On the active deformations of hybrid specimens

Purpose The purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of composite specimens are made up of thin carbon and glass substrates on which some Macro Fiber Composite® (MFC) piezoelectric patches are glued. A pr...

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Published inAircraft engineering Vol. 88; no. 5; pp. 676 - 687
Main Authors Chiarelli, Mario Rosario, Binante, Vincenzo, Botturi, Stefano, Massai, Andrea, Kunzmann, Jan, Colbertaldo, Angelo, Romano, Diego Giuseppe
Format Journal Article
LanguageEnglish
Published Bradford Emerald Group Publishing Limited 05.09.2016
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ISSN1748-8842
1758-4213
DOI10.1108/AEAT-02-2015-0058

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Abstract Purpose The purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of composite specimens are made up of thin carbon and glass substrates on which some Macro Fiber Composite® (MFC) piezoelectric patches are glued. A proper design and manufacturing of the hybrid specimens as well as testing activities have been performed. The research activity has been carried out under the FutureWings project, funded by the European Commission within the 7th Framework. Design/methodology/approach The paper describes the basic assumptions made to define specimen geometries and to carry out experimental tests. Finite element (FE) results and experimental data (laser technique measurements) have been compared: it shows very good agreement for the displacements’ distribution along the specimens. Findings Within the objectives of the project, the study of passive and active deformation characteristics of the hybrid composite material has provided reference technical data and has allowed for the correct adaptation of the FE models. More in particular, using the hybrid specimens, both the bending deformations and the torsion deformations have been studied. Practical implications The deformation capability of the hybrid specimens will be used in the development of prototypical three-dimensional structures, that, through the electrical control of the MFC patches, will be able to change the curvature of their cross section or will be able to change the angle of torsion along their longitudinal axis. Originality/value The design of nonstandard specimens and the tests executed represent a novelty in the field of structures using piezoelectric actuators. The numerical and experimental data of the present research constitute a small step forward in the field of smart materials technology.
AbstractList PurposeThe purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of composite specimens are made up of thin carbon and glass substrates on which some Macro Fiber Composite® (MFC) piezoelectric patches are glued. A proper design and manufacturing of the hybrid specimens as well as testing activities have been performed. The research activity has been carried out under the FutureWings project, funded by the European Commission within the 7th Framework.Design/methodology/approachThe paper describes the basic assumptions made to define specimen geometries and to carry out experimental tests. Finite element (FE) results and experimental data (laser technique measurements) have been compared: it shows very good agreement for the displacements’ distribution along the specimens.FindingsWithin the objectives of the project, the study of passive and active deformation characteristics of the hybrid composite material has provided reference technical data and has allowed for the correct adaptation of the FE models. More in particular, using the hybrid specimens, both the bending deformations and the torsion deformations have been studied.Practical implicationsThe deformation capability of the hybrid specimens will be used in the development of prototypical three-dimensional structures, that, through the electrical control of the MFC patches, will be able to change the curvature of their cross section or will be able to change the angle of torsion along their longitudinal axis.Originality/valueThe design of nonstandard specimens and the tests executed represent a novelty in the field of structures using piezoelectric actuators. The numerical and experimental data of the present research constitute a small step forward in the field of smart materials technology.
Purpose The purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of composite specimens are made up of thin carbon and glass substrates on which some Macro Fiber Composite® (MFC) piezoelectric patches are glued. A proper design and manufacturing of the hybrid specimens as well as testing activities have been performed. The research activity has been carried out under the FutureWings project, funded by the European Commission within the 7th Framework. Design/methodology/approach The paper describes the basic assumptions made to define specimen geometries and to carry out experimental tests. Finite element (FE) results and experimental data (laser technique measurements) have been compared: it shows very good agreement for the displacements’ distribution along the specimens. Findings Within the objectives of the project, the study of passive and active deformation characteristics of the hybrid composite material has provided reference technical data and has allowed for the correct adaptation of the FE models. More in particular, using the hybrid specimens, both the bending deformations and the torsion deformations have been studied. Practical implications The deformation capability of the hybrid specimens will be used in the development of prototypical three-dimensional structures, that, through the electrical control of the MFC patches, will be able to change the curvature of their cross section or will be able to change the angle of torsion along their longitudinal axis. Originality/value The design of nonstandard specimens and the tests executed represent a novelty in the field of structures using piezoelectric actuators. The numerical and experimental data of the present research constitute a small step forward in the field of smart materials technology.
Author Binante, Vincenzo
Kunzmann, Jan
Colbertaldo, Angelo
Romano, Diego Giuseppe
Chiarelli, Mario Rosario
Massai, Andrea
Botturi, Stefano
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CitedBy_id crossref_primary_10_1016_j_mechmat_2020_103350
crossref_primary_10_1016_j_ymssp_2018_01_026
crossref_primary_10_1155_2019_8210235
crossref_primary_10_1088_1361_665X_ad10c2
crossref_primary_10_1016_j_compstruct_2021_115018
crossref_primary_10_3390_s20040950
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Copyright Mario Chiarelli, Vincenczo Binante, Stefano Botturi, Andrea Massai, Jan Kunzmann, Angelo Colbertaldo, Diego Romano
2016. This work is published under http://creativecommons.org/licences/by/3.0/legalcode (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
2016. This work is published under http://creativecommons.org/licences/by/3.0 (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
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Issue 5
Keywords Finite element method
Hybrid specimens
Laser technique
Composite substrate
Macro Fiber Composite
Language English
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StartPage 676
SubjectTerms Carbon fiber reinforced plastics
Composite materials
Curvature
Deformation
Electric fields
Fiber composites
Finite element method
Glass substrates
Hybrid composites
Manufacturing
Mathematical models
Mechanical properties
Patches (structures)
Piezoelectric actuators
Piezoelectricity
Sensors
Smart materials
Studies
Torsion
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Title On the active deformations of hybrid specimens
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