A non-linear stiffness composite twisting I-beam
A classic structural component of mechanical engineering, the I-beam, is re-designed by adding a morphing twist functionality to the high bending stiffness inherent to the geometry of the component. The beam, as with its conventional counterpart, is made of two flanges separated by a web. Here, bi-s...
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Veröffentlicht in: | Journal of intelligent material systems and structures 2014-04, Vol.25 (6), p.744-754 |
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creator | Lachenal, Xavier Daynes, Stephen Weaver, Paul M |
description | A classic structural component of mechanical engineering, the I-beam, is re-designed by adding a morphing twist functionality to the high bending stiffness inherent to the geometry of the component. The beam, as with its conventional counterpart, is made of two flanges separated by a web. Here, bi-stability is introduced from a combination of flange pre-stress, web geometry and material properties, yielding a highly non-linear twist morphing structure while keeping the low weight and the high bending stiffness of the beam. The present case study offers two twisted stable shapes and can be morphed from one stable configuration to the other by applying a snap-through twist moment to the ends of the structure. Correlation is found between tests results, finite element model data and analytical predictions, validating the modelling assumptions. A sensitivity study is also performed to understand the influence of the design parameters of the beam and loading condition on the stability of the structure. As a result, the three conflicting requirements of adaptive structures are met in a single structural entity: low mass, load-carrying capability and compliance. |
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The beam, as with its conventional counterpart, is made of two flanges separated by a web. Here, bi-stability is introduced from a combination of flange pre-stress, web geometry and material properties, yielding a highly non-linear twist morphing structure while keeping the low weight and the high bending stiffness of the beam. The present case study offers two twisted stable shapes and can be morphed from one stable configuration to the other by applying a snap-through twist moment to the ends of the structure. Correlation is found between tests results, finite element model data and analytical predictions, validating the modelling assumptions. A sensitivity study is also performed to understand the influence of the design parameters of the beam and loading condition on the stability of the structure. 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The beam, as with its conventional counterpart, is made of two flanges separated by a web. Here, bi-stability is introduced from a combination of flange pre-stress, web geometry and material properties, yielding a highly non-linear twist morphing structure while keeping the low weight and the high bending stiffness of the beam. The present case study offers two twisted stable shapes and can be morphed from one stable configuration to the other by applying a snap-through twist moment to the ends of the structure. Correlation is found between tests results, finite element model data and analytical predictions, validating the modelling assumptions. A sensitivity study is also performed to understand the influence of the design parameters of the beam and loading condition on the stability of the structure. As a result, the three conflicting requirements of adaptive structures are met in a single structural entity: low mass, load-carrying capability and compliance.</description><subject>Beams (structural)</subject><subject>Bending</subject><subject>Buckling</subject><subject>Exact sciences and technology</subject><subject>Flanges</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>General equipment and techniques</subject><subject>H beams</subject><subject>I beams</subject><subject>Instruments, apparatus, components and techniques common to several branches of physics and astronomy</subject><subject>Mathematical analysis</subject><subject>Measurement and testing methods</subject><subject>Nonlinearity</subject><subject>Physics</subject><subject>Servo and control equipment; robots</subject><subject>Solid mechanics</subject><subject>Static elasticity (thermoelasticity...)</subject><subject>Stiffness</subject><subject>Structural and continuum mechanics</subject><issn>1045-389X</issn><issn>1530-8138</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNp1kM1LAzEQxYMoWKt3j3sRvERnks0meyzFj0LBi4K3JU0nZctutiZbxP_elIoHwdMM837zmHmMXSPcIWp9j1Aqaep3lAqEUfKETVBJ4AalOc19lvlBP2cXKW0B0CiQEwazIgyBd20gG4s0tt4HSqlwQ78bUjtSMX62eRw2xYKvyPaX7MzbLtHVT52yt8eH1_kzX748LeazJXclwshJaigr68kiGUnojUQvdL4IZYlrQao2Am25sk5WsPalswaqmrQWqlZGyCm7Pfru4vCxpzQ2fZscdZ0NNOxTg5VGpWtRY0bhiLo4pBTJN7vY9jZ-NQjNIZzmbzh55ebH3SZnOx9tcG363RNGGq0AMsePXLIbarbDPob89P--32ZebtQ</recordid><startdate>20140401</startdate><enddate>20140401</enddate><creator>Lachenal, Xavier</creator><creator>Daynes, Stephen</creator><creator>Weaver, Paul M</creator><general>SAGE Publications</general><general>Sage Publications</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>20140401</creationdate><title>A non-linear stiffness composite twisting I-beam</title><author>Lachenal, Xavier ; Daynes, Stephen ; Weaver, Paul M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c410t-e37046afea1e83e1f831f275301341d2e59821a4bac360df4ca8069e772595823</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Beams (structural)</topic><topic>Bending</topic><topic>Buckling</topic><topic>Exact sciences and technology</topic><topic>Flanges</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>General equipment and techniques</topic><topic>H beams</topic><topic>I beams</topic><topic>Instruments, apparatus, components and techniques common to several branches of physics and astronomy</topic><topic>Mathematical analysis</topic><topic>Measurement and testing methods</topic><topic>Nonlinearity</topic><topic>Physics</topic><topic>Servo and control equipment; robots</topic><topic>Solid mechanics</topic><topic>Static elasticity (thermoelasticity...)</topic><topic>Stiffness</topic><topic>Structural and continuum mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lachenal, Xavier</creatorcontrib><creatorcontrib>Daynes, Stephen</creatorcontrib><creatorcontrib>Weaver, Paul M</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of intelligent material systems and structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lachenal, Xavier</au><au>Daynes, Stephen</au><au>Weaver, Paul M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A non-linear stiffness composite twisting I-beam</atitle><jtitle>Journal of intelligent material systems and structures</jtitle><date>2014-04-01</date><risdate>2014</risdate><volume>25</volume><issue>6</issue><spage>744</spage><epage>754</epage><pages>744-754</pages><issn>1045-389X</issn><eissn>1530-8138</eissn><abstract>A classic structural component of mechanical engineering, the I-beam, is re-designed by adding a morphing twist functionality to the high bending stiffness inherent to the geometry of the component. The beam, as with its conventional counterpart, is made of two flanges separated by a web. Here, bi-stability is introduced from a combination of flange pre-stress, web geometry and material properties, yielding a highly non-linear twist morphing structure while keeping the low weight and the high bending stiffness of the beam. The present case study offers two twisted stable shapes and can be morphed from one stable configuration to the other by applying a snap-through twist moment to the ends of the structure. Correlation is found between tests results, finite element model data and analytical predictions, validating the modelling assumptions. A sensitivity study is also performed to understand the influence of the design parameters of the beam and loading condition on the stability of the structure. 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subjects | Beams (structural) Bending Buckling Exact sciences and technology Flanges Fundamental areas of phenomenology (including applications) General equipment and techniques H beams I beams Instruments, apparatus, components and techniques common to several branches of physics and astronomy Mathematical analysis Measurement and testing methods Nonlinearity Physics Servo and control equipment robots Solid mechanics Static elasticity (thermoelasticity...) Stiffness Structural and continuum mechanics |
title | A non-linear stiffness composite twisting I-beam |
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