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Investigation of Creep Feed Grinding Parameters and Heat treatment Effects on the Nickel-base Superalloys

机译:氯进料研磨参数的研究和镍基超合金的热处理效果

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The Nickel base Superalloys are the most famous complicated and useable of Superalloys to make hot zone components of the gas turbines. The complicated dimensional tolerances, specially at the root of the blade show importance of grinding processes at the production of blades root. The prediction of the effect of machining parameters on the soundness of component surface strengthening for reaching to a suitable surface finishing and avoiding from crack formation at the work part during machining operation often is not easy and feasible so needs to more industrial investigation. This research is about frame 5 blade designed by GE and made from Superalloy IN738LC has been investigated. The formation of a plastically deformed and heat affected zone during grinding of Superalloy IN738LC with a high depth of cut but slow work speed (creep feed grinding) was investigated. Parameters such as work speed, depth of cut and radial dressing speed have been considered as variables and their effects have been studied. During experimental performed, the voltage and current of motor measured and power and special energy calculated. Some samples heat-treated (of the 1176 deg C for 1 hr under neutral argon gas and cooling rate of 15 deg C /min up to 537 deg C and then air cooling) to study grains recrystallization. Other samples have been created from the roots of blades and then coated by Nickel to measure boundary layer micro-hardness. The results show that increasing work speed leads to increasing the use power. Increasing the depth of cut, by increasing material removal rate, and the radial dressing speed, by decreasing power, lead to decreasing special energy. The temperature created by grinding lead to decreasing plastic deformation and boundary layer formation. When the radial dressing speed changes from 1 to 0.6 mu m/rev and other parameters are kept unchanged the roughness of surface increases and the special energy decreases. Sufficient dressing is very essential in limiting the width of the molten zone to few micrometers. As a result, it was found that local melting at contact spots to be a rather common mechanism during grinding of superalloys, lead to so-called white layers which can easily be observed on metallographic cross sections.
机译:镍基超合金是最着名的复杂和可用的超合金,以制造燃气轮机的热区部件。复杂的尺寸公差,特别是刀片根的根目录,表明刀片根系生产的研磨过程的重要性。预测加工参数对用于在加工操作期间工作部件达到合适的表面精加工和避免裂缝形成的组件表面的声音的影响通常并不容易可行,因此需要更多的工业调查。该研究是由GE设计的框架5叶片,并研究了Up.738LC的超合金制成。研究了在Huleralloy的研磨过程中形成塑性变形和热影响区域,具有高深切割深度但缓慢的工作速度(蠕变进料研磨)。工作速度,切割深度和径向敷料速度的参数被认为是变量,并且他们的效果已经研究。在实验所执行的情况下,测量的电动机的电压和电流和功率和特殊能量计算。一些样品在中性氩气下1176℃下1小时,冷却速率为15℃/ min,高达537℃,然后空气冷却)以研究晶粒重结晶。已经从叶片的根部产生了其他样品,然后通过镍涂覆以测量边界层微硬度。结果表明,增加的工作速度导致增加使用功率。通过提高材料去除速率和径向敷料速度来增加切割深度,通过降低功率,导致特殊能量降低。通过研磨产生的温度导致塑性变形和边界层形成的降低。当径向敷料速度从1到0.6μm/ Rev和其他参数保持不变时,表面增加的粗糙度和特殊能量减小。足够的敷料在将熔融区的宽度限制到几微米的宽度是非常重要的。结果,发现在接触点处局部熔化是在研磨超合金期间成为相当常见的机制,导致所谓的白色层,其在金相横截面上可以容易地观察到。

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