首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >EXPERIMENTAL STUDY ON THERMAL EFFICIENCY OF A MULTI-JET ANTI-ICING SYSTEM WITH PICCOLO TUBE
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EXPERIMENTAL STUDY ON THERMAL EFFICIENCY OF A MULTI-JET ANTI-ICING SYSTEM WITH PICCOLO TUBE

机译:用Piccolo管多喷射防糖系统的热效率的实验研究

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An experimental study was conducted to investigate the jet impingement thermal efficiency of a typical model for a multi-jet anti-icing system under different experimental conditions such as air mass flow rate at the jet exit, piccolo tube position and circumferential angle of jet holes. The experimental results showed that jet mass flow rate, velocity at the jet exits (whether choking conditions were established at the jet exits or not) and piccolo tube-to-leading edge distance within the cavity had significant influence on thermal efficiency of the anti-icing system. The heat flux on the external surface of leading edge, diameter of jet holes and circumferential angle of jet holes had a measurable but small effect on thermal efficiency of the anti-icing system.
机译:进行了实验研究,以研究不同实验条件下多射流防掺杂系统的典型模型的喷射冲击热效率,例如喷射出口处的空气质量流量,微众管位置和射流的周向角度。实验结果表明,喷射出口的射流质量流量,速度(无论是在喷射器中是否建立窒息条件),并且在腔内的Piccolo管 - 前沿距离对抗的热效率有显着影响冰系统。前沿的外表面的热量,喷射孔的直径和喷射孔的圆周角度对防冰系统的热效率有可测量但小的影响。

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