简介:采用B50A789材料制备的压气机叶片产生的缺陷,主要是由于原材料内部夹杂、局部偏析、组织粗大,带状偏析和折叠引起的.本研究采用金相和能谱分析方法研究了锻造压气机叶片表面裂纹的形成机理,并对其锻造裂纹的形成过程进行有限元模拟.结果表明结合低倍及高倍形貌特征,可以得出叶片缺陷为锻造加工过程产生的折叠裂纹;通过有限元模拟分析认为锻造叶片表面裂纹是源于锻件在制坯过程中,在连接杆与安装圆盘的转接处形成啃伤台阶,导致终锻结束时在叶身形成折叠裂纹缺陷.同时通过对试验过程中锻造工艺调整,采用分料卡子对过渡区分料或进行打磨来保证转角半径圆滑过渡,可有效避免叶片表面折叠和裂纹缺陷的形成.
简介:Inthiswork,transformationbehaviorsandmechanicalpropertiesofcold-rolledshapememoryalloyTi50Ni49Fe1bysevereplasticdeformation(SPD)wereintensivelyinvestigated.Thephasetransformationbehaviors,phaseanalysis,andmicrostructureswerecharacterizedbydifferentialscanningcalorimetry(DSC),X-raydiffraction(XRD),andtransmissionelectronmicroscopy(TEM),respectively.TensiletestingwasperformedtoanalyzetheeffectofSPDonthemechanicalpropertiesandshapememoryofTi50Ni49Fe1alloy.Whenthethicknessreductionisbeyond30%,themartensitictransformationissuppressed.Aftercold-rolling,thealloyismainlycomposedofB2parentphaseswithsomestress-inducedmartensiticB190phases,andhighdensityofdislocationsaregeneratedandthegrainsareobviouslyrefined.Theyieldstressrbsignificantlyraisesfrom618MPaof0%coldrollingto1,338MPaof50%SPD.Shape-memoryeffectincreasesfrom6.5%withoutcoldrollingto8.5%after30%SPD,ascribedtotheinduceddefectsincoldrolling.ThoseresultsindicatethatTi50Ni49Fe1alloyhasimprovedmechanicalpropertiesandpotentialcommercialapplicationsafterSPD.
简介:ThemicrostructuresandcrystallizationbehaviorofTi–47at%Ni–3at%Feshapememoryalloywireundertheconditionofseverecolddrawingatroomtemperatureanddifferentpost-deformationannealingprocesseswereintensivelyinvestigatedusingtransmissionelectronmicroscope(TEM)anddifferentialscanningcalorimetry(DSC).ItisindicatedthattheamorphousphaseisdominantintheTi50Ni47Fe3wireafterthecolddrawingof78%arealreduction.Thecriticaltemperatureforrecrystalizationisdeterminedatabout300°C.Theaveragegrainsizegrowsfrom7upto125nmwhenannealingtemperaturerisesfrom300to500°C.Post-deformationannealingprocessexertssignificantinfluenceonthecrystallizationtemperaturewhichclimbsupwiththeincreaseofannealingtemperature.
简介:基于热分析结果,对AM50-4%(Zn,Y)(Zn/Y摩尔比为6:1)合金设计并实施一种两步递进固溶处理。利用OM、XRD、SEM/EDS、TEM、拉伸实验和硬度实验研究固溶与时效处理对AM50-4%(Zn,Y)合金组织与力学性能的影响。结果表明:与一步固溶处理相比,两步递进固溶处理能够使Φ和β相充分溶解于基体,获得更高的溶质过饱和度,从而一定程度上增强合金在后续时效处理中的弥散强化效果。在180℃进行时效处理时,Φ相析出对合金综合力学性能的影响要大于β相。经两步递进固溶处理(345℃,16h+375℃,6h)的AM50.4%(Zn,Y)合金在时效处理(180℃,12h)后获得峰时效强度。
简介:采用SEM、TEM、EDS、DSC、XRD和拉伸实验研究铸态7X50合金及其均匀化处理过程的组织演变。结果表明,铸态7X50合金相组成主要有S(Al2CuMg)、T(Al2Mg3Zn3)、MgZn2和少量的Al7Cu2Fe和Al3Zr相。均匀化处理过程中枝晶网和残留相逐渐减少,经(470°C,24h)+(482°C,12h)均匀化处理时,T相消失,S相有微量残留,Al7Cu2Fe相几乎没有变化。铸态合金的DSC曲线中在477.8°C处有一较强吸热峰,经470°C、1h均匀化后合金的DSC曲线在487.5°C处出现一个新的吸热峰,而经482°C、24h均匀化处理后合金在487.5°C处的吸热峰基本消失。在XRD谱中未出现T(Al2Mg3Zn3)相,这和T相与S(Al2CuMg)及MgZn2相相关的结论相吻合。预均匀化处理制备的板材中再结晶晶粒分数明显降低,抗拉强度和断裂韧性相对常规均匀化处理制备的板材分别提高约15MPa和3.3MPa·m1/2。