Vacuum-furnace brazing of C103 and Ti–6Al–4V with Ti–15Cu–15Ni filler-metal

Hong, In-Ting; Koo, Chun-Hao

doi:10.1016/j.msea.2005.03.007

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The Shear Strength1

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Cited by 27 publications

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“…The hardness of brazed specimens in HRc 35 to 38 corresponded to the hardness of annealed Ti-6Al-4V. The average shear strengths by brazed at 970°C for 15 and 60min then solution and aging treatment were as high as 521 and 427 Mpa, respectively, and increased by 100 MPa, over the value mentioned in reference, in which their samples are without post-brazed treatment [14][15]. It was increased 16% of that compared with post-brazed annealing as described in the reference.…”

Section: The Shear Strengthmentioning

confidence: 74%

Solution Strengthening the Ti-6Al-4V Joints were Brazed by Ti-15Cu-15Ni and Ag-26.7Cu-4.5Ti Filler Foils

Lee

Yang

2020

MSF

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Using the optimal solution and aging treatment for Ti-6Al-4V brazed by Ti-15Cu-15Ni and Ag-26.7Cu-4.5Ti fillers, the average shear strengths of the lap-joint interface are improved. And the average grain sizes and the average lengths of Widmanstätten structure are significantly smaller than that of post-brazed annealing. Both fillers specimens are examined to indicate the strengthening mechanism is to homogenize the microstructure of Ti-6Al-4V joints to simultaneously enhance the strength of joint braze and substrate.

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Section: The Shear Strengthmentioning

confidence: 74%