运七飞机座舱的压电主动振动控制实验研究  

An Experimental Investigation on Active Vibration Control of Y-7 Aircraft Fuselage Using Piezoelectric Sensors and Actuators

作　　者：姚军[1] 李岳锋[2] 姚起杭 

机构地区：[1]北京航空航天大学,北京100083 [2]南京航空航天大学,南京210076 [3]飞机强度研究所,西安710065

出　　处：《应用力学学报》2002年第2期65-69,共5页Chinese Journal of Applied Mechanics

摘　　要：由于实验规模与复杂性的限制 ,将压电材料用于实际飞机振动主动控制的实验研究极少 ,因而缺少对其实用潜力的探讨。为评估压电陶瓷在实际飞机结构上用于减振的可行性和效果 ,以运七飞机座舱壁板为试件 ,实地进行了基于准独立模态控制策略的主动振动控制实验 ,取得理想的控制效果 ;表明了建模和控制方法的正确性与有效性 。There are few active vibration control experimental investigation on actual aircraft structure using piezoelectric sensors and actuators owing to large scale and complexity of the experiment. Therefore there is a lack of discussion about practicability of piezoelectric structure. In order to evaluate feasibility and effect of suppressing vibration of actual aircraft structure using piezoelectric sensors and actuators, a test for damping control on the panel of an Y7 aircraft fuselage was carried out in the field on site, based on independence modal control approach. The results show that the model and the control strategy of this paper are effective and practicable, and indicated that it is feasible and potential to use piezoceramics to realize the active vibration control for aircraft structures.

关 键 词：运七飞机 座舱 智能结构 压电陶瓷 独立模态控制 主动振动控制 

分 类 号：TB535.1[理学—物理] V216.21[理学—声学]