence on scroll compressor rotor system balance in reducing orbiting radius regulation. It is suggested that the correlated parameters should be optimized in designing radial compliance mechanism structure. © (2013) Trans Tech Publications, Switzerland.
会议录	Advanced Materials Research
会议录出版者	Trans Tech Publications, P.O. Box 1254, Clausthal-Zellerfeld, D-38670, Germany
语种	英语
ISSN号	10226680
内容类型	会议论文
源URL	[http://ir.lut.edu.cn/handle/2XXMBERH/117566]
专题	石油化工学院土木工程学院
作者单位	Lanzhou University of Technology, Lanzhou 730050, China
推荐引用方式 GB/T 7714	Zhao, Man,Li, Chao,Yu, Shurong,et al. Effect of radial compliance mechanism on rotor system and bearing load for scroll compressor[C]. 见:. Jilin, China. October 12, 2012 - October 14, 2012.