首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >FLOW IN A SIMULATED TURBINE BLADE COOLING CHANNEL WITH SPATIALLY VARYING ROUGHNESS CAUSED BY ADDITIVE MANUFACTURING ORIENTATION
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FLOW IN A SIMULATED TURBINE BLADE COOLING CHANNEL WITH SPATIALLY VARYING ROUGHNESS CAUSED BY ADDITIVE MANUFACTURING ORIENTATION

机译:在模拟涡轮叶片冷却通道中流动,具有由加性制造方向引起的空间不同的粗糙度

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Because of the effects of gravity acting on the melt region created during the laser sintering process, additively manufactured surfaces that are pointed upward have been shown to exhibit roughness characteristics different from those seen on surfaces that point downward. For this investigation, the Roughness Internal Flow Tunnel (RIFT) and computational fluid dynamics models were used to investigate flow in channels with different roughness on opposing walls of the channel. Three rough surfaces were employed for the investigation. Two of the surfaces were created using scaled, structured-light scans of the upskin and downskin surfaces of an Inconel 718 component which was created at a 45° angle to the printing surface and documented by Snyder et al. [1]. A third rough surface was created for the RIFT investigation using a structured-light scan of a surface similar to the Inconel 718 downskin surface, but a different scaling was used to provide larger roughness elements in the RIFT. The resulting roughness dimensions (R_q
机译:由于对在激光烧结过程中产生的熔体区域上的重力作用的影响,所向上指向的加成型表面表现出与在下方的表面上看到的那些不同的粗糙度特性。对于该研究,粗糙度内部流动隧道(裂谷)和计算流体动力学模型用于研究具有不同粗糙度的通道中的流动在通道的相对壁上。采用了三个粗糙的表面进行调查。使用Inconel 718组分的上皮和下皮扫描的缩放,结构光扫描的两个表面产生,其以45°角地与印刷表面产生并由Snyder等人进行文件。 [1]。使用类似于Inconel 718下皮表面的表面的结构光扫描来创建第三粗糙表面,而是使用类似于Inconel 718下线表面的表面,但是使用不同的缩放来在裂缝中提供更大的粗糙度元件。所用三个表面的所得粗糙度尺寸(R_Q / D_H)为0.0064,0.0156和0.0405。对于由光滑壁相对的每个表面并由每个其他粗糙壁相对的每个表面测量摩擦系数在10,000

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