Abstract

In this work a combination of the characterisation techniques small angle neutron scattering (SANS) and atom probe tomography (APT) are used to study the precipitation in a maraging steel. Three similar maraging steel alloys were aged at different temperatures and ageing times, and then characterised using SANS, APT and microhardness. The alloys consist of two types of precipitates, namely Laves phase and β-NiAl, the precipitates have different composition and hence precipitate ageing, which makes it complicated to model. The SANS experimental set-up was relatively simple and allowed the precipitate size and fraction of a large number of samples to be measured in a single experiment. The APT results were used for constraining the SANS modelling, particularly the composition, shape and distribution of phases. The characterisation led to the following description of precipitation: NiAl phase reaches coarsening at early stages of ageing and shifts its strength mechanisms from shearing to Orowan looping, which cause the characteristic peak strength; the Laves phase is in growth throughout and its strength contribution increases with ageing time. These observations were shown to be consistent with precipitate evolution and strengthening models, and the work of others. Although, there are some issues with the combination of SANS and APT approach, which are discussed, the methodology provides a valuable tool to understand complex precipitation behaviours.

Highlights

  • Maraging steels are a class of steel used within the aerospace sector because of their ultra-high strength, combined with good fatigue and toughness properties [1,2]

  • Two techniques were combined with the small angle neutron scattering (SANS) analysis to understand the precipitation in this alloy: transmission electron microscopy (TEM) and atom probe microscopy (APT)

  • There is considerable overlap of the composition profiles of the two precipitates for different alloy type and ageing times. This observation is the justification for the assumption that the composition of NiAl and Laves phase are constant across all ageing times and alloys studied

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Summary

Introduction

Maraging steels are a class of steel used within the aerospace sector because of their ultra-high strength, combined with good fatigue and toughness properties [1,2] These alloys gain their beneficial properties by a fine dispersion of a nano-scale precipitates, produced after an ageing heat-treatment at an elevated temperature. The issue is further complicated because of the difficulty in quantifying the precipitates present Because of this it is common to take a two-step approach; in the first step the precipitation growth kinetics are modelled to provide information of the precipitate population, and in the second step the strengthening is calculated from the predicted precipitate population. It may be possible to predict the final strength from the heattreatment applied, without the models predicting either the precipitate evolution or the strengthening

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