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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Numerical investigation on the effect of a plenum chamber with slot-type casing treatment on the performance of an axial transonic compressor
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Numerical investigation on the effect of a plenum chamber with slot-type casing treatment on the performance of an axial transonic compressor

机译:缝隙式壳体处理增压室对轴向跨音速压缩机性能影响的数值研究

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Casing treatment is an effective approach for improving compressor stall margin in axial compressors. A plenum chamber, which connects slots in the circumferential direction, can occasionally be found in slot-type casing treatments. This study investigates the effect of a plenum chamber on the compressor overall performance and stall margin via time-accurate three-dimensional numerical simulations in a transonic compressor NASA Rotor 37 with a slot-type casing treatment. Four configurations with variable height of plenum chamber are numerically investigated. The unsteady influence of the casing treatment on compressor flow fields is studied using fast Fourier transforms to gain a deeper insight into the function of the plenum chamber. The results indicate that the plenum chamber can reduce the penalty on the compressor's total pressure ratio and adiabatic efficiency induced by the casing treatment effect at the design operating condition. A detuning effect of the plenum chamber is found and proven to be responsible for the decreased compressor performance penalty through a detailed analysis in both the blade passage and casing treatments. The detuning effect dampens the unsteady influence of the casing treatment on the compressor passage flow in terms of shock oscillations and mass flow fluctuations. Thus, the radial scope and degree of the influence induced by the casing treatment is distinctly restrained by the plenum chamber. Slot circulation, which is composed of a bleed flow from the passage into the slots and injection flow from the slots into the passage, is closely related to the stall margin improvement as the casing treatment is implemented. The plenum chamber has no significant impact on the slot circulation and thus on compressor stall margin. However, shallow slots decrease the slot circulation efficiency, which leads to a much lower stall margin enhancement.
机译:套管处理是提高轴向压缩机中压缩机失速裕度的有效方法。在狭槽式套管处理中,偶尔会发现一个沿圆周方向连接狭槽的增压室。本研究通过跨槽式外壳处理的跨音速压缩机NASA转子37中的时间精确的三维数值模拟,研究了增压室对压缩机整体性能和失速裕度的影响。数值研究了具有可变高度的增压室的四种构造。使用快速傅立叶变换研究了套管处理对压缩机流场的非稳态影响,以更深入地了解增压室的功能。结果表明,在设计工况下,增压室可以减少对压缩机总压力比和绝热效率的不利影响。通过对叶片通道和壳体处理的详细分析,发现增压室的失谐作用并证明是造成压缩机性能下降的原因。失谐效应从冲击振荡和质量流量波动方面减轻了套管处理对压缩机通道流量的不稳定影响。因此,通过充气室明显地限制了由套管处理引起的影响的径向范围和程度。缝隙循环是由从通道到缝隙的排空流和从缝隙到通道的注入流组成的,与进行套管处理时的失速裕度的提高密切相关。增压室对槽循环并因此对压缩机失速裕度没有显着影响。然而,浅槽降低了槽循环效率,这导致了更低的失速裕度增强。

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