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21-Mat-B6 Ceramic Materials · December 2017

Question 6 of 7: High-Speed Tool Steel (T1) — Austenitizing Temperature, Air Quench, and Multiple Tempering

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Reference texts: Krauss, Steels: Processing, Structure, and Performance, 2nd ed.; Reed-Hill & Abbaschian, Physical Metallurgy Principles, 4th ed.; Callister & Rethwisch, Materials Science and Engineering: An Introduction, 10th ed.; ASM Handbook, Vol. 4, Heat Treating; Porter, Easterling & Sherif, Phase Transformations in Metals and Alloys, 3rd ed.

Check: this paper's printed header reads "10-Met-B6, Physical Metallurgy of Iron and Steel," and all seven questions are ferrous physical metallurgy (martensite crystallography and volumetric strain, cast-iron ductility, martensite tempering, TTT-curve theory, austempering of strapping steel, high-speed tool-steel heat treatment, and modern automotive sheet steels) with no ceramics content anywhere.

Question VI: High-Speed Tool Steel (T1) — Austenitizing Temperature, Air Quench, and Multiple Tempering (15 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Check: the Grade T1 table's Ni and Cu entries are not part of the standard published AISI T1 ("18-4-1" tungsten high-speed steel) specification and are disregarded; the reasoning below relies only on the C/Cr/W/V figures.
Given data — T1 tool steel composition as printed (wt%)
GradeCCrNiWVCuMnSP
T10.65–0.803.75–4.000.317.25–18.750.9–1.30.250.1–0.40.030.03

6.1 — (i) Why austenitizing must go as high as 1250 °C

T1 carries very large amounts of strong carbide-forming elements — tungsten and vanadium especially, with chromium contributing as well — which form coarse, extremely thermally stable alloy carbides (M6C-type W-rich carbide, MC-type VC) during solidification and subsequent processing. These carbides have very LOW solubility in austenite at the moderate austenitizing temperatures ($800$–$900^{\circ}\text{C}$) used for plain-carbon or low-alloy steels, and do not dissolve appreciably at such temperatures. To get enough W, Cr, V and C into solid solution in the austenite — essential so that on quenching and tempering they can re-precipitate as the FINE secondary carbides responsible for this steel's characteristic secondary hardening and hot hardness (red hardness) — the steel must be heated close to its incipient-melting temperature, roughly $1250^{\circ}\text{C}$ for T1, where the coarse carbides finally dissolve substantially. Austenitizing too low leaves the alloy content locked up in undissolved primary carbides, starving the matrix of the alloying needed for both adequate hardenability and the secondary-hardening response on tempering.

6.2 — (ii) Why still-air or slow fan cooling is a workable quench

Once the heavy alloy content (W, Cr, V) is taken into solution by the high-temperature austenitizing soak, that SAME dissolved alloy content dramatically depresses the pearlite/bainite "nose" of the steel's TTT/CCT diagram to very long times — exactly the hardenability-shifting mechanism developed in Question IV(ii), here at an extreme level. With the nose pushed out that far, even the comparatively slow, uniform cooling rate available from still air (or a gentle forced-air fan, which mainly improves temperature UNIFORMITY through the section rather than raw cooling speed) is already faster than the now-very-long critical cooling time needed to avoid the nose, so the steel can be taken essentially straight to martensite without ever needing a severe oil or water quench. This is exactly why high-speed and other highly-alloyed tool steels are classed as "air-hardening": a slow, gentle air cool is not merely tolerated, it is the RECOMMENDED practice, because it also minimizes the thermal-gradient-driven distortion and quench-cracking risk that a fast liquid quench would otherwise impose on the complex, often thin-sectioned tool geometries these steels are used for.

6.3 — (iii) Why T1 (and similarly D2) require a minimum of three tempers

As-quenched high-speed steel martensite contains a substantial fraction of RETAINED austenite (not fully martensite), because the heavy alloying that depresses the pearlite nose (6.2) also depresses $M_s$/$M_f$ well below room temperature, so the quench never fully completes the austenite-to-martensite transformation. Each temper cycle serves two compounding purposes at once: (1) it precipitates a dense dispersion of very fine, coherent secondary alloy carbides (the "secondary hardening" reaction, from the same dissolved W/V/Cr — or, for a high-Cr cold-work grade such as D2, predominantly Cr — put into solution during austenitizing) from the primary martensite; and (2) the resulting compositional and volume change, together with the temper's own heating/cooling cycle, converts a substantial fraction of the previously RETAINED austenite into fresh, untempered (and therefore brittle) martensite on cooling back to room temperature. A single temper therefore leaves behind a mixture of properly tempered martensite AND freshly formed, still-untempered martensite from the just-converted retained austenite. A SECOND temper is needed to temper THAT freshly formed martensite; and because even the second temper still converts a further (smaller) increment of any remaining retained austenite into new untempered martensite, a THIRD temper is standard practice to drive the retained-austenite-to-martensite conversion essentially to completion, leaving a stable, fully tempered, minimal-retained-austenite final microstructure. D2, despite deriving its deep hardenability mainly from Cr-rich carbides rather than T1's W/V-rich carbides, shares the identical retained-austenite mechanism (its own heavy alloying likewise depresses $M_s$), which is why the same "minimum of three tempers" rule is quoted for both grades.