DocumentCode
3439258
Title
Notice of Retraction
Fatigue life analysis of an aero-engine with the measured load spectrum
Author
Wei Cai ; Pingliang Cui ; Ruiyao Yang ; Yuanjian Yang ; Yan-Feng Li ; Hong-Zhong Huang
Author_Institution
Sch. of Mech., Electron., & Ind. Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
fYear
2013
fDate
15-18 July 2013
Firstpage
1074
Lastpage
1076
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
According to the aero-engines´ flight hours and the speed cycle number, we can obtain the relationship between the load spectrum and the life of its main components; According to the analysis of actual measured load spectrum and the fatigue damage model, this paper adopts the S-N curve and Miner´s rule to estimate the fatigue life of engine´s first stage turbine disk.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
According to the aero-engines´ flight hours and the speed cycle number, we can obtain the relationship between the load spectrum and the life of its main components; According to the analysis of actual measured load spectrum and the fatigue damage model, this paper adopts the S-N curve and Miner´s rule to estimate the fatigue life of engine´s first stage turbine disk.
Keywords
aerospace components; aerospace engines; discs (structures); fatigue; fatigue testing; life testing; turbines; Miner rule; S-N curve; aero-engine flight hours; engine first stage turbine disk; fatigue damage model; fatigue life analysis; fatigue life estimation; load spectrum; speed cycle number; Engines; Estimation; Fatigue; Materials; Prediction methods; Stress; Turbines; aero-engine; fatigue; load spectrum; turbine disk;
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.2013.6625751
Filename
6625751
Link To Document