Abstract

In recent years, superheavy forgings that are manufactured from 600 t grade ingots have been applied in the latest generation of nuclear power plants to provide good safety. However, component production is pushing the limits of the current free-forging industry. Large initial grain sizes and a low strain rate are the main factors that contribute to the deformation of superheavy forgings during forging. In this study, 18Mn18Cr0.6N steel with a coarse grain structure was selected as a model material. Hot compression and hot tension tests were conducted at a strain rate of 10−4·s−1. The essential nucleation mechanism of the dynamic recrystallization involved low-angle grain boundary formation and subgrain rotation, which was independent of the original high-angle grain boundary bulging and the presence of twins. Twins were formed during the growth of dynamic recrystallization grains. The grain refinement was not obvious at 1150°C. A lowering of the deformation temperature to 1050°C resulted in a fine grain structure; however, the stress increased significantly. Crack-propagation paths included high-angle grain boundaries, twin boundaries, and the insides of grains, in that order. For superheavy forging, the ingot should have a larger height and a smaller diameter.

Highlights

  • In recent years, a large number of superheavy forgings have been manufactured and applied in the construction of the latest generation of nuclear power plants, as nozzle shells, the upper head of reactor pressure vessels, and monoblock lowpressure rotors [1]

  • In the 0.2 reduction specimen (Figure 1(a)), the high-angle grain boundaries (HAGBs) were serrated with some lowangle grain boundaries (LAGBs) appearing nearby

  • Some segments of the twin boundaries (TBs) changed into common HAGBs

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Summary

Introduction

A large number of superheavy forgings have been manufactured and applied in the construction of the latest generation of nuclear power plants, as nozzle shells, the upper head of reactor pressure vessels, and monoblock lowpressure rotors [1]. In the past, these components were manufactured by welding together small forged parts. E largest available ingots, that is, 600-ton grade ingots, are required to manufacture superheavy forgings [3]. The microstructure evolution and surface cracking behavior of superheavy forgings have not been investigated widely. e dynamic recrystallization (DRX) and cracking mechanisms have yet to be elucidated

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