ProgramMaster Logo
Conference Tools for MS&T24: Materials Science & Technology
Login
Register as a New User
Help
Submit An Abstract
Propose A Symposium
Presenter/Author Tools
Organizer/Editor Tools
About this Abstract
Meeting MS&T24: Materials Science & Technology
Symposium Composition–Processing–Microstructure-Property Relationships of Titanium Alloys
Presentation Title A Study on High-Temperature Deformation Behavior, Mechanism and Microstructure Evolution of Ti-900 Alloy for Gas Turbine Blade Application
Author(s) Dipayan Chakraborty, Ajay Kumar
On-Site Speaker (Planned) Dipayan Chakraborty
Abstract Scope High-temperature deformation behavior of novel Ti-900 (Ti-6.5Al-3.2Mo-1.8Zr-0.25Si) alloy with equiaxed microstructure is studied by conducting isothermal hot compression tests at 850°C-1050°C temperatures and 0.001s-1 to 10s-1 strain rates. The focus is on establishing a processing map and conducting microstructural analysis. Flow softening is prominent at 10s-1 strain rate with steady-state flow from a strain rate of 0.001s-1 to 1s-1. Optimal efficiency is observed at 900°C and 0.001s-1 and instability at higher strain rates. Air-cooled microstructure remains equiaxed at 850°C and 900°C, changes to bimodal at 950°C and Widmanstätten at higher temperatures. Water quenching after post-compression is also performed. Deformation mechanisms and texture are characterized by EBSD, highlighting DRX of the α phase, which can cause a decrease in LAGBs and an increase in HAGBs, is the main deformation mechanism in the α+β field deformation. QForm simulation software is employed for further investigation, ensuring defect-free manufacturing of gas turbine stator blades.

OTHER PAPERS PLANNED FOR THIS SYMPOSIUM

A Study on High-Temperature Deformation Behavior, Mechanism and Microstructure Evolution of Ti-900 Alloy for Gas Turbine Blade Application
An AM Defect Model for Fast-Acting Probabilistic Prediction of Defects in Laser Powder Bed Fusion and Its Application to Ti-6Al-4V
ATI High Temperature Titanium Alloy Development for Aerospace Applications
ATI Titan 27® : Exploiting c+a Slip to Improve Performance for Aerospace
Cross-Slips in a Near-α Titanium Alloy Made by Additive Manufacturing
Deformation and Fracture at Basal Twist Grain Boundaries In Ti-6Al-4V
Effects of Temperature on the Deformation Behavior and Microstructural Evolution during the Hot Compression Test of Ti-6Al-2V-1Fe-1Cr Alloy
Experimental Investigations on Thermomechanical Fatigue Behavior in Near Alpha Titanium Alloy
Heterogeneous Nano-Mechanical Response of Bimodal Ti-6Al-4V Alloy
Influence of Zr and O on the Evolution of Microstructural Features in High γ-Phase Ti-Al-Zr Alloys
Investigating Cold Dwell Fatigue Failure in Dual-Phase Ti Alloys: The Perspective of Hard-Soft Grain Interactions
Laser Shock Processing of Titanium Alloys: Microstructure Evolution and Enhanced Engineering Performance
Metastable and Stress-Induced Transformations in Additively Processed Ti-10V-2Fe-3Al
Microstructure, Mechanical, and Electrochemical Properties of Additively Manufactured Ti-5Al-5V-5Mo-3Cr (wt.%)
Novel Ti-Ta-Zr-Mo Alloys Utilizing Martensite-Driven TRIP/TWIP Mechanisms for Cardiovascular Stent Applications
Study of Microstructure of Titanium Alloys and Its Relation to Mechanical Properties of Alloys for Aerospace Industry
Surface Engineering Ti Alloys and Stress Impacts on Recrystallization
Tailoring Strength and Toughness of a New Titanium Alloy, ATI Titan 23™
Titanium Boron Nitride Nanotubes (Ti-BNNT) Metal Matrix Composite Processed by SPS: Microstructure, Mechanical and Tribological Characteristics
Tuning Alpha Microstructures in Beta Titanium Alloys

Questions about ProgramMaster? Contact programming@programmaster.org