共查询到18条相似文献,搜索用时 78 毫秒
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采用高速凝固法制备了CMSX-6镍基高温合金定向凝固试样。研究了热处理前后不同部位的显微组织和拉伸性能。结果表明,铸态试样先凝固部分比后凝固部分的枝晶组织更为细密,一次枝晶间距较小,共晶组织含量较少,而抗拉强度高,延伸率较小。热处理后初生相充分固溶形成了成分均一的组织,γ′相得到了明显的细化与均匀化,γ/γ′共晶也发生了溶解并存在固溶微孔。热处理略微提高合金的抗拉强度,但明显提高了合金的延伸率。试样断裂为脆性断裂,铸态为正断型断裂,热处理态为切断型断裂。 相似文献
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时效热处理对镍基单晶高温合金组织的影响 总被引:1,自引:1,他引:1
研究了经不同时效热处理后一种镍基单晶高温合金γ′相的形貌。结果表明:不同的时效热处理制度对所研究镍基单晶高温合金γ′相形貌影响显著。一次时效处理使固溶态γ′相平均尺寸增大;1 080 ℃×6 h一次时效+〖JP〗二次时效处理对γ′相平均尺寸的影响不明显,只加强了γ′相的规则度;1 050 ℃×16 h一次时效+二次时效处理时,γ′相尺寸増长显著。合金经850 ℃×24 h二次时效后,γ′/γ基体通道中均有更细小的二次或三次γ′相析出。 相似文献
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分析了等离子堆焊钴基高温合金Co-02、部分镍代钴基合金Co-04和镍基代钴基合金ND Co-02粉末涂层的金相组织、氧化膜形貌及其能谱、氧化膜断面形貌及其能谱。结果表明:三种合金涂层的金相组织均为白色奥氏体基体加细小Cr7C3、Cr7(C,B)3共晶Co-02生成Cr2O3选择性外氧化保护膜,Co-04和ND Co-02有明显的局部贫Cr区,生成CoCr2O4和NiCr2O4尖晶石结构保护性氧化膜,有效地提高了抗氧化性;三种合金均具有优良的抗氧化性能,且按ND Co-02、Co-04、Co-02顺序依次增强。评定了它们的抗氧化级别。 相似文献
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以新型镍基粉末高温合金FGH4113A(WZ-A3)为研究对象,采用“真空感应熔炼+氩气雾化制粉+热等静压+热挤压+等温锻造”工艺路线制备全尺寸涡轮盘,系统研究了锻造态FGH4113A合金在不同热处理状态下的微观组织和力学性能。结果表明:FGH4113A合金全尺寸涡轮盘宏观形貌良好,微观晶粒组织细小均匀;经亚固溶热处理后,平均晶粒度ASTM 11~13级,室温和550℃的屈服强度分别为1249和1185 MPa,抗拉强度分别为1674和1656 MPa,断后伸长率分别为23.5%和19.5%,在温度700℃,应变范围0~0.8%,加载频率0.33 Hz条件下的疲劳寿命均值为35000周次;经过固溶热处理后,平均晶粒度ASTM 6~8级,700和800℃的屈服强度分别为1063和966 MPa,抗拉强度分别为1403和1112 MPa,断后伸长率分别为17.5%和12.0%,在温度800℃,应力330 MPa,蠕变伸长量0.2%条件下的蠕变寿命均值为384 h,在温度700℃,应力强度因子范围30 MPa·m0.5条件下的裂纹扩展速率小于5×10-4 mm·cycl... 相似文献
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Effect of Cooling Rate on Microstructure and Mechanical Properties of K465 Superalloy 总被引:2,自引:0,他引:2
K465 superalloy, as a material for production of turbine nozzle, shows high mechanical properties as well as microstructure stability in critical and severe service conditions. The alloy gains its appropriate microstructure and strength through solid solution strengthening mechanism. Heat treatment parameters such as: time and temperature of homogenization, partial solution and aging temperatures, and cooling rate from solid solution affect the microstructure of the alloy. Among these parameters cooling rate from solid solution is the most effective. Therefore, in this study the effect of cooling rate on microstructure and mechanical properties (tensile and stress properties) were investigated. For this purpose, three different cooling rates were applied on the cast K465 specimens after solution treatment at 1210℃ for 4 h. Microstructures of the specimens then were studied using optical and electron microscopy. Also, tensile tests were performed at room temperature and stress rupture tests were performed under the condition of 975℃ and 230 MPa. It was found out that with increasing cooling rate the size of the γ' precipitates decreases and the mechanical properties of specimens increases. Also, it was shown that the shape and volume fraction of primary γ' particles are largely influenced by the cooling rate following solution treatment at 1210℃ for 4 h. 相似文献
