Passive damping augmentation of a vibrating beam using pseudoelastic shape memory alloy wires

被引:31
作者
Gandhi, F [1 ]
Chapuis, G [1 ]
机构
[1] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
D O I
10.1006/jsvi.2001.3935
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This paper examines the effectiveness of pseudoelastic shape memory alloy (SMA) wires for passive damping of flexural vibrations of a clamped-free beam with a tip mass. A finite-element model of the system is developed and validated with experimental results. The SMA behavior is modelled using amplitude-dependent complex modulus. Numerical simulations indicate that the damping introduced by the SMA wires will increase for higher excitation-force amplitudes that produce higher strain levels in the SMA wires. Increasing the wire cross-section area provides more damping at low force-excitation amplitudes,. but reduced damping at higher amplitudes. The angle between the beam and the SMA wires is an influential parameter, and a value in the 10-20degrees range was found to introduce maximum damping. The underlying physical mechanisms are examined in detail. System damping depends only mildly on the SMA wire length, and is unaffected by the tip mass. (C) 2002 Academic Press.
引用
收藏
页码:519 / 539
页数:21
相关论文
共 21 条
[1]  
[Anonymous], DAMPING MAT MEMBERS
[2]  
BOYD JG, 1994, P ASME MECH PHAS TRA, V189, P159
[3]  
Brinson L. C., 1993, J INTELLIGENT MATERI, V2, P229, DOI DOI 10.1177/1045389X9300400213
[4]  
CHAPUIS G, 1999, THESIS PENNSYLVANIA
[5]  
CLARK PW, 1995, P SOC PHOTO-OPT INS, V2445, P241, DOI 10.1117/12.208891
[6]  
Flugge W, 1967, VISCOELASTICITY, V1st
[7]   Characterization of the pseudoelastic damping behavior of shape memory alloy wires using complex modulus [J].
Gandhi, F ;
Wolons, D .
SMART MATERIALS & STRUCTURES, 1999, 8 (01) :49-56
[8]   Analysis of bearingless main rotor aeroelasticity using an improved time domain nonlinear elastomeric damper model [J].
Gandhi, F ;
Chopra, I .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1996, 41 (03) :267-277
[9]   ANALYTICAL MODEL FOR A NONLINEAR ELASTOMERIC LAG DAMPER AND ITS EFFECT ON AEROMECHANICAL STABILITY IN HOVER [J].
GANDHI, F ;
CHOPRA, I .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (04) :59-69
[10]   A time-domain non-linear viscoelastic damper model [J].
Gandhi, F ;
Chopra, I .
SMART MATERIALS & STRUCTURES, 1996, 5 (05) :517-528