DocumentCode :
3354812
Title :
Similarity Study between Electrostatic MEMS and Aeroelastic Wing Structures
Author :
Kalyanaraman, Rakesh ; Packirisamy, Muthukumaran ; Bhat, Rama B.
Author_Institution :
Dept. of Mech. & Ind. Eng., Concordia Univ., Montreal, QC
Volume :
4
fYear :
2006
fDate :
9-13 July 2006
Firstpage :
3381
Lastpage :
3386
Abstract :
An analogy between the instabilities in electrostatic MEMS structures and aeroelastic aircraft wing structures has been inferred in this paper. The static and dynamic analysis of a simple mass-spring model of an electrostatically actuated MEMS structure is presented to understand the pull-in instability. Then the aeroelastic phenomenon occurring on the aircraft wing structures is explained with a simple one degree of freedom wing model. The divergence and flutter instabilities are studied. The control methods taken so far to counteract the instabilities in both cases have been discussed.
Keywords :
aerospace components; elasticity; electrostatic devices; mechanical stability; micromechanical devices; aeroelastic wing structures; divergence; dynamic analysis; electrostatic MEMS; flutter instabilities; mass-spring model; pull-in instability; static analysis; Aerodynamics; Aircraft propulsion; Electrostatic analysis; Industrial engineering; Laboratories; Mechanical systems; Micromechanical devices; Permittivity; Vibrations; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial Electronics, 2006 IEEE International Symposium on
Conference_Location :
Montreal, Que.
Print_ISBN :
1-4244-0496-7
Electronic_ISBN :
1-4244-0497-5
Type :
conf
DOI :
10.1109/ISIE.2006.296009
Filename :
4078937
Link To Document :
بازگشت