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国家自然科学基金(51205318)

作品数:5 被引量:44H指数:4
相关作者:罗皎李淼泉高峻李慧敏王柯更多>>
相关机构:西北工业大学更多>>
发文基金:国家自然科学基金中央高校基本科研业务费专项资金更多>>
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Quantitative analysis on microstructure evolution of Ti-6Al-2Zr-2Sn-2Mo-1.5Cr-2Nb alloy during isothermal compression被引量:2
2015年
Isothermal compression tests of Ti-6Al-2Zr-2Sn-2Mo-1.5Cr-2Nb alloy were conducted at a Gleeble-1500 simulator in deformation temperature range of 1103–1243K, strain rate range of 0.01–5.00 s-1and height reduction range of 50 %–70 %. The effects of processing parameters on morphology, grain size and contents of a and b phases were discussed based on the quantitative microstructure examination, and the detailed explanation was shown. The results show that b transformed matrix will obviously grow up at higher deformation temperature or lower strain rate because of low grain growth activation energies. The content of a phase will decrease at higher deformation temperature or higher strain rate due to the phase transformation. Some elongated a or b grains exist at higher strain rate, implying that the dominant softening mechanism is dynamic recovery. The effect of height reduction on b transformed matrix is negligible, but the height reduction has some effects on the morphology of primary a phase.
Jun GaoMiao-Quan LiXiao-Di LiDong ZhangJian-Rui XueXue-Qi JiangChao-Yue ZhangLu-Yang Liu
高性能整体叶盘制造技术研究进展被引量:12
2015年
整体叶盘是先进大推力航空发动机的一种新型结构部件,它的应用对于提高发动机性能、简化结构、降低重量、提高可靠性等具有重要的作用。主要介绍了航空发动机整体叶盘的先进制造加工技术,综述了采用精密锻造技术、精密铸造技术、线性摩擦焊接技术、数控铣削加工技术和电解加工技术制造整体叶盘的国内外研究现状与各项技术的优缺点,并展望了我国高性能整体叶盘先进制造技术的发展方向。
罗皎李淼泉
关键词:航空发动机整体叶盘
Microstructure and mechanical properties of heat-treated Ti-5Al-2Sn-2Zr-4Mo-4Cr被引量:7
2015年
The effects of heat treatment parameters on the microstructure,and mechanical properties and fractured morphology of Ti-5Al-2Sn-2Zr-4Mo-4Cr with the equiaxed,bi-modal and Widmanst?tten microstructures were investigated.The heating temperatures for obtaining the equiaxed,bi-modal and Widmanst?tten microstructures were 830,890 and 920 °C,respectively,followed by furnace cooling at a holding time of 30 min.The volume fraction of primary α phase decreased with increasing the heating temperature,which was 45.8% at 830 °C,and decreased to 15.5% at 890 °C,and then the primary α phase disappeared at 920 °C during furnace cooling.The variation of volume fraction of primary α phase in air cooling is similar to that in furnace cooling.The increase in heating temperature and furnace cooling benefited the precipitation and growth of the secondary α phase.The equiaxed microstructure exhibited excellent mechanical properties,in which the ultimate strength,yield strength,elongation and reduction in area were 1035 MPa,1011 MPa,20.8% and 58.7%,respectively.The yield strength and elongation for the bi-modal microstructure were slightly lower than those of the equiaxed microstructure.The Widmanst?tten microstructure exhibited poor ductility and low yield strength,while the ultimate strength reached 1078 MPa.The dimple fractured mechanism for the equiaxed and bi-modal microstructures proved excellent ductility.The coexistence of dimple and intercrystalline fractured mechanisms for the Widmanst?tten microstructure resulted in the poor ductility.
李慧敏李淼泉罗皎王柯
航空发动机双性能盘制造技术与机理的研究进展被引量:17
2012年
具有双重组织的双性能涡轮盘和压气机盘因其优秀的综合性能而成为制造高推重比航空发动机的研究热点。介绍国内外航空发动机用高温合金、钛合金双性能盘的研究进展,对双合金双组织双性能盘和单合金双组织双性能盘进行比较,着重分析两类盘在制造过程存在的主要问题,未来双性能盘的研究重点将落在适合双重热处理的粉末合金和钛合金、双重热处理装置改进、超细晶盘坯和双合金连接弱化方面。
高峻罗皎李淼泉
关键词:航空发动机高温合金钛合金
Deformation behavior and processing maps during isothermal compression of TC21 alloy被引量:6
2017年
In this study,isothermal compression tests were conducted at a Gleeble-1500 simulator at deformation temperatures ranging from 1073 to 1283 K,strain rates ranging from 0.01 to 5.00 s^(-1),and height reductions ranging from 20%to 60%.The flow stress and apparent activation energy for deformation and constitutive equation were used to characterize the deformation behavior of TC21 alloy during the isothermal compression.The processing maps combined microstructure observations were established based on dynamic material model(DMM) over a range of strain rates and temperatures.The results show that an initial yield drop is observed above 1203 K or at higher strain rates ranging from 1.00 to 5.00 s^-1,and oscillatory flow curves are presented particularly at a strain rate of 5.00 s^-1.Strain has some influence on the apparent activation energy for deformation during the isothermal compression of TC21 alloy.The Q-values and microstructure observation confirm that dynamic recrystallization(DRX) occurs in the β single-phase region.The constitutive equation during the isothermal compression of TC21 alloy is developed using the Zener-Hollomon parameter in the exponent-type equation.The maximum and minimum relative errors between the calculated and the experimental flow stress are 14.1%and 0.3%,respectively.The peak efficiency of power dissipation at a strain of 0.7 is about 0.51 occurring at a deformation temperature of 1073 K and strain rate of 0.01 s^-1,corresponding to an optimal deformation condition of TC21 alloy.
Jun GaoMiao-Quan LiGe-Jun LiuShao-Fei Liu
关键词:PROCESSINGMAPS
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