GH4169合金摩擦焊规范与成形性能

以高性能航空发动机蜗轮盘和压气机盘为背景,应用能量方法对GH4169合金管状模拟试件的惯性摩擦焊接过程进行了分析与计算,推导出了焊接热力影响区主要热参数的理论计算公式。经编程计算,给出了摩擦焊接区域温度和飞边分流半径的拟合曲线,并分析研究了飞边缺陷的种类及其产生的原因。内缺陷以分流半径为参考,该处存在速度奇异点,不良的工艺规范,会导致裂纹缺陷。中间缺陷以分离半径为参考,该处存在较大的应力集中,从而容易产生裂纹缺陷。外缺陷以飞边半径为参考,当温度较低的飞边外缘处拉应力值达到某一临界值后,就会在翘起的外飞边上产生裂纹缺陷。基于本文方法,可以合理地制定出惯性摩擦焊接规范,从而为提高GH4169合金的成形性能和接头质量创造条件。     

GH4169高温合金惯性摩擦焊的有限元模拟

基于Ansys有限元分析软件,建立了GH4169高温合金惯性摩擦焊过程的二维模型,进行了热力耦合分析,得到了焊接过程中的瞬时温度场和应力应变场,获得了焊接缩短量。根据惯性摩擦焊工艺分析了温度场和应力应变场的形成过程。     

GH4169合金大型环形件的惯性摩擦焊接

介绍了获得了与母材等强度和塑性甚至稍高些接头的惯性摩擦焊方法,并用该方法成功地焊接了GH4169合金的大型环形件。     

GH4169高温合金惯性摩擦焊接接头的蠕变性能

研究了GH4169高温合金惯性摩擦焊接头的高温蠕变和持久性能,在595℃条件下,随着应力的增大,接头和母材在达到同一稳态蠕变速率ε时,接头承受的蠕变应力略小于母材;在断裂前,相对于母材,接头能承受更大的稳态蠕变速率.在650℃,承受较大应力水平时,GH4169惯性摩擦焊接头持久强度稍弱于母材,但差别很小;较低应力水平时,接头的持久强度则显著大于母材.     

GH4169合金与FGH96合金惯性摩擦焊接头组织和力学性能

在主轴转速为650 r/min、转动惯量为340 kg·m2、焊接压力为450 MPa焊接参数下,实现GH4169与FGH96异质材料惯性摩擦焊接,并对焊后热处理的接头进行显微组织与力学性能分析.在焊接热-力耦合作用下,焊接接头不同区域的金相组织发生变化,晶粒出现不同程度的细化、变形,基体强化相出现不同程度的溶解、变形.焊接接头显微硬度呈山峰状分布特征,焊接接头室温抗拉强度平均值为1 366 MPa,高温抗拉强度平均值为1 176.7 MPa,在650℃,641 MPa条件下的平均持久寿命为215 h,焊接接头具有良好的综合力学性能.     

GH4169合金惯性摩擦焊接头温度场显式有限元数值模拟

借助ABAQUS/Explicit显式有限元模拟软件,采用热力耦合方法,建立了GH4169高温合金管状工件三维弹塑性有限元大变形计算模型.考虑了计算设置中质量放大因子(mass scaling)对飞轮转动惯量的影响,确定了放大因子与转动惯量缩小倍数之间的相互关系.在此基础上对整个焊接过程工件的温度场进行了综合分析.结果...     

GH4169高温合金惯性摩擦焊的有限元模拟

基于Ansys有限元分析软件，建立了GH4169高温合金惯性摩擦焊过程的二维模型，进行了热力耦合分析，得到了焊接过程中的瞬时温度场和应力应变场，获得了焊接缩短量。根据惯性摩擦焊工艺分析了温度场和应力应变场的形成过程。     

GH4169惯性摩擦焊接过程动态再结晶组织演化的数值模拟

利用MSC.Marc的热力耦合弹塑性有限元模拟技术,建立了GH4169环形件惯性摩擦焊接过程的二维热力耦合有限元模型。考虑到惯性摩擦焊接过程中的温度变化,采用叠加原理对Na Y S建立的GH4169动态再结晶数学模型进行调整。借助MSC.Marc二次开发,将动态再结晶数学模型和有限元模型相结合,对惯性摩擦焊接过程中GH4169合金的动态再结晶组织演化进行数值模拟,得到了焊接过程中的动态再结晶分数和平均晶粒尺寸分布。对接头的宏观形貌和焊缝区的微观组织进行观察分析,发现模拟结果与实验结果吻合较好。     

