Simulation of Dual Microstructure Heat Treatment Process and Residual Stresses in Gas Turbine Disc by DeformHT Software
Keywords:
Turbine disc, grain size, microstructure, induction heat treatment, Deform softwareAbstract
Gas turbine disc is one of the most vital components in advanced gas engine. In order to improve the tensile strength and fatigue strength of the disc, finer grain size is to be attained at bore area and coarser grain structure at rim area in order to resist the growth of creep. Attempts have been made by several researchers experimentally on the development of dual microstructure for Inconel-718 by heat treatment technique. However, the simulation of induction and resistance heat treatment process to achieve dual grain size and reduce residual stresses is not yet reported. In the present work, an attempt is made to obtain the optimal induction heat treatment process parameters to achieve the dual grain structure at bore area and estimate the residual stresses to predict the disc performance. The induction heat treatment process is simulated using DEFORMHT software to achieve dual grain size of 5.6 μm at bore area and 46.3 μm at rim area of the disc. The rim area of the disc was heated to 1080ºC with varying input power from 10 to 30 kW at frequency 20 kHz. The disc was soaked for 60 min at a constant temperature of 1080ºC and then cooled at a rate of 1ºC/min to room temperature. The disc with induced residual stresses was further subjected to heating at 700, 800 and 900ºC. Reduction in residual stresses was finally achieved by soaking the disc at three intervals (3600, 7200, and 1800 s). Grain size achieved after and before resistance heat treatment was measured by obtaining state variable method in DEFORMHT software).
Downloads
Published
Issue
Section
License
Declaration and Copyright Transfer Form
(to be completed by authors)
I/ We, the undersigned author(s) of the submitted manuscript, hereby declare, that the above manuscript which is submitted for publication in the STM Journals(s), is not published already in part or whole (except in the form of abstract) in any journal or magazine for private or public circulation, and, is not under consideration of publication elsewhere.
- I/We will not withdraw the manuscript after 1 week of submission as I have read the Author Guidelines and will adhere to the guidelines.
- I/We Author(s ) have niether given nor will give this manuscript elsewhere for publishing after submitting in STM Journal(s).
- I/ We have read the original version of the manuscript and am/ are responsible for the thought contents embodied in it. The work dealt in the manuscript is my/ our own, and my/ our individual contribution to this work is significant enough to qualify for authorship.
- I/We also agree to the authorship of the article in the following order:
Author’s name
1. ________________
2. ________________
3. ________________
4. ________________
| We Author(s) tick this box and would request you to consider it as our signature as we agree to the terms of this Copyright Notice, which will apply to this submission if and when it is published by this journal. |