Abstract

Considering the constant technological developments in the aeronautical, space, automotive, shipbuilding, nuclear and petrochemical fields, among others, the use of materials with high strength mechanical capabilities at high temperatures has been increasingly used. Among the materials that meet the mechanical strength and corrosion properties at temperatures around 815 °C one can find the nickel base alloy Pyromet® 31V (SAE HEV8). This alloy is commonly applied in the manufacturing of high power diesel engines exhaust valves where it is required high resistance to sulphide, corrosion and good resistance to creep. However, due to its high mechanical strength and low thermal conductivity its machinability is made difficult, creating major challenges in the analysis of the best combinations among machining parameters and cutting tools to be used. Its low thermal conductivity results in a concentration of heat at high temperatures in the interfaces of workpiece-tool and tool-chip, consequently accelerating the tools wearing and increasing production costs. This work aimed to study the machinability, using the carbide coated and uncoated tools, of the hot-rolled Pyromet® 31V alloy with hardness between 41.5 and 42.5 HRC. The nickel base alloy used consists essentially of the following components: 56.5% Ni, 22.5% Cr, 2,2% Ti, 0,04% C, 1,2% Al, 0.85% Nb and the rest of iron. Through the turning of this alloy we able to analyze the working mechanisms of wear on tools and evaluate the roughness provided on the cutting parameters used. The tests were performed on a CNC lathe machine using the coated carbide tool TNMG 160408-23 Class 1005 (ISO S15) and uncoated tools TNMG 160408-23 Class H13A (ISO S15). Cutting fluid was used so abundantly and cutting speeds were fixed in 75 and 90 m/min. to feed rates that ranged from 0.12, 0.15, 0.18 and 0.21 mm/rev. and cutting depth of 0.8mm. The results of the comparison between uncoated tools and coated ones presented a machined length of just 30% to the first in relation to the performance of the second. The coated tools has obtained its best result for both 75 and 90 m/min. with feed rate of 0.15 mm/rev. unlike the uncoated tool which obtained its better results to 0.12 mm/rev.

Highlights

  • IntroductionIndustries that manufacture components for engines with nickel alloys and special stainless steel (automotive valves), titanium alloys (aviation turbine) are characterized by presenting a high cost in the manufacture of machined parts, mainly in relation to cost time/machine

  • Industries that manufacture components for engines with nickel alloys and special stainless steel, titanium alloys are characterized by presenting a high cost in the manufacture of machined parts, mainly in relation to cost time/machine

  • The notching was predominant in the machining of Pyromet® 31V when using the coated tools and flank wear in uncoated tools

Read more

Summary

Introduction

Industries that manufacture components for engines with nickel alloys and special stainless steel (automotive valves), titanium alloys (aviation turbine) are characterized by presenting a high cost in the manufacture of machined parts, mainly in relation to cost time/machine. Nickel base alloys constitute ~45–50% of the total material required in the manufacture of an aircraft engine due to their outstanding strength and oxidation resistance at elevated temperatures in excess of 550°C (Gossler, 1985 and Simms, 1972). The nickel base alloys, as well as in austenitic stainless steel, harden it self when worked quickly. High pressure during machining produces an effect of hardening which may cause distortions in parts with small thicknesses, compromising the integrity and tolerance of the machined components

Objectives
Methods
Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call