| Citation: | ZENG Liang, LI Lin. Experiments on dynamic response of labyrinth air seals with damping-ring/sleeves[J]. Journal of Aerospace Power, 2008, 23(10): 1813-1820.
|
| [1] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第18分册[M].北京:航空工业出版社,2001.
|
| [2] |
Alford J S.Protection of labyrinth seals from flexural vibration[J].Journal of Engineering for Power,1964:141-148.
|
| [3] |
Alford J S.Protecting turbo machinery from unstable and oscillatory flows[J].Journal of Engineering for Power,1967:513-528.
|
| [4] |
Alford,J S.Nature,cause and prevention of labyrinth air seal failures[J].Journal of Aircraft,1975,12(4):313-318.
|
| [5] |
Niemotka M A,Ziegert J C.Optimal design of split ring dampers for gas turbine engines[R].Cincinati,Ohio;International Gas Turbine and Aeroengine Congress and Exposition,1 993.
|
| [6] |
曾亮,李琳.具有接触接合面的封严组件振动特性分析[J].航空动力学报,2006,21(5):854-861.ZENG Liang,LI Lin.The vibration performance of contact system of labyrinth assembly[J].Journal of Aerospace Power,2006,2I(5):854-861.(in Chinese)
|
| [7] |
曾亮,李琳.用于篦齿封严装置的减振阻尼环设计理论[J].北京航空航天大学学报,2006,33(5):518-522.ZENG Liang,LI Lin.Design of damping-ring for vibration control in labyrinth air seals[J].Journal of Beijing University of Aeronautics and Astronautics,2006,33(5):518-522.(in Chinese)
|
| [8] |
曾亮,郭雪莲,李琳.带有阻尼环(套)的篦齿封严装置固有特性的理论及实验研究[J].航空动力学报,2007,22(7):1035-1043.ZENG Liang,GUO Xuelian,LI Lin.The theoretic and experimental modal analysis of labyrinth air seals with damping-ring/sleeves[J].Journal of Aerospace Power,2007,22(7):1035-1043.(in Chinese)
|
| [9] |
曾亮.旋转薄壁结构的减振装置设计理论与实验研究[D].北京:北京航空航天大学,2007.ZENG Liang.The design and experiment research of damping devices for vibration control in thin-walled structures[D].Beijing:Bering University of Aeronautics and Astronautics,2007.(in Chinese)
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