Piezo-composite actuated control surface system for flying vehicle
Purpose - The purpose of this paper is to develop lightweight actuators in order to replace conventional hydraulic pneumatic actuators and to apply the actuation system to a small flying vehicle.Design methodology approach - A new type of control surface using a piezo-composite actuator for a small...
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| Veröffentlicht in: | Aircraft Engineering and Aerospace Technology 2010-10, Vol.82 (6), p.372-375 |
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| container_title | Aircraft Engineering and Aerospace Technology |
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| creator | Hoon Park, Ki Soo Yoon, Bum Trung Nguyen, Ngoc Seo Goo, Nam Sam Kang, Tae Joon Yoon, Kwang |
| description | Purpose - The purpose of this paper is to develop lightweight actuators in order to replace conventional hydraulic pneumatic actuators and to apply the actuation system to a small flying vehicle.Design methodology approach - A new type of control surface using a piezo-composite actuator for a small flying vehicle has been designed and manufactured. The piezo-composite actuator is composed of a piezoelectric ceramic layer, a carbon epoxy layer and glass epoxy layers. Through this, the miniaturization and weight reduction of the actuation systems for flying vehicle can be achieved. A simple model of the control surface has been manufactured and evaluated through experiments.Findings - The performance test results showed that the developed actuator can produce stable angle of attack independent of the applied loading. A radio controller for the actuator was developed to control the motions wirelessly. It was found that the piezo-composite actuator and its integrated controller system have a possibility to be used not only as a small flying vehicle but also as a control surface actuator of a small unmanned flying robot through the miniaturization of power supply and control system.Originality value - The paper describes the procedures of designing and manufacturing smart structure application of the piezo-composite actuator with performance evaluation and comparison method. It is expected that piezo-composite actuator can be used as a small flying vehicle control surface actuator through the miniaturization of power supply and control system with the use of the integrated radio controller MIPAD. |
| doi_str_mv | 10.1108/00022661011104529 |
| format | Article |
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The piezo-composite actuator is composed of a piezoelectric ceramic layer, a carbon epoxy layer and glass epoxy layers. Through this, the miniaturization and weight reduction of the actuation systems for flying vehicle can be achieved. A simple model of the control surface has been manufactured and evaluated through experiments.Findings - The performance test results showed that the developed actuator can produce stable angle of attack independent of the applied loading. A radio controller for the actuator was developed to control the motions wirelessly. It was found that the piezo-composite actuator and its integrated controller system have a possibility to be used not only as a small flying vehicle but also as a control surface actuator of a small unmanned flying robot through the miniaturization of power supply and control system.Originality value - The paper describes the procedures of designing and manufacturing smart structure application of the piezo-composite actuator with performance evaluation and comparison method. It is expected that piezo-composite actuator can be used as a small flying vehicle control surface actuator through the miniaturization of power supply and control system with the use of the integrated radio controller MIPAD.</description><identifier>ISSN: 1748-8842</identifier><identifier>ISSN: 0002-2667</identifier><identifier>EISSN: 1758-4213</identifier><identifier>DOI: 10.1108/00022661011104529</identifier><identifier>CODEN: AATEEB</identifier><language>eng</language><publisher>Bradford: Emerald Group Publishing Limited</publisher><subject>Actuation ; Actuators ; Aircraft ; Angle of attack ; Carbon-epoxy composites ; Control surfaces ; Control systems ; Controllers ; Design ; Flight ; Flying ; Miniaturization ; Performance evaluation ; Performance tests ; Piezoelectric ceramics ; Pneumatics ; Power supply ; Radio systems ; Receivers & amplifiers ; Smart structures ; Software ; Studies ; Vehicles ; Weight reduction</subject><ispartof>Aircraft Engineering and Aerospace Technology, 2010-10, Vol.82 (6), p.372-375</ispartof><rights>Emerald Group Publishing Limited</rights><rights>Emerald Group Publishing Limited 2010</rights><rights>Copyright Emerald Group Publishing Limited 2010</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c477t-6299b38397e63b7168240da8fbaa30e3d484dc559b228761d839068795958f853</citedby><cites>FETCH-LOGICAL-c477t-6299b38397e63b7168240da8fbaa30e3d484dc559b228761d839068795958f853</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,967,27924,27925</link.rule.ids></links><search><creatorcontrib>Hoon Park, Ki</creatorcontrib><creatorcontrib>Soo Yoon, Bum</creatorcontrib><creatorcontrib>Trung Nguyen, Ngoc</creatorcontrib><creatorcontrib>Seo Goo, Nam</creatorcontrib><creatorcontrib>Sam Kang, Tae</creatorcontrib><creatorcontrib>Joon Yoon, Kwang</creatorcontrib><title>Piezo-composite actuated control surface system for flying vehicle</title><title>Aircraft Engineering and Aerospace Technology</title><description>Purpose - The purpose of this paper is to develop lightweight actuators in order to replace conventional hydraulic pneumatic actuators and to apply the actuation system to a small flying vehicle.Design methodology approach - A new type of control surface using a piezo-composite actuator for a small flying vehicle has been designed and manufactured. The piezo-composite actuator is composed of a piezoelectric ceramic layer, a carbon epoxy layer and glass epoxy layers. Through this, the miniaturization and weight reduction of the actuation systems for flying vehicle can be achieved. A simple model of the control surface has been manufactured and evaluated through experiments.Findings - The performance test results showed that the developed actuator can produce stable angle of attack independent of the applied loading. A radio controller for the actuator was developed to control the motions wirelessly. It was found that the piezo-composite actuator and its integrated controller system have a possibility to be used not only as a small flying vehicle but also as a control surface actuator of a small unmanned flying robot through the miniaturization of power supply and control system.Originality value - The paper describes the procedures of designing and manufacturing smart structure application of the piezo-composite actuator with performance evaluation and comparison method. It is expected that piezo-composite actuator can be used as a small flying vehicle control surface actuator through the miniaturization of power supply and control system with the use of the integrated radio controller MIPAD.</description><subject>Actuation</subject><subject>Actuators</subject><subject>Aircraft</subject><subject>Angle of attack</subject><subject>Carbon-epoxy composites</subject><subject>Control surfaces</subject><subject>Control systems</subject><subject>Controllers</subject><subject>Design</subject><subject>Flight</subject><subject>Flying</subject><subject>Miniaturization</subject><subject>Performance evaluation</subject><subject>Performance tests</subject><subject>Piezoelectric ceramics</subject><subject>Pneumatics</subject><subject>Power supply</subject><subject>Radio systems</subject><subject>Receivers & amplifiers</subject><subject>Smart structures</subject><subject>Software</subject><subject>Studies</subject><subject>Vehicles</subject><subject>Weight reduction</subject><issn>1748-8842</issn><issn>0002-2667</issn><issn>1758-4213</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><sourceid>GNUQQ</sourceid><recordid>eNp10E1LwzAYB_AgCs7pB_BW9OLBat6THnX4BgM96DmkaaIdbVOTVpif3syJB-dOSeD3z_PwB-AYwQuEoLyEEGLMOYIoPSnDxQ6YIMFkTjEiu6s7lbmUFO-DgxgXECLOIJmA66fafvrc-Lb3sR5sps0w6sFWmfHdEHyTxTE4bWwWl3GwbeZ8yFyzrLvX7MO-1aaxh2DP6Sbao59zCl5ub55n9_n88e5hdjXPDRViyDkuipJIUgjLSSkQl5jCSktXak2gJRWVtDKMFSXGUnBUJQq5FAUrmHSSkSk4W__bB_8-2jioto7GNo3urB-jQlwgTCD-pid_6MKPoUvbKYnS6NTYCp1uQ5iSAjEGKU4KrZUJPsZgnepD3eqwVAiqVfVqo_qUOV9nbGuDbqrfyAZVfeUSh__z7RO-APYHjlM</recordid><startdate>20101019</startdate><enddate>20101019</enddate><creator>Hoon Park, Ki</creator><creator>Soo Yoon, Bum</creator><creator>Trung Nguyen, Ngoc</creator><creator>Seo Goo, Nam</creator><creator>Sam Kang, Tae</creator><creator>Joon Yoon, Kwang</creator><general>Emerald Group Publishing Limited</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7RQ</scope><scope>7TB</scope><scope>7WY</scope><scope>7XB</scope><scope>8AF</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BEZIV</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>F28</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>K6~</scope><scope>KB.</scope><scope>L.-</scope><scope>L6V</scope><scope>L7M</scope><scope>M0F</scope><scope>M1Q</scope><scope>M2P</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PDBOC</scope><scope>PQBIZ</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>Q9U</scope><scope>7QQ</scope><scope>JG9</scope></search><sort><creationdate>20101019</creationdate><title>Piezo-composite actuated control surface system for flying vehicle</title><author>Hoon Park, Ki ; Soo Yoon, Bum ; Trung Nguyen, Ngoc ; Seo Goo, Nam ; Sam Kang, Tae ; Joon Yoon, Kwang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c477t-6299b38397e63b7168240da8fbaa30e3d484dc559b228761d839068795958f853</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2010</creationdate><topic>Actuation</topic><topic>Actuators</topic><topic>Aircraft</topic><topic>Angle of attack</topic><topic>Carbon-epoxy composites</topic><topic>Control surfaces</topic><topic>Control systems</topic><topic>Controllers</topic><topic>Design</topic><topic>Flight</topic><topic>Flying</topic><topic>Miniaturization</topic><topic>Performance