Abstract

Nickel-based superalloys exhibit an exceptional combination of corrosion resistance, enhanced mechanical properties at high temperatures, and thermal stability. The mechanical behavior of nickel-based superalloys depends on the grain size and the precipitation state after aging. Haynes 282 was developed in order to improve the creep behavior, formability, and strain-age cracking of the other commonly used nickel-based superalloys. Nevertheless, taking into account the interest of the industry in the machinability of Haynes 282 because of its great mechanical properties, which is not found in other superalloys like Inconel 718 or Waspaloy, more research on this alloy is necessary. Cutting tools suffer extreme thermomechanical loading because of the high pressure and temperature localized in the cutting zone. The consequence is material adhesion during machining and strong abrasion due to the hard carbides included in the material. The main recommendations for finishing turning in Haynes 282 include the use of carbide tools, low cutting speeds, low depth of pass, and the use of cutting fluids. However, because of the growing interest in sustainable processes and cost reduction, dry machining is considered to be one of the best techniques for material removal. During the machining of Haynes 282, at both the finishing and roughing turning, cemented carbide inserts are most commonly used and are recommended all over the industry. This paper deals with the machining of Haynes 282 by means of coated carbide tools cutting fluids (dry condition). Different cutting speeds and feeds were tested to quantify the cutting forces, quality of surface, wear progression, and end of tool life. Tool life values similar to those obtained with a lubricant under similar conditions in other studies have been obtained for the most favorable conditions in dry environments.

Highlights

  • Turbine components suffer the extreme conditions of thermomechanical loading during their service life

  • The evolution of the cutting forces—cutting force (Fc ), feed force (Ff ), and back force (Fp )—were recorded for each preformed test using a frequency of acquisition of 100 Hz

  • This behavior was not observed for the feed equal to 0.15 mm/rev, whereas the cutting speed was increased from 50 m/min to

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Summary

Introduction

Turbine components suffer the extreme conditions of thermomechanical loading during their service life. The development of new advanced materials and the continuous improvement of the processing routes are required in order to improve the performance of the turbine components [2]. Nickel-based superalloys are widely used in turbine elements because of their excellent mechanical properties at high temperatures and their resistance to corrosion [3]. The excellent mechanical properties of this family of superalloys include low formability, with different problems during component processing that could affect its service life. New-generation alloys are developed in order to solve these problems. Haynes 282 focuses on the improvement of the weldability and fabricability with a similar creep strength. These combinations of properties are of great interest

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