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航空发动机叶片丢失问题研究综述
引用本文:马艳红,梁智超,王桂华,张大义,洪杰.航空发动机叶片丢失问题研究综述[J].航空动力学报,2016,31(3):513-526.
作者姓名:马艳红  梁智超  王桂华  张大义  洪杰
作者单位:1. 北京航空航天大学 能源与动力工程学院, 北京 100191;
摘    要:对近年来航空发动机叶片丢失问题的研究进展进行了综述.简述了叶片丢失过程相关的力学问题,重点探讨了叶片丢失激励下转子和整机结构系统的瞬态动力特性以及持续生存能力方面的力学机理、数值仿真和试验研究成果,包括叶片丢失过程中的载荷及力学行为、整机动力学建模和求解技术、整机和机理性的试验研究等.研究表明:对于恶劣载荷环境下复杂结构系统,需要以整机系统为研究对象并考虑载荷时效特征,通过结构和动力学安全性设计策略提升结构完整性和可靠性. 

关 键 词:叶片丢失    结构安全性    瞬态动力特性    持续生存能力    突加不平衡    严重碰摩    非对称转子
收稿时间:2014/7/25 0:00:00

Review on the blade loss of aero-engine
MA Yan-hong,LIANG Zhi-chao,WANG Gui-hu,ZHANG Da-yi and HONG Jie.Review on the blade loss of aero-engine[J].Journal of Aerospace Power,2016,31(3):513-526.
Authors:MA Yan-hong  LIANG Zhi-chao  WANG Gui-hu  ZHANG Da-yi and HONG Jie
Institution:1. School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China;3. Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China
Abstract:Research progress on the blade loss of aero-engine was reviewed in recent years. The mechanical problems related to the blade loss process were outlined. The mechanical mechanism, numerical simulation and the test study of the transient dynamical characteristic and survival ability due to blade loss in the rotor and whole aero-engine structural system were discussed emphatically. The studies involved the load and mechanical behavior, the techniques of modeling and calculation, the test of mechanism and the whole aero-engine. The results show that it's necessary to take the whole aero-engine system as object and consider the load aging characteristic of the complex structural system in severe environment. The structural integrity and reliability can be improved by structural and dynamical design strategy.
Keywords:blade loss  structural safety  transient dynamical characteristic  survival ability  sudden unbalance  heavy rub-impact  anisotropic rotor
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