首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >COMPUTATIONAL AND EXPERIMENTAL STUDIES OF CELLULAR SAMPLES MANUFACTURED USING ADDITIVE METHODS FOR USE IN ADVANCED LIGHTWEIGHT DESIGNS OF ENGINE PARTS
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COMPUTATIONAL AND EXPERIMENTAL STUDIES OF CELLULAR SAMPLES MANUFACTURED USING ADDITIVE METHODS FOR USE IN ADVANCED LIGHTWEIGHT DESIGNS OF ENGINE PARTS

机译:使用添加剂方法制造的细胞样品的计算和实验研究,用于发动机件的先进轻质设计

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The use of cellular structures is one way to reduce the weight of engine parts. Cellular structures are used to provide rigidity and strength for parts subject to compression, bending, and shock loads. Failure of the individual elements of a lattice/cell structure does not result in the destruction of the entire part; this stands in contrast to the structure of a conventional homogeneous metal object, in which cracks will continue to increase with increasing load, causing the destruction of the entire part. Lattice/cell structures have relatively high characteristics of rigidity and strength, excellent thermal insulation properties, energy absorption characteristics, and high fatigue resistance. The use of this type of structure in engine part construction opens up new opportunities for advanced aviation applications. However, the deformation behavior of porous and metallic structures differs significantly from that of conventional homogeneous materials. Samples with cellular and porous structures are themselves designs. Therefore, procedures for strength testing and interpretation of experimental results for cellular and porous structures differ from those for samples derived from homogeneous materials. The criteria for determining the properties of cellular structures include density, stiffness, ability to accumulate energy, etc. These parameters depend on the configuration of the cells, the size of each cell, and the thickness of the connecting elements. Mechanical properties of cellular structures can be established experimentally and confirmed numerically. Special cellular specimens have been designed for uniaxial tensile, bending, compression, shear, and low-cycle fatigue testing. Several variants of cell structures with relative densities ranging from 13 to 45% were considered. Specifically, the present study examined the stress-strain states of cell structures from brands "CobaltChrome MP1" powder compositions obtained by laser synthesis on an industrial 3D printer Concept Laser M2 Cusing Single Laser 400W. Numerical simulations of the tests were carried out by the finite element method. Then, the most rational cellular structures in terms of mass and strength were established on the basis of both real and numerical experiments.
机译:使用蜂窝结构是减少发动机部件重量的一种方式。蜂窝结构用于为受压力,弯曲和冲击负载进行的部件提供刚性和强度。格子/细胞结构的个体元素的失效不会导致整个部分的破坏;这与传统均质金属物体的结构相反,其中裂缝将继续随着负荷的增加而增加,导致整个部分的破坏。晶格/电池结构具有相对高的刚性特性和强度,绝热性能优异,能量吸收特性和高疲劳性。在发动机部件施工中使用这种结构为先进的航空应用开辟了新的机会。然而,多孔和金属结构的变形行为与常规均匀材料的变形行为显着不同。具有细胞和多孔结构的样品本身设计。因此,对细胞和多孔结构的实验结果的强度测试和解释的程序不同于衍生自均质材料的样品。确定蜂窝结构特性的标准包括密度,刚度,积累能量的能力等。这些参数取决于电池的配置,每个单元的尺寸和连接元件的厚度。可以在实验上确定细胞结构的机械性能并在数值上确认。专为单轴拉伸,弯曲,压缩,剪切和低循环疲劳试验设计了特殊的细胞样本。考虑了相对密度范围为13至45%的细胞结构的几种变体。具体地,本研究检测了通过激光合成在工业3D打印机概念激光M2中获得的品牌“CobaltChrome MP1”粉末组合物的压力 - 应变状态,该粉末组合物在工业3D打印机概念激光M2上围绕单激光400W。通过有限元法进行测试的数值模拟。然后,基于实际和数值实验建立质量和强度方面最合理的细胞结构。

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