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Hot Deformation And Creep Behavior Of Network Ti5Si3/TiAl Composites

Posted on:2018-03-21Degree:MasterType:Thesis
Country:ChinaCandidate:Y SongFull Text:PDF
GTID:2321330536982221Subject:Materials science
Abstract/Summary:PDF Full Text Request
Due to the low density,high specific strength,TiAl alloy can significantly improve thrust-weight ratio.It is expected to be aerospace ideal material of leap-forward development for the future.Applied mostly for high temperature parts,creep property is a key factor for the safe use of the material.The addition of Ti 5Si3 particles is conducive to further enhance the high temperature strength,oxidation resistance and creep resistance.In this paper,network distributed Ti5Si3/TiAl composites with different content?1.2%?3.5%?6.9%?of reinforcement and TiAl material without reinforcement respectively were manufactured by pressure infiltration and hot-pressure sintering in order to perform better creep properties.The hot deformation behavior of composites were investigated to overcome the shortcoming of hot working.OM,SEM,TEM and XRD were utilized to observe and analyze the microstructure of the composites.And determination of density,hardness and tensile p roperties was conducted.The thermal simulation test and creep test of composites were conducted for the study of the thermal deformation and creep behaviors.6.9vol.%Ti5Si3/TiAl composite and 3.5vol.%Ti5Si3/TiAl composite were distributed by double quasi continuous networks,and 1.2vol.%Ti5Si3/TiAl reinforced composite material was distributed along the grain boundary,while pure TiAl material was composed of equiaxial ? phase and lamella microstucture.Along with the increase Ti5Si3,microhardness increased at room temperature.High temperature tensile test indicated that ductile to brittle transition temperature of the composite was between 800830?.3.5vol.%Ti5Si3/TiAl composite performed best yield strength at high temperatures up to 399.2MPa at 800?.And the elongation at 850? was 25.5%.The hot compression deformation results indicated that flow-stress of composites increased as increasing strain rate and as reducing temperature.Compared with 3.5vol.%Ti5Si3/ TiAl composite,6.9vol.%Ti5Si3/TiAl composite performed higher compressive strength at elevated temperature.But 3.5vol.%Ti5Si3/TiAl composite possessed better potential in hot working at lower temperature.Under the condition of 10001200? and 0.0011s-1,Thermal deformation activation of 3.5vol.%Ti5Si3/TiAl composite was 564.67 k J/mol,and corresponding thermal deformation constitutive equation was acquired.Hot working diagram of strain of 0.2?0.3?0.4 and 0.5 showed that the following areas above 1125? and the under strain rate of 0.01s-1 were ideal hot working conditions for 3.5%Ti5Si3/TiAl composite.In addition,Along with the increase of temperature and the decrease of strain rate,it was advantageous to the dynamic recrystallization and grain growth.The existence of the Ti5Si3 particle was helpful to accelerate the rate of dynamic recrystallization,but it would limit grain growth.3.5vol% Ti5Si3/TiAl composite performed the highest creep properties under the same creep test condition.Too much Reinforcing Ti5Si3 would accelerate the decomposition of lamella microstructure to reduce the creep properties of the material.For 3.5vol% Ti5Si3/TiAl material,improving of temperature and load stress would result in increasing of steady creep rate.Stress played a leading role on creep deformation at low temperature,while temperature played a dominant role at high temperature.Under the condition of 700775? and 150225MPa the test creep constitutive equation could be described as e?5?=0.545???2.60exp?-259122/RT?.TEM observation indicated that microscopic deformation structure of 3.5vol.%Ti5Si3/TiAl composite under 750? and 225 MPa was intensive dislocations in ? grain slipping,and creep stress index n value was 2.91.While Under 750? and 250 MPa microscopic deformation structure was {111} deformation twin.It?s main deformation mechanism was accomplishing orientation adjustment by twinning,and creep stress index was 11.17.
Keywords/Search Tags:TiAl matrix composite, Ti5Si3, hot deformation, creep
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