In order to achieve the strength-ductility synergy and improve the work-hardening capacity,Ti64 based composites with dispersive nanoscaled TiB whiskers inside grains were fabricated by plasma rotating electrode proce...In order to achieve the strength-ductility synergy and improve the work-hardening capacity,Ti64 based composites with dispersive nanoscaled TiB whiskers inside grains were fabricated by plasma rotating electrode process coupled with spark plasma sintering.Based on the rapid eutectic reaction,the nanoscaled TiB whiskers exhibited ultra-fine network distribution in composite powders.During the spark plasma sintering process,the network dissolved,and TiB followed the Ostwald ripening mechanism and merged along the(100)plane.The intragranular TiB whiskers could significantly refine the primaryβgrain andαlath.The ultimate tensile strength of the composite with only 2 vol.%TiB whiskers was enhanced to(1123±17)MPa while the elongation was similar to that of the as-sintered Ti64 alloy with approximately 8%.The strength-ductility synergy effect was mainly attributed to the significant grain refinement and the work-hardening ability improvement contributed by intragranular nanoscaled TiB.展开更多
To assess the high-temperature creep properties of titanium matrix composites for aircraft skin,the TA15 alloy,TiB/TA15 and TiB/(TA15−Si)composites with network structure were fabricated using low-energy milling and v...To assess the high-temperature creep properties of titanium matrix composites for aircraft skin,the TA15 alloy,TiB/TA15 and TiB/(TA15−Si)composites with network structure were fabricated using low-energy milling and vacuum hot pressing sintering techniques.The results show that introducing TiB and Si can reduce the steady-state creep rate by an order of magnitude at 600℃ compared to the alloy.However,the beneficial effect of Si can be maintained at 700℃ while the positive effect of TiB gradually diminishes due to the pores near TiB and interface debonding.The creep deformation mechanism of the as-sintered TiB/(TA15−Si)composite is primarily governed by dislocation climbing.The high creep resistance at 600℃ can be mainly attributed to the absence of grain boundaryαphases,load transfer by TiB whisker,and the hindrance of dislocation movement by silicides.The low steady-state creep rate at 700℃ is mainly resulted from the elimination of grain boundaryαphases as well as increased dynamic precipitation of silicides andα_(2).展开更多
基金supported by the National Key R&D Program of China(No.2022YFB3707402)the National Natural Science Foundation of China(Nos.52301189,U22A20113)the Natural Science Foundation of Heilongjiang Province,China(No.LH2023E031).
文摘In order to achieve the strength-ductility synergy and improve the work-hardening capacity,Ti64 based composites with dispersive nanoscaled TiB whiskers inside grains were fabricated by plasma rotating electrode process coupled with spark plasma sintering.Based on the rapid eutectic reaction,the nanoscaled TiB whiskers exhibited ultra-fine network distribution in composite powders.During the spark plasma sintering process,the network dissolved,and TiB followed the Ostwald ripening mechanism and merged along the(100)plane.The intragranular TiB whiskers could significantly refine the primaryβgrain andαlath.The ultimate tensile strength of the composite with only 2 vol.%TiB whiskers was enhanced to(1123±17)MPa while the elongation was similar to that of the as-sintered Ti64 alloy with approximately 8%.The strength-ductility synergy effect was mainly attributed to the significant grain refinement and the work-hardening ability improvement contributed by intragranular nanoscaled TiB.
基金financially supported by the National Key R&D Program of China(No.2022YFB3707405)the National Natural Science Foundation of China(Nos.U22A20113,52171137,52071116)+1 种基金Heilongjiang Provincial Natural Science Foundation,China(No.TD2020E001)Heilongjiang Touyan Team Program,China.
文摘To assess the high-temperature creep properties of titanium matrix composites for aircraft skin,the TA15 alloy,TiB/TA15 and TiB/(TA15−Si)composites with network structure were fabricated using low-energy milling and vacuum hot pressing sintering techniques.The results show that introducing TiB and Si can reduce the steady-state creep rate by an order of magnitude at 600℃ compared to the alloy.However,the beneficial effect of Si can be maintained at 700℃ while the positive effect of TiB gradually diminishes due to the pores near TiB and interface debonding.The creep deformation mechanism of the as-sintered TiB/(TA15−Si)composite is primarily governed by dislocation climbing.The high creep resistance at 600℃ can be mainly attributed to the absence of grain boundaryαphases,load transfer by TiB whisker,and the hindrance of dislocation movement by silicides.The low steady-state creep rate at 700℃ is mainly resulted from the elimination of grain boundaryαphases as well as increased dynamic precipitation of silicides andα_(2).
