Thermal and mechanical effect during rapid heating of astroloy for improving structural integrity

• The behaviour of γ′ phase to thermal and mechanical effects during rapid heating of Astrology
• The thermo-mechanical affected zone (TMAZ) and heat affected zone (HAZ).
• significantly enhanced resistance to weld liquation cracking of the alloy.
• This was not observed in purely thermally simulated samples.
• The microstructure within the TMAZ of the as-welded alloy is similar to the microstructure in the forged Gleeble specimens.

The behaviour of γ′ phase to thermal and mechanical effects during rapid heating of Astroloy(Turbine Disc alloy) a Powder metallurgy (PM) nickel base superalloy has been investigated. The thermo-mechanical affected zone (TMAZ) and heat affected zone (HAZ) microstructure of an inertia friction welded Astroloy were simulated using a Gleeble thermo-mechanical simulation system. Detailed microstructural examination of the simulated TMAZ and HAZ and those present in actual inertial friction welded specimens showed that γ′ particles persisted during rapid heating up to a temperature where the formation of liquid is thermodynamically favoured, and subsequently re-solidified eutectically. The result obtained showed that forging during the thermo-mechanical simulation significantly enhanced resistance to weld liquation cracking of the alloy. This is attributable to strain-induced rapid isothermal dissolution of the constitutional liquation products within 150 μm from the centre of the forged sample. This was not observed in purely thermally simulated samples. The microstructure within the TMAZ of the as-welded alloy is similar to the microstructure in the forged Gleeble specimens.

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