Optimization of 75 mm Ultra-Thick Ti-6Al-4V Alloy Plates for Aerospace Applications: Microstructure and Mechanical Properties Analysis

The production of ultra-thick Ti-6Al-4V (Ti-64) alloy plates is critical for aerospace applications, however, meeting the demanding mechanical and microstructural standards presents significant challenges. This study focuses on optimizing the manufacturing process of 75 mm ultra-thick Ti-64 plates to meet the stringent requirements of the AMS4905E specification. Initial attempts revealed that the presence of the primary hcp-α phase, even after β-annealing, severely limited ductility and work-hardening capacity. The mechanical performance, particularly elongation, failed to meet the standard despite achieving adequate yield strength (YS) and ultimate tensile strength (UTS). To overcome these limitations, an optimized process was developed, incorporating a homogenization step prior to hot forging and a globularization step after hot rolling. This approach was aimed at achieving a more uniform microstructure and enhancing the α-to-β phase transformation during heat treatment. Microstructural characterization using optical microscopy (OM), scanning electron microscopy (SEM), and electron backscatter diffraction (EBSD) confirmed the elimination of the primary hcp-α phase, with the formation of a refined and homogenous Widmanstatten structure. These changes resulted in a significant improvement in mechanical properties, particularly elongation, which increased from 4–7.5% in the preliminary trials to 10–11.5%, fully meeting the AMS4905E requirements. In addition to mechanical properties, the size of the prior β grains was carefully controlled to remain within the specified limits of the standard, ensuring full compliance with both microstructural and performance criteria. This optimized process not only enhances the mechanical performance of 75 mm ultra-thick plates but also establishes a reliable foundation for the future production of 100 mm thick Ti-64 plates, which are currently under development. The advancements demonstrated in this study contribute significantly to the field of high-performance titanium alloys for aerospace applications.

Authors

Institutions

Publication Details

Journal
MATERIALS TRANSACTIONS
Published
2025-04-24
DOI
https://doi.org/10.2320/matertrans.mt-mc2024007
Citations
1
Primary Topic
Titanium Alloys Microstructure and Properties
Type
article
Field-Weighted Citation Impact
0.52
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Optimization of 75 mm Ultra-Thick Ti-6Al-4V Alloy Plates for Aerospace Applications: Microstructure and Mechanical Properties Analysis

Mahdi Aghaahmadi, Jeoung Han Kim, Woo Hyeok Kim, Hyun‐Seok Lee et al.
1 citations
MATERIALS TRANSACTIONS
Titanium Alloys Microstructure and Properties
0.52
article

Optimization of 75 mm Ultra-Thick Ti-6Al-4V Alloy Plates for Aerospace Applications: Microstructure and Mechanical Properties Analysis

Mahdi Aghaahmadi, Jeoung Han Kim, Woo Hyeok Kim, Hyun‐Seok Lee, Ji Soo Kim, Mi-Seon Choi
article en
1 citations

Abstract

The production of ultra-thick Ti-6Al-4V (Ti-64) alloy plates is critical for aerospace applications, however, meeting the demanding mechanical and microstructural standards presents significant challenges. This study focuses on optimizing the manufacturing process of 75 mm ultra-thick Ti-64 plates to meet the stringent requirements of the AMS4905E specification. Initial attempts revealed that the presence of the primary hcp-α phase, even after β-annealing, severely limited ductility and work-hardening capacity. The mechanical performance, particularly elongation, failed to meet the standard despite achieving adequate yield strength (YS) and ultimate tensile strength (UTS). To overcome these limitations, an optimized process was developed, incorporating a homogenization step prior to hot forging and a globularization step after hot rolling. This approach was aimed at achieving a more uniform microstructure and enhancing the α-to-β phase transformation during heat treatment. Microstructural characterization using optical microscopy (OM), scanning electron microscopy (SEM), and electron backscatter diffraction (EBSD) confirmed the elimination of the primary hcp-α phase, with the formation of a refined and homogenous Widmanstatten structure. These changes resulted in a significant improvement in mechanical properties, particularly elongation, which increased from 4–7.5% in the preliminary trials to 10–11.5%, fully meeting the AMS4905E requirements. In addition to mechanical properties, the size of the prior β grains was carefully controlled to remain within the specified limits of the standard, ensuring full compliance with both microstructural and performance criteria. This optimized process not only enhances the mechanical performance of 75 mm ultra-thick plates but also establishes a reliable foundation for the future production of 100 mm thick Ti-64 plates, which are currently under development. The advancements demonstrated in this study contribute significantly to the field of high-performance titanium alloys for aerospace applications.

MATERIALS TRANSACTIONSVol. 66(5)
Hanbat National University (KR), Pohang Iron and Steel (South Korea) (KR), Research Institute of Industrial Science and Technology (KR)
Openalex Percentile: Top 39%
Titanium Alloys Microstructure and Properties
0.52
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.