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热处理对一种Ni3Al基单晶合金组织的影响 总被引:2,自引:0,他引:2
利用光学显微镜和扫描电镜对Ni3Al基单晶合金IC21的铸态组织和不同热处理制度后的组织进行了观察,研究了固溶温度和时效温度对合金热处理组织的影响.研究结果表明,IC21单晶合金的铸态组织由γ’相、γ相以及枝晶间的白色块状析出相组成,枝晶干上γ’相尺寸比枝晶间的γ’相尺寸大.IC21单晶合金的初熔温度约为1345℃,热处理窗口约为65℃.枝晶间γ’相的溶解温度低于枝晶干γ’相的溶解温度.固溶温度越高,时效处理后γ’相的尺寸越均匀.一级时效处理温度对γ’相的尺寸、形态和数量有明显影响.随着一级时效温度的增加,γ’相的体积分数和尺寸增加,形状由类球状向立方状再向长条状转变.1320 ℃/10 h/aac+ 1060℃/2 h/ac +870℃/32 h/ac热处理后可使合金获得γ’相尺寸和分布均匀且立方度高的优良组织. 相似文献
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Microstructure, Properties and Heat Treatment Process of Powder Metallurgy Superalloy FGH95 总被引:7,自引:0,他引:7
Microstructure and properties of nickel based powder metallurgy (PM) superalloy were presented. Effects of nonmetallic inclusions and heat treatment on microstructure and properties were discussed. Development tendency of microstructure and properties of PM superalloy was presented. 相似文献
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采用金相和电镜微观组织观察、室温和高温拉伸试验、物理化学相分析等综合试验方法,对经600、700、800、900℃和100、200、500、1 000 h长期时效处理的GH4199合金进行测试和研究.结果表明,GH4199合金经长期时效后,其室温和高温力学性能仍保持在较高水平;合金的组织稳定性良好,析出相主要为γ'相和碳化物.据相分析结果可知,在700~900℃时效1 000 h左右,合金组织中存在极微量的脆性(TCP)相--μ相和σ相,它们对合金的力学性能基本无影响,组织中虽然存在微量TCP相,但合金的室温和高温塑性不发生"脆化". 相似文献
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采用激光熔化沉积方法制备出Rene95镍基高温合金薄壁样, 分析了沉积态的凝固组织, 并进行了热处理和力学性能测试. 研究表明, 激光熔化沉积Rene95镍基合金的凝固组织为外延生长的定向凝固组织, 其一次枝晶间距在20 μm左右, 二次枝晶臂细小甚至退化, 元素偏析较轻; 通过适当的热处理后, 合金中γ′沉淀相的体积分数明显增加, 合金的显微硬度由沉积态的HV_(0.1) 500提高到HV_(0.1) 540; 经过热处理后, 激光熔化沉积Rene95合金的室温抗拉强度为1247 MPa, 较粉末冶金C级水平略低, 而沿沉积高度方向的延伸率为16.2%, 高于粉末冶金A级水平. 相似文献
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The need for nickel-base powder metallurgy (PM) superalloy turbine discs is becoming increasingly evi dent. With the eventual aim of improving thrust-to-weight ratio of aeroengines for power generation, well integration of significantly high strength, high damage tolerance and high-temperature capability would be reasonably required. An advanced PM superalloy, which was designed for applications up to 815- 8 5 0 ℃, was experimentally investigated. Emphasis was primarily put on microstructure and mechanical properties. The results indicated the measured phases in the sample were composed of γ,γ', MC, and Ma B2. With uniform coarse grain microstruc ture (ASTM 5-6), the sample appeared to exhibit overwhelming superiority over the prior art materials FGH95, FGH96, FGH97 and FGH98. The dominant embodiments consisted of high tensile strength (Rm = 1000 MPa and Rp0.2 800 MPa at 850℃), strong creep resistance (ξp 0.12% at 815 ℃/400 MPa/50 h), and considerable stressrupture life (τ=457.4 h at 815 ℃/450 MPa). The technical practicability of applications up to 815-850 ℃ of this alloy was conclusively proved. 相似文献
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随着液化天然气(LNG)储罐朝着大型化发展,在不增加容器壁厚的情况下,必须提高钢板强度。在传统9Ni钢中添加Cu,通过析出强化,使其强度水平得到显著提高。提出一种新型含1.25%Cu(质量分数)9Ni钢。试验钢经过控轧直接淬火(DQ);研究了DO材料分别经过1)QLT(奥氏体(γ)单相区淬火(Q)+两相区(α+γ)淬火... 相似文献