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 in | Aircraft engineering Vol. 88; no. 5; pp. 676 - 687 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Bradford
Emerald Group Publishing Limited
05.09.2016
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Subjects | |
Online Access | Get full text |
ISSN | 1748-8842 1758-4213 |
DOI | 10.1108/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. |
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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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Keywords | Finite element method Hybrid specimens Laser technique Composite substrate Macro Fiber Composite |
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References_xml | – volume: 24 start-page: 20 issue: 10 year: 2015 ident: key2020121221003803600_ref007 article-title: Design, realization and structural testing of a compliant adaptable wing publication-title: Smart Materials and Structures – ident: key2020121221003803600_ref009 – volume: 22 start-page: 10 issue: 7 year: 2013 ident: key2020121221003803600_ref003 article-title: Experimental identification of smart material coupling effects in composites structures publication-title: Smart Materials and Structures – volume: 20 start-page: 10 issue: 1 year: 2011 ident: key2020121221003803600_ref015 article-title: Control of a flexible beam actuated by macro-fiber composite patches: II, Hysteresis and creep compensation, experimental results publication-title: Smart Materials and Structures – volume: 18 start-page: 12 issue: 2 year: 2009 ident: key2020121221003803600_ref002 article-title: Active shape control of composite structures under thermal loading publication-title: Smart Materials and Structures – volume: 107 start-page: 346 issue: 1 year: 2014 ident: key2020121221003803600_ref016 article-title: A bidirectional B-spline finite point method for the analysis of piezoelectric laminated composite plates and its application in material parameter identification publication-title: Composite Structures – ident: key2020121221003803600_ref004 – ident: key2020121221003803600_ref006 – volume: 2013 start-page: 9 year: 2013 ident: key2020121221003803600_ref013 article-title: Procedure to use PZT sensors in vibration and load measurements publication-title: Smart Materials Research – year: 2011 ident: key2020121221003803600_ref001 article-title: Surface actuated variable-camber and variable-twist morphing wings using piezocomposites – ident: key2020121221003803600_ref017 – year: 2010 ident: key2020121221003803600_ref008 article-title: A composite wing with a morphing leading edge – year: 2004 ident: key2020121221003803600_ref012 article-title: Overview of the common DLR/ONERA project ‘Active twist blade’ (ATB) – volume: 18 start-page: 9 issue: 1 year: 2009 ident: key2020121221003803600_ref010 article-title: Active wing design with integrated flight control using piezoelectric macro fiber composites publication-title: Smart Materials and Structures – volume: 20 start-page: 7 issue: 1 year: 2011 ident: key2020121221003803600_ref014 article-title: Control of a flexible beam actuated by macro-fiber composite patches: I, Modeling and feed forward trajectory control publication-title: Smart Materials and Structures – volume: 21 start-page: 7 issue: 1 year: 2012 ident: key2020121221003803600_ref005 article-title: Fatigue life characterization for piezoelectric macrofiber composites publication-title: Smart Materials and Structures – volume: 25 start-page: 12 issue: 5 year: 2016 ident: key2020121221003803600_ref011 article-title: Finite element modelling and analysis of piezo-integrated composite structures under large applied electric fields publication-title: Smart Materials and Structures |
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The purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of... PurposeThe purpose of this study concerns numerical studies and experimental validation of the mechanical behavior of hybrid specimens. These kinds of... |
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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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