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SIMULATION OF VIBRATION STRESS RELIEF AFTER WELDING BASED ON FEM 被引量:7
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作者 X.C. Zhao Y.D. Zhang +1 位作者 H.W. Zhang Q. Wu 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2008年第4期289-294,共6页
A finite element model is developed for the simulation of vibration stress relief (VSR) after welding. For the nonresonant vibration, the reduction in stress strongly depends on the amplitude of vibration. For the r... A finite element model is developed for the simulation of vibration stress relief (VSR) after welding. For the nonresonant vibration, the reduction in stress strongly depends on the amplitude of vibration. For the resonant vibration, the vibration frequency is the key for stress relief. The vibration frequency should be close to the structure natural frequency for the desired vibration mode. Only small vibration amplitude is required, which will be amplified during vibration. Vibration time does not have a major impact on vibration stress relief. When the amplitude of vibration stress relief is large, the treatment will be more effective. 展开更多
关键词 Residual stress vibration stress relief SIMULATION
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Forced vibration analysis of nano-composite rotating pressurized microbeam reinforced by CNTs based on MCST with temperature-variable material properties 被引量:1
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作者 R.Rostami M.Mohammadimehr +1 位作者 M.Ghannad A.Jalali 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2018年第2期97-108,共12页
In this study, free and forced vibration analysis of nano-composite rotating pressurized microbeam reinforced by carbon nanotubes (CNTs) under magnetic field based on modify couple stress theory (MCST) with temper... In this study, free and forced vibration analysis of nano-composite rotating pressurized microbeam reinforced by carbon nanotubes (CNTs) under magnetic field based on modify couple stress theory (MCST) with temperature-variable material propertiesis presented. Also, the boundary conditions at two ends of nano-composite rotating pressurized microbeam reinforced by CNTs are considered as simply supported. The governing equations are obtained based on the Hamilton's principle and then computed these equations by using Navier's solution. The magnetic field is inserted in the thickness direction of the nano-composite microbeam. The effects of various parameters such as angular velocity, temperature changes, and pressure between of the inside and outside, the magnetic field, material length scale parameter, and volume fraction of nanocomposite microbeam on the natural frequency and response systemare studied. The results show that with increasing volume fraction of nano-composite microbeam, thickness, material length scale parameter, and magnetic fields, the natural frequency increases. The results of this research can be used for optimization of micro-structures and manufacturing sensors, displacement fluid, and drug delivery. 展开更多
关键词 Forced vibration analysis Nano-composite rotating pressurized microbeam Carbon nanotubes Modify couple stress theory Temperature-variable material properties
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Efficient Method for Accelerated Reliability Qualification Testing
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作者 任志乾 于宗乐 +1 位作者 陶俊勇 林武强 《Journal of Donghua University(English Edition)》 EI CAS 2014年第6期882-885,共4页
Based on the theoretical inference and experiment verification,a method was proposed to carry out the accelerated reliability qualification testing. First,theoretical inference was used to get the acceleration coeffic... Based on the theoretical inference and experiment verification,a method was proposed to carry out the accelerated reliability qualification testing. First,theoretical inference was used to get the acceleration coefficients of super Gauss vibration stress and temperature stress. Then, by applying these coefficients, an accelerated reliability qualification testing curve was obtained from the standard tests. Finally,the actual experiment on a digital marine control device was carried out under the proposed testing method.The experiment result shows that the proposed method can reduce the total experiment time and improve the efficiency of the reliability qualification test. 展开更多
关键词 super G auss vibration stress cumulative fatigue damage acceleration testing reliability qualification testing
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Effect of laser shock peening on combined low- and high-cycle fatigue life of casting and forging turbine blades 被引量:4
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作者 Cao Chen Xiao-yong Zhang +3 位作者 Xiao-jun Yan Jun Ren Da-wei Huang Ming-jing Qi 《Journal of Iron and Steel Research International》 SCIE EI CAS CSCD 2018年第1期108-119,共12页
Laser shock peening (LSP) is a novel effective surface treatment method to improve the fatigue performance of turbine blades. To study the effect of LSP on combined low- and high-cycle fatigue (CCF) life of turbin... Laser shock peening (LSP) is a novel effective surface treatment method to improve the fatigue performance of turbine blades. To study the effect of LSP on combined low- and high-cycle fatigue (CCF) life of turbine blades, the CCF tests were conducted at elevated temperatures on two types of full-scale turbine blades, which were made of K403 by casting and GH4133B by forging. Probabilistic analysis was conducted to find out the effect of LSP on fatigue life of those two kinds of blades. The results indicated that LSP extended the CCF life of both casting blades and forging blades obviously, and the effect of LSP on casting blades was more evident; besides, a threshold vibration stress existed for both casting blades and forging blades, and the CCF life tended to be extended by LSP only when the vibration stress was below the threshold vibra- tion stress. Further study of fractography was also conducted, indicating that due to the presence of compressive residual stress and refined grains induced by LSP, the crack initiation sources in LSP blades were obviously less, and the life of LSP blades was also longer; since the compressive residual stress was released by plastic deformation, LSP had no effect or adverse effect on CCF life of blade when the vibration stress of blade was above the threshold vibration stress. 展开更多
关键词 Laser shock peening Combined low-and high-cycle fatigue life (CCF) Full-scale turbine blade S-N curve -Threshold vibration stress
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