Influence of Variable-Geometry Adjustment on the Matching Characteristics of a Medium Variable Bypass Ratio Compression System

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Qiaodan Luo, Shengfeng Zhao, Shiji Zhou, Huafeng Xu, X.Q. Sheng
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Abstract

The research is based on a full 3D model of a medium variable bypass ratio compression system. The effects of core-driven fan stage (CDFS) VIGV adjustment and forward variable area bypass injector (FVABI) adjustment on the internal flow and component matching characteristics of the compression system during the mode transition process are investigated. The findings of the study reveal that during the mode transition period, the adjustment of variable-geometry components has a negligible impact on the aerodynamic performance of the fan. The closure of the CDFS VIGV has a significant effect on reducing the pressure ratio of the CDFS but only a minor effect on its efficiency. Additionally, the efficiency and pressure ratio of the high-pressure compressor (HPC) increase with the closure of the CDFS VIGV, particularly the second stage of the HPC. When the CDFS VIGV is closed by 30°, the efficiency of the second stage of the HPC increases by 3.4%, while that of the first stage only increases by 3.1%. Under the high bypass mode, increasing the FVABI opening will move the matching point of the CDFS towards the choke boundary. When the FVABI opening increases from 0.30 to 0.58, the efficiency of the CDFS decreases by 3.6%, while the efficiency of the HPC only increases by 0.4%. In summary, closing the CDFS VIGV and increasing the opening of the FVABI will increase the bypass ratio of the compression system, and the former has a more significant impact. When the compression system transitions from the low bypass mode to the high bypass mode, opening of the FVABI should be appropriately reduced to prevent CDFS matching in the operating condition too closely to the choke boundary, thereby maintaining the efficiency of each component of the compression system at a relatively high level.
变几何调整对介质变涵道比压缩系统匹配特性的影响
该研究基于介质变涵道比压缩系统的全三维模型。研究了核心驱动风机级(CDFS) VIGV调节和前向变面积旁通喷油器(FVABI)调节对压缩系统模态转换过程中内部流动和部件匹配特性的影响。研究结果表明,在模态转换期间,变几何部件的调整对风机气动性能的影响可以忽略不计。CDFS VIGV的关闭对降低CDFS的压比有显著影响,但对其效率影响较小。此外,高压压气机(HPC)的效率和压力比随着CDFS VIGV的关闭而增加,特别是在高压压气机的第二阶段。当CDFS的VIGV关闭30°时,HPC的第二级效率提高了3.4%,而第一级效率仅提高了3.1%。在高旁路模式下,增大FVABI开度会使CDFS的匹配点向扼流圈边界移动。当FVABI开度从0.30增加到0.58时,CDFS的效率降低3.6%,而HPC的效率仅提高0.4%。综上所述,关闭CDFS的VIGV和增加FVABI的开度会增加压缩系统的涵道比,且前者的影响更为显著。当压缩系统由低涵道模式过渡到高涵道模式时,应适当减小FVABI的开度,防止运行工况下CDFS匹配过于靠近扼流圈边界,从而使压缩系统各部件的效率保持在较高水平。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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