@inproceedings{0c467e86b95d42d09a1171730c58ca7a,
title = "Static strength and durability analysis of the gear-rack for an aircraft slat",
abstract = "Duo to the limitation of the gear-rack's structure profile for an aircraft slat, the maximum stress value got from test is not the value under actual load. In this paper, based on finite element model of gear-rack built by analysis software ABAQUS, the maximum stress value of gear-rack is determined by force analysis. Thus the strength of the gear-rack is checked, and finally the fatigue life is estimated. At the same time, strength test of gear-rack shows that calculation results and test are well consistent. This method can provide a foundation for the design optimization and reliability design of gear-rack for aircraft slat.",
keywords = "ABAQUS, fatigue life, finite element analysis, gear-rack, reliability, strength",
author = "Tuo Zhang and Weimin Cui and Tianxiang Yu and Bifeng Song",
year = "2013",
doi = "10.1109/QR2MSE.2013.6625569",
language = "英语",
isbn = "9781479910144",
series = "QR2MSE 2013 - Proceedings of 2013 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering",
pages = "217--220",
booktitle = "QR2MSE 2013 - Proceedings of 2013 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering",
note = "2013 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering, QR2MSE 2013 ; Conference date: 15-07-2013 Through 18-07-2013",
}