Structure-Property Correlation in Additively Manufactured High-Temperature Materials: Insights from Nickel-Based Superalloy IN718 & Nickel-Based Eutectic High Entropy Alloy AlCoCrFeNi2.1

By: Contributor(s): Material type: TextTextLanguage: en. Publication details: Bangalore IISc 2023Description: 271p. col. ill. ; 29.1 cm * 20.5 cm e-Thesis 11.04MbSubject(s): DDC classification:
  • 620 RAJ
Online resources: Dissertation note: PhD; 2023; Materials engineering Summary: High-temperature alloys are technically very important materials that possess higher resistance toward mechanical and chemical degradation at 0.4-0.6 TM for a constant/cyclic load. These attributes make them candidate materials for aerospace and energy generation systems that require harsh operating conditions. The most popularly used high-temperature alloys are the Nickel-base superalloys, and among various Ni-base alloys, Inconel 718 (IN 718) is the most used material. The currently used superalloys are already exploited to very high operating temperatures near their solidus or the precipitate solvus temperatures. Any further increase in Carnot efficiency is only possible through design improvements and enhanced turbine cooling efficiency, which the Additive Manufacturing (AM) technique can address. However, the adoption of AM processes for aerospace/mission-critical components is impeded due to microstructural heterogeneities and spontaneous defects observed in AM-produced parts. It is, therefore, necessary to develop processes that head to minimum porosity and design suitable heat treatments, and to evaluate the relevant mechanical properties post-heat treatment.
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Call number Status Date due Barcode
E-BOOKS E-BOOKS JRD Tata Memorial Library Available ET00130

Include bibliographical references and index

PhD; 2023; Materials engineering

High-temperature alloys are technically very important materials that possess higher resistance toward mechanical and chemical degradation at 0.4-0.6 TM for a constant/cyclic load. These attributes make them candidate materials for aerospace and energy generation systems that require harsh operating conditions. The most popularly used high-temperature alloys are the Nickel-base superalloys, and among various Ni-base alloys, Inconel 718 (IN 718) is the most used material. The currently used superalloys are already exploited to very high operating temperatures near their solidus or the precipitate solvus temperatures. Any further increase in Carnot efficiency is only possible through design improvements and enhanced turbine cooling efficiency, which the Additive Manufacturing (AM) technique can address. However, the adoption of AM processes for aerospace/mission-critical components is impeded due to microstructural heterogeneities and spontaneous defects observed in AM-produced parts. It is, therefore, necessary to develop processes that head to minimum porosity and design suitable heat treatments, and to evaluate the relevant mechanical properties post-heat treatment.

There are no comments on this title.

to post a comment.

                                                                                                                                                                                                    Facebook    Twitter

                             Copyright © 2024. J.R.D. Tata Memorial Library, Indian Institute of Science, Bengaluru - 560012

                             Contact   Phone: +91 80 2293 2832