Journal of System Simulation
Abstract
Abstract: Based on the characteristics of the high-pressure turbine blade, a numerical simulation method for the actual load spectrum of the high-pressure turbine blade of the civil aircraft engine based on the QAR data is proposed. The actual service load spectrum of the engine recorded during aircraft flight is extracted from the QAR data; the time history of centrifugal force, aerodynamic force and thermal stress of the turbine blade in actual use is obtained by means of finite element simulation; and with life prediction model, the actual service life of the blade is estimated. This method provides a reliable engineering method for evaluating the remaining life and obtaining the actual service load of the high-pressure turbine blade, which is valuable for studying the reliability and load characteristics of the high-pressure turbine blade.
Recommended Citation
Jun, Pi; Gao, Shuwei; Huang, Jiangbo; Lei, Huang; and Long, Ma
(2019)
"Fatigue Life Prediction of Turbine Blades Based on QAR Data,"
Journal of System Simulation: Vol. 31:
Iss.
6, Article 17.
DOI: 10.16182/j.issn1004731x.joss.17-0202
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol31/iss6/17
First Page
1165
Revised Date
2017-09-17
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.17-0202
Last Page
1171
CLC
V232.4
Recommended Citation
Pi Jun, Gao Shuwei, Huang Jiangbo, Huang Lei, Ma Long. Fatigue Life Prediction of Turbine Blades Based on QAR Data[J]. Journal of System Simulation, 2019, 31(6): 1165-1171.
DOI
10.16182/j.issn1004731x.joss.17-0202
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