首页> 外文会议>Internaional conference on aluminium alloys >The influence of processing and microstructural parameters on the exfoliation corrosion susceptibility of 2025
【24h】

The influence of processing and microstructural parameters on the exfoliation corrosion susceptibility of 2025

机译:加工和微观结构参数对2025的剥离腐蚀易感性的影响

获取原文
获取外文期刊封面目录资料

摘要

2025 is an established wrought heat-treatable alloy used in aerospace applications that demand good damage tolerance combined with medium strength levels. One such application is fixed and variable pitch propeller blades for turboprop aircraft engines. These propeller blades are normally hot forged from extruded bar and the resulting grain structure exerts a profound influence on the exfoliation corrosion resistance. The avoidance of this damage mechanism is important as propeller blades are normally considered to have infinite lives with respect to fatigue and this necessitates a high quality, stable surface finish on the blade. The present study characterises the microstructural development during hot extrusion and forging of 2025, and attempts to determine the influence of microstructural characteristics on the exfoliation corrosion resistance. Poor exfoliation corrosion resistance in 2025 is associated with the retention of an unrecrystallised hot worked sub-grain structure in the final product. If sufficient plastic deformation is retained prior to solution heat-treatment, a recrystallised structure can result and these structures perform well when subject to standard exfoliation tests like ASTM-G34. However, if recrystallisation produces a coarse grain size the tensile properties are diminished. The effects of three different compositions of 2025 with varying wrought grain refining elements are investigated, when subject to hot extrusion and subsequent forging processes at several temperatures. Optical microscopy methods were used to evaluate the deformation microstructure following the forming processes, with particular attention to the degree of recrystallisation. Exfoliation tests were performed in accordance with ASTM-G34 and mechanical tests were also conducted. The results indicate that the hot forming temperature has a significant influence on the microstructure, and therefore on final exfoliation corrosion resistance and mechanical properties of 2025. In order to better understand the influence of plastic deformation and processing conditions on microstructural development of 2025, the forging process has been modelled using the commercial finite element software ABAQUS and MSC.Patran.
机译:2025是一种在航空航天应用中使用的锻造热处理合金,需求良好的损害耐受性与中等强度水平相结合。一种这样的应用是固定的和用于涡轮螺旋桨飞机发动机的可变音高螺旋桨叶片。这些螺旋桨叶片通常从挤出棒中锻造锻造,并且所得的晶粒结构对剥离耐腐蚀性产生深远的影响。这种损坏机制的避免是重要的,因为螺旋桨叶片通常被认为具有相对于疲劳的无限寿命,这需要在叶片上的高质量,稳定的表面光洁度。本研究表征了2025年热挤出和锻造期间的微观结构发育,并试图确定微观结构特性对剥离耐腐蚀性的影响。 2025年的脱模耐腐蚀性差与最终产品中未结晶的热工作亚颗粒结构的保留相关。如果在溶液热处理之前保留足够的塑性变形,则可以产生重结晶结构,并且当受到ASTM-G34的标准剥离试验时,这些结构表现良好。然而,如果重结晶产生粗粒尺寸,则拉伸性能降低。在几个温度下进行热挤出和随后的锻造过程,研究了三种不同的2025种不同组成与不同的锻造精制元件的影响。光学显微镜方法用于评估成形过程后的变形微观结构,特别注意重结晶程度。根据ASTM-G34进行灭菌试验,也进行机械测试。结果表明,热成形温度对微观结构具有显着影响,因此对2025年的最终剥离耐腐蚀性和机械性能。为了更好地了解塑性变形和加工条件对2025微观结构的影响,锻造使用商业有限元软件ABAQUS和MSC.Patran进行了建模。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号