2009
DOI: 10.1088/0964-1726/18/2/025007
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Active shape control of composite structures under thermal loading

Abstract: Maintaining the shape of high-precision structures such as space antennas is a challenging issue for designers. Varying temperature conditions will induce thermal distortions in these structures. Development of smart materials offers great potential to correct the shape. In this study, shape control of a composite structure under thermal loading using piezocomposites is investigated. Macro-Fibre Composite (MFC TM) patches are bonded to the structure. The structure is subjected to a through-the-thickness temper… Show more

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Cited by 18 publications
(8 citation statements)
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References 21 publications
(33 reference statements)
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“…Finite element predictions of beam deflection were in good agreement with experimental data, however no quantitative comparison of prediction error was presented. Recently, Binette et al[17] conducted experimental characterisation of laminate deflection for a composite panel subjected to thermal loading. Piezoelectric actuation via two MFC actuators was used to reverse the induced thermal deformation.…”
mentioning
confidence: 99%
“…Finite element predictions of beam deflection were in good agreement with experimental data, however no quantitative comparison of prediction error was presented. Recently, Binette et al[17] conducted experimental characterisation of laminate deflection for a composite panel subjected to thermal loading. Piezoelectric actuation via two MFC actuators was used to reverse the induced thermal deformation.…”
mentioning
confidence: 99%
“…In order to get the structural response of piezo composite laminated plates and shells, the earlier studies of simulation techniques are mainly using commercial software, for example, ANSYS (Bowen et al, 2011; Dano et al, 2008), ABAQUS (Binette et al, 2009; Ren, 2008), with the results compared to those from experiments. Furthermore, the investigations of cured shape and snap-through of asymmetric bistable laminates actuated by MFC has been carried out by Bowen et al (2011) and Giddings et al (2011).…”
Section: Modeling Of Piezo-fiber Composite Bonded Structuresmentioning
confidence: 99%
“…Barkanov et al investigated the active twist control of a helicopter rotor blade using an MFC actuator to reduce vibration and noise, without any complex mechanism in the rotating systems [17]. Binette et al studied the shape control of composite structures using MFC actuators [18]. They used MFC actuators to compensate for thermally-induced distortion of a sandwich plate subjected to a through-the-thickness thermal gradient.…”
Section: Introductionmentioning
confidence: 99%