Residual Stress Relaxation of Thin-walled Long Stringer Made of Aluminum Alloy 7050-T7451 under Transportation Vibration

Yinfei Yang, Lu Jin, Jixing Du, Liang Li, Wei Yang

Chinese Journal of Mechanical Engineering ›› 2020, Vol. 33 ›› Issue (3) : 39-39.

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Chinese Journal of Mechanical Engineering ›› 2020, Vol. 33 ›› Issue (3) : 39-39. DOI: 10.1186/s10033-020-00456-0
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Residual Stress Relaxation of Thin-walled Long Stringer Made of Aluminum Alloy 7050-T7451 under Transportation Vibration

  • Yinfei Yang1, Lu Jin1, Jixing Du1, Liang Li1, Wei Yang2
作者信息 +

Residual Stress Relaxation of Thin-walled Long Stringer Made of Aluminum Alloy 7050-T7451 under Transportation Vibration

  • Yinfei Yang1, Lu Jin1, Jixing Du1, Liang Li1, Wei Yang2
Author information +
文章历史 +

摘要

Thin-walled long stringer made of aluminum alloy 7050-T7451 is prone to deformation during transportation, so a research of residual stress relaxation was launched in this paper. The transport resonance stress of long stringer was analyzed based on the power spectral density of road transport acceleration. The residual stress relaxation experiment of aluminum alloy 7050-T7451 under different equivalent stress levels was designed and carried out. According to the amount of residual stress relaxation in the experiment, an analytical model was established with the equivalent stress level coefficient. The deflection range of long stringer was evaluated under different damping ratios. The results show that when the equivalent stress exceeds 0.8σ0.2, the residual stress relaxation of the thin-walled samples occurs. The residual stress relaxation increases linearly with the equivalent stress, which is logarithmically related to the loading cycle. The deformation caused by residual stress relaxation of the long stringer is proportional to the square of the length and the bending moment caused by stress rebalance, and inversely proportional to the moment of inertia of the structure. As the damping ratio decreases from 0.03 to 0.01, the total deflection of the long stringer increases from 0 to above 1.55 mm.

Abstract

Thin-walled long stringer made of aluminum alloy 7050-T7451 is prone to deformation during transportation, so a research of residual stress relaxation was launched in this paper. The transport resonance stress of long stringer was analyzed based on the power spectral density of road transport acceleration. The residual stress relaxation experiment of aluminum alloy 7050-T7451 under different equivalent stress levels was designed and carried out. According to the amount of residual stress relaxation in the experiment, an analytical model was established with the equivalent stress level coefficient. The deflection range of long stringer was evaluated under different damping ratios. The results show that when the equivalent stress exceeds 0.8σ0.2, the residual stress relaxation of the thin-walled samples occurs. The residual stress relaxation increases linearly with the equivalent stress, which is logarithmically related to the loading cycle. The deformation caused by residual stress relaxation of the long stringer is proportional to the square of the length and the bending moment caused by stress rebalance, and inversely proportional to the moment of inertia of the structure. As the damping ratio decreases from 0.03 to 0.01, the total deflection of the long stringer increases from 0 to above 1.55 mm.

关键词

Aluminum alloy 7050-T7451 / Large thin-walled part / Transportation process / Residual stress / Structural deformation

Key words

Aluminum alloy 7050-T7451 / Large thin-walled part / Transportation process / Residual stress / Structural deformation

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导出引用
Yinfei Yang, Lu Jin, Jixing Du, Liang Li, Wei Yang. Residual Stress Relaxation of Thin-walled Long Stringer Made of Aluminum Alloy 7050-T7451 under Transportation Vibration[J]. Chinese Journal of Mechanical Engineering, 2020, 33(3): 39-39 https://doi.org/10.1186/s10033-020-00456-0
Yinfei Yang, Lu Jin, Jixing Du, Liang Li, Wei Yang. Residual Stress Relaxation of Thin-walled Long Stringer Made of Aluminum Alloy 7050-T7451 under Transportation Vibration[J]. Chinese Journal of Mechanical Engineering, 2020, 33(3): 39-39 https://doi.org/10.1186/s10033-020-00456-0

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基金

Supported by National Natural Science Foundation of China(Grant No.51405226)
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