To solve the problem of reliability robust design optimization of structure with implicit limit state functions and limit output performance functions
the robustness of the performance
reliability sensitivity robust and six sigma robust design were integrated
and a reliability robust design optimization model based on response surface method was presented involving the detailed calculation processes of the method.The second-degree polynomials were introduced to simulate the output performance functions and the limit state functions of the structure.The equations of the first order reliability index
the mean value and the standard deviation of the structure were calculated based on the response function.Then taking the structural reliability as the basic constraint condition
the final optimization result with the sequential quadratic programming method was obtained.Finally the example was introduced to explain and validate the model.The method was used to design the model lines of a gas turbine blade.After design optimization
the results indicate that the aerodynamic efficiencies of the guide blade and working blade increase by 1.5% and 6.4% respectively
and the maximum stress and the maximum strain of the working blade decrease by 7.9% and 5.6% respectively.The intensity structural reliability of the working blade increases from 91.3% to 99.9%.
Numerical simulation of LCF probability life of a turbine disk
Experimental Evaluation of High Temperature Low Cycle Fatigue/Creep Life of Turbine Blade
Predicting method of safety life of reusable liquid rocket engine turbopump
Analysis of scrapping characteristics and reliability of civil aero engine high pressure turbine blade in dual failure modes
Optimization design for nozzle contour of rocket engine based on response surface method
Related Author
TANG Jun-xing
LU Shan
WANG Yan-rong
SONG Zhao-hong
HOU Gui-cang
Shijie LIU
Dengfeng LIU
Xiaoqiu MA
Related Institution
School of Engine and Energy, Northwestern Polytechnical University
Beijing University of Aeronautics and Astronautics
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Laboratory of Science and Technology on Cryogenic Liquid Propulsion,Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation