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Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps

机译：压电陶瓷堆叠致动器中的滞后表征及其对主动控制襟翼直升机振动和降噪的影响

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Eric Muir; Li Liu; Peretz Friedmann; Devesh Kumar;
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1. Effect of Piezoceramic Actuator Hysteresis on Helicopter Vibration and Noise Reduction [J] . Eric R. Muir, Li Liu, Peretz P. Friedmann, Journal of guidance, control, and dynamics . 2012,第4期

机译：压电陶瓷作动器迟滞对直升机振动和降噪的影响
2. Dynamic hysteresis of piezoceramic stack actuators used in helicopter vibration control: experiments and simulations [J] . Viswamurthy SR, Rao AK, Ganguli R Smart Materials & Structures . 2007,第4期

机译：直升机振动控制中使用的压电陶瓷叠层执行器的动态滞后：实验和模拟
3. An experimental and numerical study of piezoceramic actuator hysteresis in helicopter active vibration control [J] . Rajnish Mallick, Ranjan Ganguli, M. Seetharama Bhat Proceedings of the Institution of Mechanical Engineers . 2014,第g5期

机译：压电陶瓷作动器迟滞在直升机主动振动控制中的实验和数值研究
4. Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps [C] . E. Muir, P. Friedmann, D. Kumar, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 18th AIAA/ASME/AHS Adaptive Structures Conference, 12th AIAA Non-Deterministic Approaches Conference, 11th AIAA Gossamer Systems Forum, 6th AIAA Multidisciplinary Design Optimization Specialist Conference . 2010

机译：压电陶瓷作动器的磁滞特性及其对使用主动控制襟翼的直升机振动和降噪的影响
5. Simultaneous BVI noise and vibration reduction in rotorcraft using actively-controlled flaps and including performance considerations. [D] . Patt, Daniel A. 2004

机译：使用主动控制襟翼同时降低旋翼航空器的BVI噪声和振动，并考虑性能。
6. Research on Hysteresis of Piezoceramic Actuator Based on the Duhem Model [O] . Miaolei Zhou, Jingyuan Wang 2013

机译：基于Duhem模型的压电陶瓷执行器磁滞研究
7. REDUCTION OF VIBRATIONS DUE TO DYNAMIC STALL IN HELICOPTERS USING AN ACTIVELY CONTROLLED FLAP [O] . G. Depailler, P. P. Friedmann 2014

机译：使用活动控制的皮瓣减少直升机动态失速引起的振动
8. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade [R] . Millott, T. A., Friedmann, P. P. 1994

机译：使用位于叶片上的主动控制的部分跨度后缘襟翼减少直升机旋翼的振动

Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps

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