Piezoelectric polymer actuators for vibration suppression

dc.contributor.authorSchmidt, V. Hugo
dc.contributor.authorConant, J.
dc.contributor.authorBohannan, Gary W.
dc.contributor.authorEckberg, J.
dc.contributor.authorHalko, S.
dc.contributor.authorHallenberg, J.
dc.contributor.authorNelson, C.
dc.contributor.authorPeterson, N.
dc.contributor.authorSmith, C.
dc.contributor.authorThrasher, C.
dc.contributor.authorTikalsky, B.
dc.date.accessioned2016-12-05T22:55:32Z
dc.date.available2016-12-05T22:55:32Z
dc.date.issued1999
dc.description.abstractWe have designed and built piezoelectric polymer actuators in a 'bellows' configuration and have used them in a near-zero-g environment vibrations suppression apparatus. The actuator is based on poly(vinylidene fluoride) (PVDF) sheets produced by AMP and electroded to our specifications. The actuator consists of two bimorphs, each with a double-bend precurvature, glued together at their ends so that the actuator has its thickest air gap at the middle. Each bimorph consists of two sheets glued together. Each sheet is electroded completely on the outside (ground) side, and has three electrode areas on the other side. If the electrode on the middle half is positive, and on the outer two quarters are negative, the bimorph curvature and the actuator length increase; with opposite polarities they decrease. In the vibration isolation application, the box to be isolated has actuators mounted between it and its surrounding enclosure on the vibrating vehicle. Feedback control is provided to change actuator length to compensate for vehicle motions and vibrations. This feedback is provided by accelerometers and by laser diode position sensors. The inherent softness of the actuator provides good passive damping of higher frequencies. So far, a one-dimensional test of the system has been made using a mass on a 'folded pendulum' as a 'weightless' (no restoring force for small displacements) load. Also, a two- dimensional version was flown on NASA's KC-135, which provided 25-second near-zero-g intervals during parabolic flight segments. Our goal is three-dimensional isolation for space vehicle applications.en_US
dc.identifier.citationV.H. Schmidt, J. Conant, G. Bohannan, J. Eckberg, S. Halko, J. Hallenberg, C. Nelson, N. Peterson, C. Smith, C. Thrasher, and B. Tikalsky, “Piezoelectric polymer actuators for vibration suppression,” Proceedings of the SPIE: Smart Structures and Materials 1999: Electroactive Polymer Actuators and Devices, vol. 3669, pp. 162-170 (1999).en_US
dc.identifier.issn0277-786X
dc.identifier.urihttps://scholarworks.montana.edu/handle/1/12322
dc.language.isoen_USen_US
dc.titlePiezoelectric polymer actuators for vibration suppressionen_US
dc.typeArticleen_US
mus.citation.extentfirstpage162en_US
mus.citation.extentlastpage170en_US
mus.citation.journaltitleProceedings of the SPIE: Smart Structures and Materials 1999: Electroactive Polymer Actuators and Devices (EAPAD)en_US
mus.citation.volume3669en_US
mus.identifier.categoryPhysics & Mathematicsen_US
mus.identifier.doihttp://dx.doi.org/10.1117/12.349673en_US
mus.relation.collegeCollege of Letters & Scienceen_US
mus.relation.departmentPhysicsen_US
mus.relation.universityMontana State University - Bozemanen_US

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