High-Temperature Properties of TC11-(TiB + TiC) Titanium Matrix Composites Fabricated by Hot Isostatic Pressing

To meet the demand for lightweight, high-strength, and high-temperature-resistant structural materials in aerospace applications, TC11-(TiB + TiC) composites with varying B4C contents (0, 2 and 5 wt.%) were fabricated by hot isostatic pressing (HIP), and their microstructures and high-temperature mechanical properties were systematically investigated. Results reveal that in situ TiB whiskers and TiC particles were obtained in all the composites, and the matrix microstructure changed non-monotonically with the B4C content. A fine and uniform basketweave microstructure was obtained at 2 wt.% B4C, whereas at 5 wt.% the reinforcements formed a quasi-continuous network along the prior particle boundaries, and pores developed at the grain boundaries owing to B4C agglomeration and incomplete local reaction. At room temperature, the yield strength rose from 1020 MPa to 1586 MPa with increasing B4C, but the fracture strain dropped from about 37% to 11%. At 650 °C, however, the base alloy softened severely, its peak stress falling from 1998 MPa to 484 MPa. The composites, by contrast, were strengthened, with the peak stresses of TMC2 and TMC5 reaching 603 and 841 MPa, exceeding the base alloy by 24.6% and 73.8%, respectively. This reversal can be attributed to a change in the role of the reinforcements. At room temperature, the reinforcements act primarily as stress-concentration sites. At elevated temperatures, however, they function as a rigid load-bearing skeleton. Load transfer through this skeleton, together with the relaxation of interfacial stresses by matrix plasticity, accounts for the monotonic increase in high-temperature strength with increasing reinforcement content. The moderate CTE mismatch between the reinforcements and the matrix may provide a secondary contribution, as suggested by the increasing apparent microstrain from XRD and the stacking faults within TiB observed by HRTEM. In addition, the B27 crystal structure of TiB, its [010] growth habit, and the well-bonded symbiotic TiB/TiC interfaces may further impede dislocation motion at elevated temperature.

Authors

Institutions

Publication Details

Journal
Materials
Published
2026-10-27
DOI
https://doi.org/10.3390/ma19214519
Primary Topic
Titanium Alloys Microstructure and Properties
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

High-Temperature Properties of TC11-(TiB + TiC) Titanium Matrix Composites Fabricated by Hot Isostatic Pressing

Zhengfei Zhou, Zhongyang Mao, Yuyang Han, Yangyang Sun
3 links
Materials
Titanium Alloys Microstructure and Properties
article

High-Temperature Properties of TC11-(TiB + TiC) Titanium Matrix Composites Fabricated by Hot Isostatic Pressing

Zhengfei Zhou, Zhongyang Mao, Yuyang Han, Yangyang Sun
article en

Abstract

To meet the demand for lightweight, high-strength, and high-temperature-resistant structural materials in aerospace applications, TC11-(TiB + TiC) composites with varying B4C contents (0, 2 and 5 wt.%) were fabricated by hot isostatic pressing (HIP), and their microstructures and high-temperature mechanical properties were systematically investigated. Results reveal that in situ TiB whiskers and TiC particles were obtained in all the composites, and the matrix microstructure changed non-monotonically with the B4C content. A fine and uniform basketweave microstructure was obtained at 2 wt.% B4C, whereas at 5 wt.% the reinforcements formed a quasi-continuous network along the prior particle boundaries, and pores developed at the grain boundaries owing to B4C agglomeration and incomplete local reaction. At room temperature, the yield strength rose from 1020 MPa to 1586 MPa with increasing B4C, but the fracture strain dropped from about 37% to 11%. At 650 °C, however, the base alloy softened severely, its peak stress falling from 1998 MPa to 484 MPa. The composites, by contrast, were strengthened, with the peak stresses of TMC2 and TMC5 reaching 603 and 841 MPa, exceeding the base alloy by 24.6% and 73.8%, respectively. This reversal can be attributed to a change in the role of the reinforcements. At room temperature, the reinforcements act primarily as stress-concentration sites. At elevated temperatures, however, they function as a rigid load-bearing skeleton. Load transfer through this skeleton, together with the relaxation of interfacial stresses by matrix plasticity, accounts for the monotonic increase in high-temperature strength with increasing reinforcement content. The moderate CTE mismatch between the reinforcements and the matrix may provide a secondary contribution, as suggested by the increasing apparent microstrain from XRD and the stacking faults within TiB observed by HRTEM. In addition, the B27 crystal structure of TiB, its [010] growth habit, and the well-bonded symbiotic TiB/TiC interfaces may further impede dislocation motion at elevated temperature.

MaterialsVol. 19(21)
Nanjing Tech University (CN), Nantong University (CN), Nantong Science and Technology Bureau (CN), Nantong Institute of Technology (CN)
Openalex Percentile: Top 29%
Titanium Alloys Microstructure and Properties
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.

Laika access coming soon