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Investigations on the effect of heating temperature and cooling rate on evolution of microstructure in an α + β titanium alloy

Published online by Cambridge University Press:  03 April 2018

Aman Gupta
Affiliation:
Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT), Nagpur-440010, Maharashtra, India
Rajesh Kisni Khatirkar*
Affiliation:
Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT), Nagpur-440010, Maharashtra, India
Amit Kumar
Affiliation:
Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT), Nagpur-440010, Maharashtra, India
Manendra Singh Parihar
Affiliation:
Department of Metallurgical and Materials Engineering, Visvesvaraya National Institute of Technology (VNIT), Nagpur-440010, Maharashtra, India
*
a)Address all correspondence to this author. e-mail: rajesh.khatirkar@gmail.com, rajeshk@mme.vnit.ac.in

Abstract

In the present work, the effect of cooling rate on the evolution of the microstructure and mechanical properties of an α + β titanium alloy has been systematically investigated. Titanium alloy samples were heated to 1066 °C (above the β transus), 930 °C (just below the β transus), and 850 °C (well below the β transus) followed by oil quenching, air cooling, and furnace cooling, respectively. Primary alpha (αp), lamellar alpha (αL), and martensite (α′) were the dominant features of the microstructures for all the samples heated below the β transus. Furnace-cooled samples showed variation in the size and shape of the αp and fraction of αL according to the heating temperature. At slower cooling rates, the thickness of the αL increased with the increase in temperature. Transmission electron microscopy and X-ray diffraction confirmed the presence of α′ in all the quenched samples. The volume fraction and size of the αp decreased with the increase in temperature but was independent of the cooling rate. The microhardness was relatively unaffected by the cooling rate for heating just below the β transus, i.e., 930 °C. The modulus of elasticity was found to be extremely sensitive to the microstructure.

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Article
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Copyright © Materials Research Society 2018 
Figure 0

FIG. 1. (a) Secondary electron SEM image, (b) EBSD PM (black is α matrix and white is β phase), (c) indexed XRD pattern, (d) and (e) BF-TEM image for the as-received sample. SAED pattern of the α phase is also shown in (d).

Figure 1

FIG. 2. EBSD-IPF map for (a) the as-received sample, (b) OQ from 1066 °C, (c) OQ from 930 °C and (d) OQ from 850 °C, (e) OM, secondary electron SEM images and EBSD-IQ map for sample OQ from 1066 °C, (f) EBSD-IQ map for sample OQ from 930 °C, and (g) EBSD-IQ and secondary electron SEM image for sample OQ from 850 °C. The color coding for (a) through (d) is as per the IPF triangle shown in (a).

Figure 2

FIG. 3. BF-TEM images for OQ samples. (a) and (b) quenched from 1066 °C, (c) and (d) quenched from 930 °C, (e) and (f) quenched from 850 °C. SAED pattern in (f) is for cubic β phase.

Figure 3

FIG. 4. Secondary electron SEM image and EBSD-IPF map for (a) 1066 °C AC, (b) 930 °C AC, and (c) 850 °C AC samples, respectively. The color coding for EBSD-IPF maps is as per the IPF triangle shown in Fig. 2(a).

Figure 4

FIG. 5. Secondary electron SEM image and EBSD-IPF map for (a) 1066 °C FC, (b) 930 °C FC, and (c) 850 °C FC samples, respectively. The color coding for EBSD-IPF maps is as per the IPF triangle shown in Fig. 2(a).

Figure 5

FIG. 6. Grain shape aspect ratio map for samples heat treated at 850 °C [(a), (b), and (c)] and 930 °C [(d), (e), and (f)].

Figure 6

FIG. 7. XRD patterns for samples heat treated at (a) 1066 °C, (b) 930 °C, and (c) 850 °C.

Figure 7

TABLE I. Peak broadening [full width at half maximum (°) as determined by XRD peak profile analysis] for different conditions.

Figure 8

FIG. 8. (a) Vickers microhardness, (b) load–depth curve for OQ samples, and (c) load–depth curve for FC samples.

Figure 9

TABLE II. Modulus of elasticity (GPa, determined from load–displacement curves) for different conditions.