转速对FGH96/GH4169高温合金惯性摩擦焊接头组织与力学性能的影响

应用惯性摩擦焊机完成了FGH96/GH4169高温合金焊接,采用光学显微镜、扫描电镜以及拉伸试验机等设备观察并测试了焊接接头的微观组织形貌、显微硬度及拉伸性能。结果表明接头存在FGH96侧母材、热力影响区、焊缝区、GH4169侧热力影响区及母材五个区域,焊缝区组织为细小的等轴晶粒,晶粒尺寸远小于母材,热力影响区则发生了拉伸变形。接头近界面处最高温度达到1 100 ℃以上,超过γ′等强化相的固溶温度。焊后热力影响区处强化相部分重溶,在界面细晶区强化相几乎完全重溶。随着转速增大,焊缝区晶粒增大,典型原子的扩散距离增加,接头室温抗拉强度和高温抗拉强度值升高。     

GH4169合金与S31042钢线性摩擦焊接头组织及力学性能

使用25 Hz振动频率、2 mm振幅、100 MPa摩擦压力和150 MPa顶锻压力的工艺参数对GH4169合金和S31042钢进行线性摩擦焊连接,通过OM、SEM和TEM分析异质接头的组织特征,并进行拉伸、硬度和蠕变实验测试异质接头在室温和高温环境下的力学性能。结果表明,GH4169合金与S31042钢的连接界面在线性摩擦焊过程中发生动态再结晶,形成无孔无裂纹的冶金结合,同时焊缝区在高温和应力作用下形成大量弥散分布的强化相颗粒。通过细晶强化和析出强化的综合作用,异质接头的抗拉强度高于S31042钢,焊缝区的硬度明显高于2种母材。     

Microstructure and properties of modified and conventional 718 alloys

Continuing the effort to redesign IN718 alloy in order to provide microstructural and mechanical stability beyond 650 ℃, IN718 alloy was modified by increasing the Al, P and 13 contents, and the microstructure and mechanical properties of the modified alloy were compared with those of the conventional alloy by SEM and TEM. The precipitation of the grain boundaries of the two alloys is different. The Cr-rich phase, Laves phase and α-Cr phase are easily observed in the modified alloy. The γ＂ and γ＇ phases in the modified alloy are precipitated in a ＂compact form＂. The tensile strengths of the modified alloy at room temperature and 680 ℃ are obviously higher than those of the conventional one. The impact energy of the modified alloy is only about half of that of the conventional alloy. Ageing at 680 ℃ up to 1000 h lowers the tensile properties and impact energy of both the conventional and modified 718 alloys, except increasing the ductility at 680 ℃. It is concluded that the modified alloy is more stable than the conventional one.     

Effects of Thermally Assisted Warm Laser Shock Processing on the Microstructure and Fatigue Property of IN718 Superalloy

The effects of laser shock processing (LSP) and warm laser shock processing (WLSP) on the microstructure of surface hardening layer and high-cycle fatigue performance at room temperature and high temperature (600 ℃) of IN718 alloy were investigated.It has been revealed that the grain refined hardening layer with greater residual compression stresses,higher fraction of coincidence site lattice (CSL) boundaries and dislocation densities was formed in WLSP-treated alloy than in LSP-treated alloys.Moreover,microtwins included γ" phase/high density dislocation complex was found in the surface of WLSP-treated alloy.These characters caused the significant enhancement of the medium value fatigue strength of WLSP-treated alloy at room temperature and elevated temperature.Apparently,the microtwins included y" phase/high density dislocation complex formed in the surface hardening layer of LSP-treated alloy has more complicated steric structure and more stable at elevated temperature than γ" phase/low density dislocation complex formed in LSP-treated alloy,leading to the slow recovery process.Therefore,the surface hardening layer in the WLSP-treated alloy remained more ideal strengthen-ing effect under high-cycle fatigue at elevated temperature than that in LSP-treated alloy.This resulted in the much longer fatigue crack initiation incubation and longer high-cycle life of WLSP-treated IN718 alloy under cycling load at 600 ℃.This discovery provides a new cognition of fatigue resistance by WLSP treatment of precipitation strengthening superalloy.     

