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Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (13): 629347-629347.doi: 10.7527/S1000-6893.2023.29347

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Microstructure of γ⁃TiAl and Ti2AlNb linear friction welding joint

Suigeng DU1,2(), Hongyi HU1,3, Ke DING1,2   

  1. 1.Key Laboratory of High Performance Manufacturing for Aero Engine (Ministry of Industry and Information Technology),Northwestern Polytechnical University,Xi’an 710072,China
    2.Engineering Research Center of Advanced Manufacturing Technology for Aero Engine (Ministry of Education),Northwestern Polytechnical University,Xi’an 710072,China
    3.Sanhua R&D Center,Hangzhou 310018,China
  • Received:2023-07-20 Revised:2023-08-14 Accepted:2023-09-07 Online:2024-07-15 Published:2023-11-01
  • Contact: Suigeng DU E-mail:fwcenter@nwpu.edu.cn
  • Supported by:
    National Natural Science Foundation of China(51675434);Science Center for Gas Turbine Project(P2022-A-IV-001-002)

Abstract:

To promote the linear friction welding technology in manufacturing the dissimilar materials blisk of the γ-TiAl blades and Ti2AlNb disc, linear friction welding of γ-TiAl and Ti2AlNb is studied. The microstructure and mechanical properties of the welded joints that are as welded and post weld heat treated were analyzed by SEM, EBSD and tensile testing. The results indicate that the phase composition of the welding zone from the TiAl side to the Ti2AlNb side is γ-α2-B2 as welded and changed into γ-α2+B2-O+B2 after 800 ℃/2 h AC post weld heat treatment. The Thermal and Mechanical Affected Zone (TMAZ) on the γ-TiAl side undergoes laminar bending deformation, while the TMAZ on the Ti2AlNb side undergoes grain refinement and recrystallization. The tensile strength of the joints after post weld heat treatment reaches 277 MPa and 478 MPa at room temperature and 650 ℃, respectively.

Key words: friction welding, TiAl, Ti2AlNb, microstructure, blisk

CLC Number: