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Strategic Study of CAE >> 2001, Volume 3, Issue 5

The Near β Forging Overthrows the Conventional Forging Theory and Develops a New Tri-modal Microstructure

Northwestern Polytechnical University, Xi'an 710072, China

Received: 2001-02-10 Available online: 2001-05-20

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Abstract

The near beta forging for titanium alloys proposed by the authors has overthrown the conventional forging theory in the following two aspects: firstly, the material is heated and forged at 10〜15℃ below beta transus temperature and then water cooled; secondly, the heat treatment technology after forging consists of a high-temperature toughening treatment and a low-temperature strengthening treatment instead of the conventional aging treatment. Because of ingenious combination of phase transformation, defomation and strengthening and toughening theory, materials forged by the near beta forging do not produce an equiaxed microstructure or a basketweave microstructure as usually found in conventionally forged titanium alloy, but do produce a new trimodal microstructure, which consists of about 20% equiaxed alpha, 50%~60% basketweave formed by striature alpha and transformed beta matrix. The trimodal microstructure not only develops a new type of microstructure in addition to the existing four titanium alloy microstructures (i.e. equiaxed, bi-modal, basketweave and lamella), but also has the advantages that both the equiaxed microstructure and the basketweave microstructure have, so it shows excellent mechanical properties. It shows an increased high-temperature property, a high low-cycle fatigue property and a high fracture toughness without decreasing ductility and thermal stability. Moreover, it can raise the service temperature from 500℃ to 550℃ . The near beta forging is applicable not only to alpha-beta alloy, but also to alpha, near alpha and near beta titanium alloys. This method has been used to forge several engine compressor disks and some important structure components of missils and airplanes

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References

[ 1 ] OkadaM .In :FroesFH , CaplanILeds., Titaniumscienceandtechnology , SanDiego , California , TMS1992 , 15 5 1

[ 2 ] CroanLS , RizzitanaFJ .WALreport 40 1/ 2 6 8, watertownArsendLaboratories, Mass, 195 8

[ 3 ] 周义刚 .金属学报 , 1980 , 16 (3) :30 2 link1

[ 4 ] SheegarevAS , GlyaooevAP .Researchonhigh strengthalloysandrefinedgrain , Moscow , AcademyofSciencePress , 196 3, 142

[ 5 ] FentmanWP , GooseyRE .In :JaffeeRI, PromiselNEeds., Thesciencetechnologyandapplicationoftitani um , London :PergamonPress, 1970 .987

[ 6 ] MinomiM , KobayashiT .ISIJInt, 1991, 31:488

[ 7 ] 周义刚 , 曾卫东 , 曹春晓等 .金属学报 , 1999, 35 (1) :45 link1

[ 8 ] 王金友 , 葛志明 航空用钛合金 , 上海 :上海科学技术出版社 , 1985 .2 2 1 link1

[ 9 ] HenningHJ.DMICReportS 2 4, DefenseMetalsIn formationCenter , BottelleMemorialInstitute , 196 8

[10] B .K .亚力山大 .钛合金半成品 [M], 宁龙兴译 宝鸡有色金属研究所出版 , 1984.38

[11] ZhouYG , ZengWD , YuHQ .Materialsscienceandengineering , 1996 , A2 2 1:5 9

[12] TobinA .AD A0 0 742 7, 1975

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