2016
DOI: 10.1515/tjj-2015-0004
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Fatigue Life Analysis of Turbine Disks Based on Load Spectra of Aero-engines

Abstract: Load spectra of aero-engines reflect the process of operating aircrafts as well as the changes of parameters of aircrafts. According to flight hours and speed cycle numbers of the aero-engines, the relationship between load spectra and the fatigue life of main components of the aero-engines is obtained. Based on distribution function and a generalized stress-strength interference model, the cumulative fatigue damage of aero-engines is then calculated. After applying the analysis of load spectra and the cumulat… Show more

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Cited by 11 publications
(3 citation statements)
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“…[26][27][28][29][30][31][32][33][34][35][36] In practical engineering applications, since the calculation method of Miner's rule is simple, and the estimated fatigue life error can meet manufacturing demand, it is often used to predict fatigue life. [37][38][39][40][41] With the improvement of the reliability requirements of the mechanical structure, the life prediction error by the Miner's rule has attracted widespread attention. Recently, many researchers have focused on the CCF life prediction model.…”
Section: Introductionmentioning
confidence: 99%
“…[26][27][28][29][30][31][32][33][34][35][36] In practical engineering applications, since the calculation method of Miner's rule is simple, and the estimated fatigue life error can meet manufacturing demand, it is often used to predict fatigue life. [37][38][39][40][41] With the improvement of the reliability requirements of the mechanical structure, the life prediction error by the Miner's rule has attracted widespread attention. Recently, many researchers have focused on the CCF life prediction model.…”
Section: Introductionmentioning
confidence: 99%
“…The damage mechanics theory is a common method to predict fatigue life. [18][19][20] According to the continuous damage mechanics framework, Chen et al 21 introduced the concept of material configuration force as a variable to explain fatigue damage accumulation. At the same time, a damage rate function is proposed on the basis of the configuration force and damage state of the material to predict fatigue life of the material.…”
Section: Introductionmentioning
confidence: 99%
“…Although great advancements have been made in the micro-physical mechanisms of fatigue failure, it is not surprising that such analytical theories are relatively complicated and difficult to implement in engineering. In contrast, phenomenological theories [9][10][11][12][13][14] are still the main approaches for fatigue analysis, where simple fatigue formulas 2 of 17 that can be identified directly from experiments are preferred. In cases of uniform fatigue loading, some phenomenological formulas are representative and constitute the generic fatigue rules available for many different materials, such as Basquin's law (stress-life), Manson-Coffin's law (strain-life), Goodman's law (mean stress correction), and Paris' law (crack propagation rate).…”
Section: Introductionmentioning
confidence: 99%