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超低间隙TC4钛合金形变热处理工艺

王海 , 魏芬绒 , 崔文俊 , 樊亚军 , 邵晖 , 李雷

材料热处理学报

实验用TC4ELI铸锭,经过开坯、锻造、轧制为φ18 mm的棒材,轧制变形量为91.6%;轧制后进行淬火,淬火温度为830℃,最后对淬火后材料进行温度为650℃、750℃,时间为lh、2h的热处理实验.结果表明:淬火后TC4ELI钛合金的抗拉强度最高,达到1064 MPa,此时材料的屈强比只有0.79.XRD结果表明,淬火后β相发生了马氏体转变,提高了材料的强度;在拉伸过程中,亚稳定的转变组织由于应变引起的转变,使材料均匀伸长率提高,增大了抗拉强度与屈服强度的比值.采用轧制(变形量为91.6%)+淬火(830℃)+650℃×lh的形变热处理工艺后材料的抗拉强度和屈强比分别为1017 MPa和0.94,伸长率为17.5%,综合性能优异.

关键词: TC4钛合金 , 超低间隙 , 形变热处理 , 屈强比

INVESTIGATION ON 1/3[111] FRANK LEDGE DISLOCATIONS AT α_2/γINTERFACE IN HOT-DEFORMED Ti-45Al-10Nb ALLOY

J.G WanG , L.C Zhang , G.L. Chenand HQ. Ye(State Key Laboratory for Advanced Metals and Materials , Unborsity of Science and Technology Beijing , Beijing 100083 , China)(Laboratory of Atond Imaging of Solids , Institute of Metal Research , Chinese Academy of Sciences , Shenyang 110015 , China)

金属学报(英文版)

The dislocation ledges at the α2/7 intedece in a hot-dejormed Ti-45Al-10N alloywere analyzed by high-resolution tmnsmission electron microscopy. A new type ofdislocation ledge containing 1/3[111] Frank partial was found. The height of the ledgestDas always three [111]γplanes. The Burpers vectore of these diBlocation ledges weredetermined to be 1/2[110] and 1/2<101] corresponding to the 90 dey. and 30 deg.Shockley partials at noral ledges, i.e. 90 dep. ShockIey Partial dislocation +1/3[111]Frank partial dislocation; and 30 deg. Shockley partial dislocation + 1/3[111] Frankparfial dislocations. The jormation mechanism of this new tare of dislocation ledgewas discussed.

关键词: titanium aluminide , null , null , null

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