evaluation</topic><topic>Performance tests</topic><topic>Piezoelectric ceramics</topic><topic>Pneumatics</topic><topic>Power supply</topic><topic>Radio systems</topic><topic>Receivers & amplifiers</topic><topic>Smart structures</topic><topic>Software</topic><topic>Studies</topic><topic>Vehicles</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hoon Park, Ki</creatorcontrib><creatorcontrib>Soo Yoon, Bum</creatorcontrib><creatorcontrib>Trung Nguyen, Ngoc</creatorcontrib><creatorcontrib>Seo Goo, Nam</creatorcontrib><creatorcontrib>Sam Kang, Tae</creatorcontrib><creatorcontrib>Joon Yoon, Kwang</creatorcontrib><collection>CrossRef</collection><collection>Career & Technical Education Database</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>ABI/INFORM Collection</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>STEM Database</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Business Premium Collection</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>ProQuest Central Student</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Business Collection</collection><collection>Materials Science Database</collection><collection>ABI/INFORM Professional Advanced</collection><collection>ProQuest Engineering Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>ABI/INFORM Trade & Industry</collection><collection>Military Database</collection><collection>Science Database</collection><collection>Engineering Database</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>Materials Science Collection</collection><collection>ProQuest One Business</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>Engineering Collection</collection><collection>ProQuest Central Basic</collection><collection>Ceramic Abstracts</collection><collection>Materials Research Database</collection><jtitle>Aircraft Engineering and Aerospace Technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hoon Park, Ki</au><au>Soo Yoon, Bum</au><au>Trung Nguyen, Ngoc</au><au>Seo Goo, Nam</au><au>Sam Kang, Tae</au><au>Joon Yoon, Kwang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Piezo-composite actuated control surface system for flying vehicle</atitle><jtitle>Aircraft Engineering and Aerospace Technology</jtitle><date>2010-10-19</date><risdate>2010</risdate><volume>82</volume><issue>6</issue><spage>372</spage><epage>375</epage><pages>372-375</pages><issn>1748-8842</issn><issn>0002-2667</issn><eissn>1758-4213</eissn><coden>AATEEB</coden><abstract>Purpose - The purpose of this paper is to develop lightweight actuators in order to replace conventional hydraulic pneumatic actuators and to apply the actuation system to a small flying vehicle.Design methodology approach - A new type of control surface using a piezo-composite actuator for a small flying vehicle has been designed and manufactured. The piezo-composite actuator is composed of a piezoelectric ceramic layer, a carbon epoxy layer and glass epoxy layers. Through this, the miniaturization and weight reduction of the actuation systems for flying vehicle can be achieved. A simple model of the control surface has been manufactured and evaluated through experiments.Findings - The performance test results showed that the developed actuator can produce stable angle of attack independent of the applied loading. A radio controller for the actuator was developed to control the motions wirelessly. It was found that the piezo-composite actuator and its integrated controller system have a possibility to be used not only as a small flying vehicle but also as a control surface actuator of a small unmanned flying robot through the miniaturization of power supply and control system.Originality value - The paper describes the procedures of designing and manufacturing smart structure application of the piezo-composite actuator with performance evaluation and comparison method. It is expected that piezo-composite actuator can be used as a small flying vehicle control surface actuator through the miniaturization of power supply and control system with the use of the integrated radio controller MIPAD.</abstract><cop>Bradford</cop><pub>Emerald Group Publishing Limited</pub><doi>10.1108/00022661011104529</doi><tpages>4</tpages></addata></record> |
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| ispartof | Aircraft Engineering and Aerospace Technology, 2010-10, Vol.82 (6), p.372-375 |
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| language | eng |
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| source | Emerald Journals |
| subjects | Actuation Actuators Aircraft Angle of attack Carbon-epoxy composites Control surfaces Control systems Controllers Design Flight Flying Miniaturization Performance evaluation Performance tests Piezoelectric ceramics Pneumatics Power supply Radio systems Receivers & amplifiers Smart structures Software Studies Vehicles Weight reduction |
| title | Piezo-composite actuated control surface system for flying vehicle |
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