首页> 外文会议>International Astronautical Congress >MICROGRAVITY SCIENCES AND PROCESSES SYMPOSIUM (A2) Poster Session (P):AN INVESTIGATION OF THE MICROSTRUCTURE OF SOLIDIFIED TI6AL4V ALLOY AFTER THERMAL PROCESSING UNDER REDUCED GRAVITY CONDITIONS
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MICROGRAVITY SCIENCES AND PROCESSES SYMPOSIUM (A2) Poster Session (P):AN INVESTIGATION OF THE MICROSTRUCTURE OF SOLIDIFIED TI6AL4V ALLOY AFTER THERMAL PROCESSING UNDER REDUCED GRAVITY CONDITIONS

机译:微匍匐科学与过程研讨会(A2)海报(P):在减少重力条件下热处理后凝固Ti6Al4V合金微观结构的研究

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The following research is part of the REXUS/BEXUS programme, which is realised under a bilateral Agency Agreement between the German Aerospace Center (DLR) and the Swedish National Space Board (SNSB). EuroLaunch is a cooperation between the Esrange Space Center of SSC and the Mobile Rocket Base (MORABA) of DLR and it is responsible for the campaign management and operations of the launch vehicles. A sounding rocket scheduled to fly in May 2014 will carry an experimental setup containing a 25 W LASER diode that will be used to melt and weld Ti6A14V samples under reduced gravity conditions. The principal experimental objective is to understand and, thus quantify the role gravity has in the formation of microstructure in a solidifying alloy. For this purpose, two experiments are conducted, one in an Earth-based laboratory under normal gravity conditions and one in the flight environment of the REXUS rocket, where we benefit from a miligravity interval, in which gravity-induced convection effects that affect the stability of the dendritic growth and crystallographic orientation are considerably reduced. Moreover, a control-volume-based Boundary Element Method (Mochnacki Majchrzak; 2007b) was used to simulate the structure formation in an alloy as a result of solidification. Since no convection effects were accounted for in the mathematical model we expect the experimental results from the rocket flight to be a valid test for the accuracy of the numerical method. A Scanning Electron Microscope (SEM) and a Transmission Electron Microscope (TEM) were employed in order to characterize the microstructure of the samples. The expected differences in the geometry of the structure (in terms of uniformity, isotropy of the growth pattern, fineness) are to be then correlated with the changes in the mechanical properties of the Ti alloy that are to be quantified from micro hardness tests, tension tests, bending tests. In conclusion,the current investigation aimed at understanding how Ti alloys transform when thermally processed in the absence of convection is expected to yield important theoretical and experimental results in the field of material science.
机译:以下研究是REXUS / BEXUS计划的一部分,该计划是在德国航空航天中心(DLR)和瑞典国家空间板(SNSB)之间的双边代理协定中实现。 Euroolaunch是SSC的Esrange空间中心与DLR的移动火箭基地(Moraba)之间的合作,它负责发动车辆的竞选管理和运营。安排在2014年5月的探测火箭将携带含有25 W激光二极管的实验设置,该模型将用于在减压条件下熔化和焊接Ti6a14V样品。主要实验目的是理解,因此量化在凝固合金中形成微观结构的角色重力。为此目的,在正常重力条件下,在正常重力条件下进行两次实验,其中一个在Rexus火箭的飞行环境中,我们受益于影响稳定性的重力引起的对流效应树枝状生长和结晶取向显着降低。此外,基于控制体积的边界元法(Mochnacki Majchrzak; 2007b)用于模拟合金的结构形成。结果。由于在数学模型中没有考虑对流效果,我们预计火箭飞行的实验结果是有效的数值方法的准确性。采用扫描电子显微镜(SEM)和透射电子显微镜(TEM)以表征样品的微观结构。结构几何形状的预期差异(在均匀性,生长模式的各向同性,细度,细度)与Ti合金的机械性能的变化相关,这些机械性能从微量硬度测试中量化,张力测试,弯曲测试。总之,目前的调查旨在了解Ti合金在没有对流的情况下热处理时如何变化的旨在产生重要的理论和实验结果,在材料科学领域。

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