High Temperature Properties of Discontinuously Reinforced Titanium Matrix Composites: A Review

doi:10.1007/s40195-014-0155-y

摘要/Abstract

Abstract:

Further improvement on high temperature durability is one of the most important aims except for high specific strength, high specific stiffness, and excellent wear resistance, to design and fabricate discontinuously reinforced titanium matrix composites (DRTMCs). Their superior properties render them extensive application potential in aerospace and military industries due to the urgent demand for the materials with characteristics of lightweight, high strength, high stiffness and high temperature durability. With development on fabrication methods and room temperature properties, testing, characterizing, evaluating and further increasing high temperature properties of DRTMCs are becoming more and more important to promote their applications. This review provides insights and comprehensions on the high temperature tensile properties, superplastic tensile properties, creep behaviors, and high temperature oxidation behaviors of DRTMCs, and research proposals to further improve the high temperature properties of DRTMCs are given.

Key words: Titanium matrix composites, High temperature tensile properties, Creep behaviors, Oxidation behaviors, Superplasticity

. [J]. 金属学报英文版, 2014, 27(5): 787-797.

Geng Lin, Huang Lujun. High Temperature Properties of Discontinuously Reinforced Titanium Matrix Composites: A Review[J]. Acta Metallurgica Sinica (English Letters), 2014, 27(5): 787-797.

图/表 10

Fig. 1 Tensile properties of (TiB + TiC + La2O3)/Ti composites at high temperatures: a fracture strains; b tensile strengths [31]

Fig. 2 Tensile stress-strain curves a, tensile properties b of TiBw/Ti composites in the range of room temperature to 900°C [33]

Fig. 3 SEM images showing the longitudinal sections near the fracture surfaces of the TiBw/Ti composite sheet tested at 600°C a; 900°C b [33]

Fig. 4 Comparison of high temperature tensile strength between TiBw/Ti6Al4V composites with network microstructure and the monolithic Ti6Al4V alloy [9]

Fig. 5 Creep data compensation of DRTMCs with threshold stresses: a low stress region; b high stress region [53]

Fig. 6 Arrhenius plots of the logarithmic creep rates versus the reciprocal Kelvin temperature for the matrix alloy and DRTMCs at effective constant stresses [53]

Fig. 7 Cross-sectional microstructure of 6.3 vol% TiBw/Ti6Al composites formed after oxidation for 50 h at 750°C a; 800°C b [55]

Fig. 8 SEM images of TiC in TiC/Ti composites a; TiC b; Nd2O3 c in (TiC + TiB + Nd2O3)/Ti composites after oxidation [58]

Fig. 9 SEM micrographs of oxidation surfaces at 700°C for 100 h a, schematic illustration showing anti-oxidation mechanism of TiCp/Ti6Al4V composites with a network microstructure b [25]

Fig. 10 Mass gain-time relationship of monolithic Ti60 alloy, 1.7 vol% TiBw/Ti60 and 5.1 vol% TiBw/Ti60 composites at different temperatures: a 600°C; b 700°C; c 800°C; d 900°C [59]

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