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横向气动载荷作用下转子系统动力响应研究 被引量:4

Study of dynamic responses of rotor systems to transverse forces
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摘要 旋转失速会对发动机转子系统产生横向作用力 .根据旋转失速时压气机内压力在时间域和空间域的变化规律建立了横向载荷的数学模型 ,在有限元软件MSC/NASTRAN计算平台上 ,利用DMAP语言开发了考虑陀螺力矩影响的复杂转子系统动力分析程序 .对单、双转子发动机在横向载荷作用下转子系统的动力响应进行了数字模拟 .得到了横向载荷作用下转子系统动力响应的一般规律 。 The characteristics of the rotating stall and surge in axial compressors showed that it is the rotating stall that generates the force on the rotor in radial direction. A mathematic model of the force on rotor in radial direction was established to simulate the change of pressure in compressors. The complex eigenvalues and transient responses of the single-rotor system and dual-rotor system were studied using the programs which were developed in direct matrix abstraction program(DMAP) based on MSC/NASTRAN platform. Some general disciplin arians of dynamic responses of rotor systems to transverse force were found, which was helpful to how to take into account the transverse forces when designing the rotor systems of aeroengine.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2004年第1期64-69,共6页 Journal of Beijing University of Aeronautics and Astronautics
关键词 旋转失速 动力特性 瞬态响应 数字模拟 rotating stall dynamic characteristics transient response numerical simulation
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参考文献4

  • 1彭泽琰 杜声同 郭秉衡.航空燃气轮机原理[M].北京:国防工业出版社,1989..
  • 2Hiroshi ISHII, Yasushige KASHIWABARA. A study on surge and rotating stall in axial compressors(a summary of the measurement and fundamental analysis method)[J]. JSME International Journal, Series II,1989,32(4):583~590
  • 3Willems F, Rram de Jager. Modeling and control of rotating stall and surge: an overview[A]. Proceedings of the 1998 IEEE International Conference on Control Application[C]. Trieste, Italy, 1998.331-335
  • 4冯国权 朱梓根.航空发动机喘振对转子系统横向载荷的确定方法[A]..第十届航空发动机结构强度与振动会议论文集[C].安徽歙县,2000.325-328.

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