Internal Heat Transfer Measurement on Metal-Based Additively Manufactured Channels Using a Transient Technique

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL
Patrick Lüscher, Marin Deflorin, Manuel Voggesser, Peter Stuber, Vincent Galoul, Minseok Ko
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Abstract

Abstract The advancements in additive manufacturing (AM) of metals open new possibilities in the design of gas turbine parts. Especially the cooling efficiency of internal channels can be improved with more complex geometries. Naturally, AM channels have a higher surface roughness than conventionally manufactured parts, which influences the cooling air pressure loss as well as the heat transfer. Implementing novel cooling designs using AM can be possible only if the effect of increased surface roughness on the flow and on the heat transfer can be predicted with an appropriate accuracy. The objective of the current study was to measure these parameters experimentally in simple AM channels to build a database for designing complex and efficient cooling designs using the AM technique. A test rig and postprocessing method was elaborated to derive the local internal heat transfer distribution of metal-based AM channels. Six circular single channel coupons made by selective laser melting (SLM) were tested for Reynolds numbers ranging from 20,000 to 50,000. The coupon with the lowest relative roughness shows good agreement with the Dittus–Boelter correlation. All the other coupons show a consistent increase of internal heat transfer and flow friction with the increase of the internal surface roughness.
用瞬态技术测量金属基增材制造通道的内部传热
金属增材制造技术的进步为燃气轮机部件的设计开辟了新的可能性。特别是内部通道的冷却效率可以通过更复杂的几何形状来提高。当然,AM通道具有比传统制造部件更高的表面粗糙度,这会影响冷却空气压力损失以及传热。只有当增加的表面粗糙度对流动和传热的影响能够以适当的精度预测时,使用增材制造实现新颖的冷却设计才有可能。本研究的目的是在简单的调幅通道中实验测量这些参数,为使用调幅技术设计复杂而高效的冷却设计建立数据库。阐述了金属基调幅通道局部内部传热分布的实验装置和后处理方法。采用选择性激光熔化(SLM)法制备了6种圆形单通道片状材料,对其雷诺数在20000 ~ 50000之间进行了测试。相对粗糙度最低的地层与Dittus-Boelter相关性吻合较好。随着内表面粗糙度的增加,内部换热和流动摩擦的增加是一致的。
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来源期刊
CiteScore
4.70
自引率
11.80%
发文量
168
审稿时长
9 months
期刊介绍: The Journal of Turbomachinery publishes archival-quality, peer-reviewed technical papers that advance the state-of-the-art of turbomachinery technology related to gas turbine engines. The broad scope of the subject matter includes the fluid dynamics, heat transfer, and aeromechanics technology associated with the design, analysis, modeling, testing, and performance of turbomachinery. Emphasis is placed on gas-path technologies associated with axial compressors, centrifugal compressors, and turbines. Topics: Aerodynamic design, analysis, and test of compressor and turbine blading; Compressor stall, surge, and operability issues; Heat transfer phenomena and film cooling design, analysis, and testing in turbines; Aeromechanical instabilities; Computational fluid dynamics (CFD) applied to turbomachinery, boundary layer development, measurement techniques, and cavity and leaking flows.
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