DocumentCode
3438557
Title
Analysis of random vibration life of mechanical parts of actuating cylinder based on the finite element
Author
Si-Xue Qu ; Dan Xu ; Rui Kang
Author_Institution
Sch. of Reliability & Syst. Eng., Beihang Univ., Beijing, China
fYear
2013
fDate
15-18 July 2013
Firstpage
917
Lastpage
920
Abstract
This paper presents a finite element analysis method and three interval method based on Gaussian distribution to study the computing problems of random vibration fatigue life. First, the finite element model is established in ANSYS WORKBENCH software, and through modal analysis, natural frequencies and corresponding vibration modes of the structure are obtained. Then, through the PSD random vibration response analysis, the maximum stress under the condition of flight load random vibration is obtained. The fatigue life under random vibration is estimated by using the three interval method based on Gaussian distribution. Finally, taking the mechanical parts of actuating cylinder as the research object, the method for fatigue life estimation under the random vibration condition is applied and verified.
Keywords
Gaussian distribution; fatigue; finite element analysis; modal analysis; shapes (structures); vibrations; ANSYS WORKBENCH software; Gaussian distribution; PSD random vibration response analysis; actuating cylinder; fatigue life estimation; finite element analysis; flight load random vibration; maximum stress; mechanical parts; modal analysis; natural frequencies; random vibration condition; random vibration fatigue life; random vibration life analysis; three interval method; vibration modes; Broadband communication; Fatigue; Finite element analysis; Load modeling; Pistons; Stress; Vibrations; fatigue life; power spectral density; random vibration; the finite element; three interval method;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-1014-4
Type
conf
DOI
10.1109/QR2MSE.2013.6625717
Filename
6625717
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