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Performance and Functionality Based Design Methods for Improved and Novel Aircraft Engine Components for Additive Manufacturing

机译:基于性能和功能的设计方法,用于增材制造的改进和新型飞机发动机组件

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For aircraft engine manufacturers the technology of AM appears promising. AM provides the opportunity for a highly flexible and a cost effective part production. Furthermore AM offers new potentials and possibilities for lightweight designs. The implementation and applications of AM can be divided in three different strategic application levels. The first level includes manufacturing simple existing parts; these kinds of parts are already in production. In the second level, new design tools, such as structural optimization, are used to improve an existing part by benefiting from the new design freedom but without changing its functionality. The third level includes novel parts with new functionality. This paper presents design methods for AM parts for the second and third level: performance and solution based approach, respectively. Also the safety classification of engine parts is looked into. Step-by-step design methods are presented, accompanied by case studies that demonstrate improvement to the initial design: a light weight, topology optimized turbine guide vane (level two) and an aircraft engine casing design that has an improved tip clearance behavior under transient operating cycles (level three).
机译:对于飞机发动机制造商而言,增材制造技术似乎很有前途。 AM为高度灵活和具有成本效益的零件生产提供了机会。此外,AM为轻量化设计提供了新的潜力和可能性。 AM的实施和应用可以分为三个不同的战略应用级别。第一级包括制造简单的现有零件。这些零件已经在生产中。在第二级中,新的设计工具(例如结构优化)通过受益于新的设计自由性而无需更改其功能来改进现有零件。第三层包括具有新功能的新颖部件。本文介绍了第二级和第三级AM零件的设计方法:分别是基于性能和基于解决方案的方法。还研究了发动机零件的安全性分类。介绍了分步设计方法,并结合案例研究证明了对初始设计的改进:重量轻,拓扑优化的涡轮导向叶片(第二级)和飞机发动机壳体设计,在瞬态情况下具有改进的叶尖间隙性能操作周期(三级)。

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