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Experimental Investigations on the Effect of Slot-Type Casing Treatments with the Aim of Improvement the Aerodynamic and Acoustic Characteristics of Advanced Fans

机译:槽型套管处理效果的实验研究旨在提高高级风机的空气动力学和声学特性

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This paper presents experimental investigations of aerodynamic and acoustic characteristics for the C179-2 bypass fan model with different versions of a slot-type casing treatment (CT). This work aims at optimization the CT configuration for a simultaneously improvement of aerodynamic parameters (efficiency and stall margin), as well as the use of this CT as a reactive type silencer to reduce fan noise. All versions of the slot-type CTs under study are designed on the basis of a semi-empirical procedure developed by CIAM. Three versions of a slot-type CT are designed and tested as applied to the C179-2 fan model. Based on the analysis of experimental data found by aerodynamic tests to study the effect of the number of CT rows, the geometry of CT slots, their relative positions and the height of its annular cavity on key aerodynamic characteristics of the C179-2 fan model, it is found that: 1.all CTs under study considerably increase stall margins (by 8% -16%) of the fan in moderate and high modes determined by n - corrected rotational speed (n=75 - 100 %). The stall margin at n = 54 % increases by approx. 30 %. 2.relative position of slots in the three CTs with identical number of slots in both rows has a noticeable effect on the CT gas-dynamic efficiency. A half-step shift of axes of the slots relative to each other leads to a slight increase (by max. 1.6%) in stall margins in moderate and high modes and a considerable increase in efficiency (by avg. 2 %) in the same modes, except for n = 100 %. The beneficial effect of the CT on an increase in stall margins ASM and efficiency (along the operating line) is found for the Cl 79-2 single-row bypass fan model stage with total pressure ratio 1.56 in the bypass duct and corrected tip speed 404 m/s. A series of experimental studies of acoustic characteristics of the Cl 79-2 fan model stage with three versions of the slot-type casing treatment is completed in conditions of the C-3A acoustic test facility with an anechoic chamber. The acoustic tests of the fan model are carried out within n=40 - 100 % corrected rotational speeds (as compared with the nominal speed). The specified speed range covers takeoff (n=90.7 %), climb (n=85.2 %), cruise (n=100 %), and approach (n=58.2 %) modes. For all fan operating modes, narrow-band noise spectra and radiation patterns are compared for the C179-2 model configurations with a smooth flow passage and with the CT. In addition to a substantial improvement in gas-dynamic characteristics, the use of the slot-type CT for the C179-2 bypass fan model stage results in a considerable improvement in its acoustic characteristics. In total, the sound power of the Cl 79-2 single-row by-pass fan model decreases by 3 dB for three certification modes.
机译:本文为C179-2旁通风扇模型提供了具有不同版本的槽型套管处理(CT)的实验研究。这项工作旨在优化CT配置,同时改进空气动力学参数(效率和失速余量),以及使用该CT作为反应式消音器以降低风扇噪声。根据CIAM开发的半实证程序,设计了正在研究的所有版本的插槽类型CT。设计并测试了三个插槽类型CT的版本,以应用于C179-2风扇模型。基于对空气动力学测试发现的实验数据的分析,研究CT行数,CT槽几何形状,其相对位置和其环形腔高度对C179-2风扇模型的关键空气动力学特性,结果发现:1.所有正在研究的CTS在由N校正的转速(n = 75-100%)确定的中等和高模式中的空气裕度大大增加了失速余量(通过8%-16%)风扇(n = 75-100%)。 n = 54%的失速余量增加约。 30%。 2.在两个行中具有相同数量的插槽中的三个CTS中的插槽的关系对CT气体动力学效率具有显着影响。相对于彼此相对于彼此相对于彼此的轴的半步偏移导致中等和高模式的失速边缘略微增加(最大1.6%),并且效率相当大增加(AVG。2%)模式,除n = 100%之外。 CT对停顿边缘ASM和效率(沿着操作线)的增加的有益效果是针对CL 79-2单排旁路风扇模型阶段的,以总压力比为1.56在旁路管道上,校正尖端速度404多发性硬化症。一系列关于CL 79-2风扇模型阶段的声学特性的一系列实验研究,其中三个版本的槽型壳体处理在具有化学杂志的C-3A声学测试设备的条件下完成。风扇模型的声学测试在n = 40-100%校正的旋转速度内进行(与标称速度相比)。指定的速度范围涵盖起飞(n = 90.7%),爬升(n = 85.2%),巡航(n = 100%),以及方法(n = 58.2%)模式。对于所有风扇操作模式,将窄带噪声光谱和辐射模式与C179-2模型配置进行比较,具有平滑的流动通道和CT。除了大幅提高气体动力学特性之外,对于C179-2旁路风扇模型阶段的槽型CT的使用导致其声学特性的相当大。总共,CL 79-2单排旁通风扇模型的声功率为三种认证模式减少了3 dB。

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