An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system

doi:10.1177/0954410020972898

CORC > 金属研究所 > 中国科学院金属研究所

	An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system
	Zhao, Bingfeng 2,3; Xie, Liyang 2,3; Zhang, Yu 1; Ren, Jungang 2; Bai, Xin 4; Qin, Bo 2
刊名	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
	2020-12-06
页码	19
关键词	Aero-engine rotor blade load-strength interference reliability analysis strength degradation
ISSN号	0954-4100
DOI	10.1177/0954410020972898
通讯作者	Xie, Liyang(lyxie@mail.neu.edu.cn) ; Zhang, Yu(yu.zhang@sjzu.edu.cn)
英文摘要	As the power source of an aircraft, aero-engine tends to meet many rigorous requirements for high thrust-weight ratio and reliability with the continuous improvement of aero-engine performance. In this paper, based on the order statistics and stochastic process theory, an improved dynamic load-strength interference (LSI) model was proposed for the reliability analysis of aero-engine rotor blade system, with strength degradation and catastrophic failure involved. In presented model, the "unconventional active" characteristic of rotor blade system, changeable functioning relationships and system-component configurations, was fully considered, which is necessary for both theoretical analysis and engineering application. In addition, to reduce the computation cost, a simplified form of the improved LSI model was also built for convenience of engineering application. To verify the effectiveness of the improved model, reliability of turbojet 7 engine rotor blade system was calculated by the improved LSI model based on the results of static finite element analysis. Compared with the traditional LSI model, the result showed that there were significant differences between the calculation results of the two models, in which the improved model was more appropriate to the practical condition.
资助项目	National Natural Science Foundation of China[52005087] ; National Natural Science Foundation of China[U1708255] ; National Natural Science Foundation of China[51775355]
WOS研究方向	Engineering
语种	英语
出版者	SAGE PUBLICATIONS LTD
WOS记录号	WOS:000682556700001
资助机构	National Natural Science Foundation of China
内容类型	期刊论文
源URL	[http://ir.imr.ac.cn/handle/321006/159511]
专题	金属研究所_中国科学院金属研究所
通讯作者	Xie, Liyang; Zhang, Yu
作者单位	1.Shenyang Jianzhu Univ, Sch Mech Engn, Shenyang, Peoples R China 2.Northeastern Univ, Sch Mech Engn & Automat, Shenyang, Peoples R China 3.Minist Educ, Key Lab Vibrat & Control Aeroprop Syst, Shenyang, Peoples R China 4.Chinese Acad Sci, Shi Changxu Innovat Ctr Adv Mat, Inst Met Res, Shenyang, Peoples R China
推荐引用方式 GB/T 7714	Zhao, Bingfeng,Xie, Liyang,Zhang, Yu,et al. An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,2020:19.
APA	Zhao, Bingfeng,Xie, Liyang,Zhang, Yu,Ren, Jungang,Bai, Xin,&Qin, Bo.(2020).An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,19.
MLA	Zhao, Bingfeng,et al."An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING (2020):19.