等温锻造对IN718合金组织和性能的影响

对IN718合金在1020℃下以应变速率0．01进行变形量为40％的等温锻造．并对锻造过程进行数值模拟，预测了涡轮盘件锻造载荷的情况。试验结果表明：经等温锻造后IN718合金具有细晶组织，晶粒度为ASTM10级．其力学性能高于指标要求。通过数值模拟等温锻过程并与试验结果对比可以看出：数值模拟等温锻造过程中变形量与成形件几何尺寸、设备载荷以及材料损伤情况的模拟与试验情况吻合     

MICROSTRUCTURE AND MECHANICAL PROPERTIES OF NOVEL 718 SUPERALLOY

Recently, a novel 718 superalloy with remarkable structural stability at 680℃ has been designed and fabricated by CISRI (Central Iron and Steel Research Institute) etc. Phase identification of novel 718 alloy under the above-mentioned heat-treatment condition was performed using optical microscopy (OM), scanning electron microscopy (SEM), and transmission electron microscopy (TEM). Results show that the novel 718 alloy has outstanding structural stability at 680℃. The novel 718 alloy possess excellent structural stability and good mechanical properties, which is attributed to ?酌'-phase strengthening and also to the specific sandwich structure of the ?酌' ＋ ?酌' strengthening phase.     

In718合金高温锻造数值模拟与试验研究

利用MSC．SuperForm有限元分析软件对In718合金镦粗过程进行三维数值模拟和试验研究．分析了不同温度、摩擦和变形速率条件下等效应力-应变分布和载荷曲线。通过热模拟试验研究了In718合金不同条件下的真应力-应变曲线和微观组织。结果表明：镦粗变形分为三个变形区域，摩擦增加了变形的不均匀性和塑性变形抗力：高温锻造过程中，In718合金在基体边界上发生了动态再结晶，再结晶晶粒细小，动态再结晶进行程度随着工艺条件的不同而不同；In718合金比较合适的锻造温度为1010-1040℃之间，变形速率为0．05～0．5s^-1之间,最大变形程度可以达到70％以上。     

TC4合金线性摩擦焊摩擦时间与变形量的关系

用自制的XMH-160型线性摩擦焊机，试验研究了TC4钛合金线性摩擦焊的摩擦时间对摩擦变形量的影响，结果表明，其变形量随摩擦时间的增加近似呈指数关系增大。分析了出现非线性摩擦变形量的原因，以及线性摩擦焊飞边形貌的一些基本特点。     

摩擦搅拌焊6061-T6铝合金焊接接头的组织与性能

采用搅拌摩擦焊对6mm厚度的6061-T6铝合金进行单道平板对接焊,研究了焊接接头的力学性能和组织.结果表明,转速较小时,焊接接头会出现明显的搅拌摩擦焊接特有的“螺旋体”断口,其接头性能不高;随着转速的提高,接头性能得到改善.X射线衍射分析结果表明,焊缝组织中由于搅拌温度而引起部分强化相的重溶.透射电镜的研究结果表明,焊缝中的主要增强相依然为β”.     

Friction welding of TiAI intermetallics and structural steel by applying Inconel 718 as interlayer

Inconel 718 with thickness ranged from 0. 1 - 1.7 mm was chosen as interlayer to promote weldability in friction welding of TiAl intermetallics and structural steel such as AIS14140, in which the welded joint presents single fin showing less welding deformation on TiAl side. The correlations between tensile strength and the interlayer thickness were analyzed and fitted to a model. It indicates an optimum interlayer thickness ranged from 0.9 - 1.1 mm where the tensile strength reaches as high as 360 MPa. Otherwise, while the interlayer thickness decreases to 0. 1 mm, brittle compounds of TiC, Al2Ti4C2 and MTC3 are formed in the welded zone so that the tensile strength decays. Thicker interlayer should be also avoided as double joints may occur at TiAl -lnconel 718 and lnconel 718 -AISI 4140, respectively, which lowers the tensile strength to some extent.