首页> 外文会议>Smart Structures and Integrated Systems Mar 3-6, 2003 San Diego, California, USA >Development of a semi-active friction device to reduce vibration by energy dissipation
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Development of a semi-active friction device to reduce vibration by energy dissipation

机译:开发一种半主动摩擦装置,以通过能量耗散来减少振动

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Aerospace structures such as antennas and solar panels often consist of truss elements which are connected by bolted joints. Friction damping in these bolted joint connections structures has been identified as a major source of damping. It has been proposed that an improvement in vibration reduction could be obtained by controlling the normal contact force using integrated piezoelectric elements in order to maximize the energy dissipated at the interface between the connected parts. This paper presents analytical and experimental results in order to demonstrate the interest of implementing semi-active vibration reduction by dissipating energy through dry friction contact surfaces. This work fits within the scope of a research project aiming at the development of a semi-active compact piezoelectric friction device which can be bonded to any light structure. In this device, a moving component will rub on two friction surfaces and the normal force on friction surfaces will be controlled so that the distance between moving component and friction surfaces is neither too small (to avoid shock and stiction that cancel the slip between two surfaces and then friction effect) or too large (lose of contact surface). This device will then be positioned on the structure in order to allow the maximum energy dissipation by friction to reduce the vibrations of the structure. Such semi-active device will ensure stability of the control approach and will avoid the spillover effect found with the active approach in addition to reduce energy consumption cost. In this paper, an analytical and experimental study is carried out on two beams assembled by a joint bolted to show the influence of the normal gripping force (tightening torque in this case), directly related to the friction force, on the damping of the modes.
机译:诸如天线和太阳能电池板之类的航空航天结构通常由通过螺栓连接连接的桁架元件组成。这些螺栓连接结构中的摩擦阻尼已被确定为阻尼的主要来源。已经提出,通过使用集成的压电元件控制法向接触力,以使在连接部分之间的界面处耗散的能量最大化,可以提高减振效果。本文介绍了分析和实验结果,以证明通过通过干摩擦接触表面耗散能量来实现半主动减振的兴趣。这项工作适合于旨在开发可粘合到任何轻型结构的半主动紧凑型压电摩擦装置的研究项目。在此设备中,运动的组件将在两个摩擦表面上摩擦,并且将控制摩擦表面上的法向力,以使运动的组件和摩擦表面之间的距离不会太小(以避免震动和静摩擦消除两个表面之间的滑动)然后产生摩擦效果)或太大(接触面丢失)。然后将该设备放置在结构上,以便通过摩擦最大程度地耗散能量,以减少结构的振动。这样的半主动装置将确保控制方法的稳定性,并且除了减少能耗成本之外,还将避免主动方法发现的溢出效应。在本文中,对通过螺栓连接的两根梁进行了分析和实验研究,以显示法向夹持力(在这种情况下为拧紧扭矩)与摩擦力直接相关,对模式阻尼的影响。 。

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