J. Mater. Sci. Technol. ›› 2024, Vol. 174: 249-261.DOI: 10.1016/j.jmst.2023.07.056

• Research Article • Previous Articles    

Simultaneous enhancements of strength and toughness by multiscale lamellar structure in Ti2AlNb based intermetallic

Fan Zhanga,b, Weidong Zenga,b,*, Penghui Zhanga,b, Haoyuan Maa,b, Jianwei Xua,b   

  1. aState Key Laboratory of Solidification Processing, School of Materials Science and Engineering, Northwestern Polytechnical University, Xi'an 710072, China;
    bDefense Technologies Innovation Center of precision forging and ring rolling, School of Materials Science and Engineering, Northwestern Polytechnical University, Xi'an 710072, China
  • Received:2023-06-01 Revised:2023-07-18 Accepted:2023-07-23 Published:2024-03-01 Online:2023-09-09
  • Contact: *State Key Laboratory of Solidification Processing, School of Materials Science and Engineering, Northwestern Polytechnical University, Xi’an 710072, China. E-mail address: zengwd@nwpu.edu.cn (W. Zeng)

Abstract: Multi-scale lamellar structure significantly improves toughness of Ti2AlNb based alloys, which are inherently brittle intermetallics, without compromising their strength. This structure was achieved through-B2-transus-forging (TBTF) combined with O + B2 two-phase region heat treatments. Various types of multi-scale lamellar structures were obtained by controlling the cooling rate after TBTF. These variations were mainly attributed to differences in the distribution, content, and size of the thick lamellar O phase and the size and crystallographic orientation of B2 grain. By analyzing the microstructural characteristics and crystallographic orientation near the crack propagation path, it was found that the crack propagation resistance of thick lamellae, sub grain and grain boundaries (GBs) O phase increased sequentially, accompanied by more tortuous crack propagation path. Moreover, B2 grains with high misorientation significantly deflected the crack propagation by cleavage ridges between adjoining cleavage planes. Additionally, the development of numerous secondary cleavage ridges, resulting from the transition through varying secondary cleavage planes in distinct sub B2 grains, further hindered the quick propagation of cracks. It was clarified that the cleavage planes were dominantly belonging to {110}. These findings provided valuable guidance for the design of damage tolerance strategies for Ti2AlNb-based intermetallics.

Key words: Multiscale lamellae structure, Fracture toughness, Crack propagation, Ti2AlNb-based intermetallic, Through-B2-transus-forging