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Evaluation of Ti-48Al-2Cr-2Nb Under Fretting Conditions

机译:微动条件下Ti-48Al-2Cr-2Nb的评价

摘要

The fretting behavior of Ti-48Al-2Cr-2Nb (y-TiAl) in contact with the nickel-base superalloy 718 was examined in air at temperatures from 296 to 823 K (23 to 550 C). The interfacial adhesive bonds between Ti-48Al-2Cr-2Nb and superalloy 718 were generally stronger than the cohesive bonds within Ti-48Al-2Cr-2Nb. The failed Ti-48Al-2Cr-2Nb debris subsequently transferred to the superalloy 718. In reference experiments conducted with Ti-6Al-4V against superalloy 718 under identical fretting conditions, the degree of transfer was greater for Ti-6A1-4V than for Ti-48Al-2Cr-2Nb. Wear of Ti-48Al-2Cr-2Nb generally decreased with increasing fretting frequency. The increasing rate of oxidation at elevated temperatures led to a drop in wear at 473 K. However, fretting wear increased as the temperature was increased from 473 to 823 K. At 723 and 823 K, oxide film disruption generated cracks, loose wear debris, and pits on the Ti-48Al-2Cr-2Nb wear surface. Both increasing slip amplitude and increasing load tended to produce more metallic wear debris, causing severe abrasive wear in the contacting metals.
机译:在空气中,温度为296至823 K(23至550℃)下检查了与镍基高温合金718接触的Ti-48Al-2Cr-2Nb(y-TiAl)的微动行为。 Ti-48Al-2Cr-2Nb和超级合金718之间的界面粘合力通常比Ti-48Al-2Cr-2Nb内部的粘合力强。失效的Ti-48Al-2Cr-2Nb碎屑随后转移到超级合金718。在相同微动条件下针对Ti-6Al-4V对超级合金718进行的参考实验中,Ti-6A1-4V的转移程度大于Ti -48Al-2Cr-2Nb。 Ti-48Al-2Cr-2Nb的磨损通常随着微动频率的增加而降低。高温下氧化速率的增加导致473 K的磨损降低。但是,随着温度从473 K升高至823 K,微动磨损增加。在723和823 K时,氧化膜破裂会产生裂纹,松动的磨损碎屑,并且在Ti-48Al-2Cr-2Nb磨损表面上形成凹坑。增大的滑动幅度和增大的负载都倾向于产生更多的金属磨损碎片,从而在接触的金属中引起严重的磨料磨损。

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