Abstract

Marginal-restraint mandrel-free spinning is an advanced technology for manufacturing ellipsoidal heads with large diameter-thickness ratios. Nevertheless, the spinning-induced residual stress, which greatly influences the in-service performance of spun heads, should be removed. In this study, the effects of annealing on the residual-stress relaxation behavior of 5052H32 aluminum alloy spun heads were investigated. It is found that the residual stress first rapidly decreases and then remains steady with the increase in annealing time at the tested annealing temperatures. The relaxation of the residual stress becomes increasingly obvious with the increase in annealing temperature. When the annealing temperature is less than 220 °C, there are no obvious changes in grain size. Moreover, the spinning-induced dislocations are consumed by the static recovery behavior, which decreases the residual stress during annealing. When the annealing temperature is approximately 300 °C, the broken grains transform into equiaxed grains. In addition, static recrystallization and recovery behaviors occur simultaneously to promote the relaxation of the residual stress. Considering the different stress relaxation mechanisms, a model based on the Zener-Wert-Avrami equation was established to predict the residual-stress relaxation behavior. Finally, the optimized annealing temperature and time were approximately 300 °C and 30 min, respectively.

Highlights

  • With the rapid development of the aerospace industry, large-scale high-performance curved components are increasingly required

  • The spinning-induced dislocations are consumed by the static recovery behavior, which decreases the residual stress during annealing

  • An attempt was made to reduce the residual stress by annealing treatment, and the effects of annealing treatment on the residual-stress relaxation behavior and microstructures of 5052H32 aluminum alloy spun heads were studied in detail

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Summary

Introduction

With the rapid development of the aerospace industry, large-scale high-performance curved components are increasingly required. The Zener-Wert-Avrami model is widely used to describe the residual-stress relaxation behavior of aluminum alloys [30, 31] and other alloys [32, 33] accurately in the heat treatment process. Some research has been conducted on the residual-stress relaxation behavior in alloy components, there have been few efforts to develop residual-stress relaxation strategies of 5052H32 aluminum alloy spun heads. An attempt was made to reduce the residual stress by annealing treatment, and the effects of annealing treatment on the residual-stress relaxation behavior and microstructures of 5052H32 aluminum alloy spun heads were studied in detail. A model was developed to describe the residual-stress relaxation features of the spun ellipsoidal head during the annealing treatment.

Residual-stress measurement
Spun heads and annealing scheme
Effects of annealing parameters on the residual stress
Effects of annealing parameters on the microstructures
Effects of annealing parameters on the dislocation density
Establishment of the residual-stress relaxation model
Verification of the residual-stress relaxation model
Conclusions

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