带宽弦叶片的盘片耦合振动特性研究  

Model analysis of bladed disk coupled system of compressor with low aspect ratio

作　　者：张大义[1] 史亚杰[1] 林力[2] 洪杰[1] 

机构地区：[1]北京航空航天大学能源与动力工程学院,北京100083 [2]民航上海中等专业学校,上海200232

出　　处：《北京航空航天大学学报》2004年第9期808-812,共5页Journal of Beijing University of Aeronautics and Astronautics

摘　　要：为确定盘片系统将发生的耦合共振 ,建立了带宽弦叶片的盘片耦合系统的基本重复扇区的有限元模型 ,并采用波传播技术对耦合系统进行了振动特性的计算分析 .指出了宽弦叶片在振动中表现出的特有振型 ,以及随转速的变化规律 .分析了盘片耦合后的振动特性 。To study the blade vibration in coupled impellers system, a finite element model in the base sector for a coupled impellers system with low aspect ratio in a compressor was created. A vibration analysis for the coupled system by wave transmitting technique was processed, thus computing the coupled vibration that may occur during operation. The special vibration mode of blades with low aspect ratio was figured and the relation between frequency of vibration and rotating speed was developed. The special modes of vibration in the impellers system with low aspect ratio and the relation between frequency of vibration and node lines were described.

关 键 词：叶片振动 叶轮 耦合共振 小展弦比 有限单元法 

分 类 号：V232.4[航空宇航科学与技术—航空宇航推进理论与工程]