[1] HALWES D R. LIVE—Liquid Inertia Vibration Eliminator[C]//American Helicopter Society 36th Annual Forum. Fairfax, VA: American Helicopter Society, 1980. [2] YORK D, WANG X, GORDANINEJAD F. A new MR Fluid-Elastomer (MRF-E) vibration isolator[J]. Journal of Intelligent Material Systems and Structures,2007, 27: 87-93. [3] 龚亮. 液弹隔振器设计与试验研究[D]. 南京: 南京航空航天大学, 2012: 26-42. GONG L. Design and testing of the fluid elastomer isolator[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012: 26-42 (in Chinese). [4] 航空航天工业部科学技术研究院.直升机动力学手册[M]. 北京: 航空工业出版社, 1991: 28-40. Chinese Aeronautics and Astronautics Establishment. Handbook of helicopter dynamics[M]. Beijing: Aviation Industry Press, 1991: 28-40 (in Chinese). [5] 邓旭东. 直升机高性能主减隔振系统分析与仿真研究[D]. 南京: 南京航空航天大学, 2011: 8-18. DENG X D. Analysis and simulation for helicopter intelligent vibration isolating system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011: 8-18 (in Chinese). [6] 张扬. 带液弹隔振器的直升机主减隔振系统动力学建模与仿真[D]. 南京: 南京航空航天大学, 2013: 23-32. ZHANG Y. The dynamic modeling and simulation of the helicopter gearbox isolation system with fluid elastomer isolator[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013: 23-32 (in Chinese). [7] 覃海鹰, 李满福, 洪蛟. 新型液弹阻尼器原理与初步构型设计分析[J]. 直升机技术, 2003(3): 21-24. QIN H Y, LI M F, HONG J. Principle and analysis of primary configuration design of new fluidelastic lead-lag damper[J]. Helicopter Technique, 2003(3): 21-24 (in Chinese). [8] 雷少保, 张勇, 王华明. 聚焦式液弹隔振系统的传递性分析[J]. 南京航空航天大学学报, 2015, 47(2): 275-278. LEI S B, ZHANG Y, WANG H M. Transmission characteristics of focul fluid elastomer vibration isolation system[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2015, 47(2): 275-278 (in Chinese).