CAJ | 학술논문

航空发动机压气机声共振机理十分复杂，涉及到“气动-结构-声学”的多物理场耦合问题，能导致压气机叶片疲劳破坏，危害巨大，近年来已经成为国外压气机气动、振动、声学领域的研究热点。综述了国外流体诱发腔体发声机理的研究进展，分析了国外航空发动机压气机声共振的研究现状，总结了单级、多级压气机声共振现象的主要特征，并结合中国某型压气机的试验结果，进行了气动、振动、噪声等物理参数的特征分析，认为某型压气机虽然存在着某些独特的问题需要深入研究，但其故障特点与近年来国外开展的声共振现象具有很强的相似性，即认为该型压气机工作中可能存在声共振现象。
항공발동궤압기궤성공진궤리십분복잡，섭급도“기동-결구-성학”적다물리장우합문제，능도치압기궤협편피로파배，위해거대，근년래이경성위국외압기궤기동、진동、성학영역적연구열점。종술료국외류체유발강체발성궤리적연구진전，분석료국외항공발동궤압기궤성공진적연구현상，총결료단급、다급압기궤성공진현상적주요특정，병결합중국모형압기궤적시험결과，진행료기동、진동、조성등물리삼수적특정분석，인위모형압기궤수연존재착모사독특적문제수요심입연구，단기고장특점여근년래국외개전적성공진현상구유흔강적상사성，즉인위해형압기궤공작중가능존재성공진현상。
The acoustic resonance mechanism of aeroengine compressors was complicated, which related to the problem of multi- physics coupling for the aerodynamics-structure-acoustics. It became a hot research issue internationally in the fields of compressor aerodynamics, vibration and acoustics in recent years, because it might cause the fatigue failure of compressor blades. The international research development of flow-induced cavity sound mechanism was overviewed, the present research of international aeroengine acoustic resonance was analyzed, and the main features of the acoustic resonance for the single stage and multi-stage compressors were concluded. The feature analysis of physical parameters such as aerodynamics, vibration and acoustics was conducted in China. Some special problems are analyzed in compressor, but its failure features were similar with the acoustic resonance in foreign countries. The results show that the acoustic resonance may exist in the compressor operation.