An Experimental Study on the Mechanical Performance and Vibration Response of Annealed Inconel 625 Superalloy

Ahmad Al-Qaisia1,2

Safwan Al-Qawabah2, Email

Mike Kh Haddad3

Nabeel Alshabatat4

1Department of Mechanical Engineering, School of Engineering, The University of Jordan, (On Sabbatical Leave), Amman, 11942, Jordan 
2Department of Mechanical Engineering, Al-Zaytoonah University of Jordan, Amman, 11733, Jordan
3Renewable Energy Engineering Department, Faculty of Engineering, Isra University, Amman, 11622, Jordan
4Department of Mechanical Engineering, Faculty of Engineering, Tafila Technical University, Tafila, 66110, Jordan

 

Abstract

Inconel 625, also referred to as 5599 Nickel Superalloy, is a nickel-based superalloy widely used in applications such as jet engine exhaust systems, marine components exposed to seawater, and fasteners or cable connectors. In this study, the effects of the annealing process on the mechanical properties and vibrational behavior of the alloy were investigated both at room temperature and at 950 °C. Comprehensive analyses were performed on Inconel 625, including microhardness measurements, true stress–true strain characterization, vibrational testing, and SEM/EDS examinations. The results revealed a notable 30% increase in hardness and a 50% improvement in toughness after annealing. Furthermore, experimental vibration measurements showed that the annealing process significantly reduced the damping ratio (from 0.0249 to 0.012) by eliminating dislocations and internal stresses that typically act as energy-dissipating mechanisms.

An Experimental Study on the Mechanical Performance and Vibration Response of Annealed Inconel 625 Superalloy