摘要
研究了 Ti-47Al-2 W-0 .5 Si合金在 65 0~ 75 0℃区间的蠕变行为和变形机制。结果表明 ,合金 65 0℃蠕变寿命与施加应力之间符合线性的双对数关系 ,可用表达式 lgtf=1 0 lgσ+3 0来描述。蠕变寿命与最小蠕变速率之间满足 Monkman-Grant关系的修正式。合金的比蠕变强度与抗热腐蚀镍基高温合金 K43 8G相当。在70 0℃变载荷下蠕变时具有与恒载荷下蠕变相类似的特征。 80 0℃长期时效粗化合金组织 ,降低蠕变寿命。
Creep behavior and mechanisms of Ti-47Al-2W-0.5Si cast alloy have been investigated. The results show that the creep rupture time at 650°C decreases rapidly with the increase of applied stress, and can be expressed by the formula lgtf=10lgσ+30. The creep rupture time and the minimum creep rate fit a linear double-logarithmic relationship, and can be described with the revision of Monkman-Grant relationship. Its creep strength is comparable to the density-corrected strength of nickel-based corrosion-resistant superalloy K438G. Step-like various load creep has similar deformation characteristics compared with constant-load creep. Long period aging at 800°C coarsens the lamellar structure, and subsequently lowers the creep rupture life. Dislocation gliding and deformation twinning are attributed to the dominant creep mechanisms.
出处
《航空学报》
EI
CAS
CSCD
北大核心
2002年第4期302-306,共5页
Acta Aeronautica et Astronautica Sinica
基金
意大利国家研究委员会 ( CNR)
国际理论物理中心 ( ICTP)