t和應(yīng)力比R下Ti-5Al-5Mo-5V-1Cr-1Fe (Ti-55511)鍛件和棒材縱向的室溫高周疲勞性能及斷口形貌。結(jié)果表明:應(yīng)力比和應(yīng)力集中系數(shù)是影響疲勞性能的兩個(gè)重要因素。鍛件和棒材的疲勞強(qiáng)度均隨應(yīng)力比R的增大而增大,隨應(yīng)力集中系數(shù)Kt的增大而減小。鍛件的疲勞性能優(yōu)于棒材,并且鍛件的疲勞強(qiáng)度是棒材的1.08~1.57倍。"/>
1.西安建筑科技大學(xué)冶金工程學(xué)院;2.航空工業(yè)第一飛機(jī)設(shè)計(jì)研究院
陜西省自然科學(xué)基金(2016KW-054)
1.School of Metallurgical Engineering,Xi’an University of Architecture Technology,Xi’an;2.AVIC the First Aircraft Institute,Xi’an
Natural Science Foundation of Shaanxi Province (2016KW-054)
劉瑩瑩,張樂,史曉楠,薛希豪,楊健. Ti–5Al–5Mo–5V–1Cr–1Fe合金高周疲勞性能及斷裂行為的研究[J].稀有金屬材料與工程,2018,47(12):3666~3671.[Yingying Liu, Le Zhang, Xiaonan Shi, Xihao Xue, Jian Yang. Study on the High Cycle Fatigue Properties and Fracture Behavior of Ti–5Al–5Mo–5V–1Cr–1Fe Titanium Alloy[J]. Rare Metal Materials and Engineering,2018,47(12):3666~3671.]
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