<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>1390-0129</journal-id>
<journal-title><![CDATA[Revista Politécnica]]></journal-title>
<abbrev-journal-title><![CDATA[Rev Politéc. (Quito)]]></abbrev-journal-title>
<issn>1390-0129</issn>
<publisher>
<publisher-name><![CDATA[Escuela Politécnica Nacional]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S1390-01292017000100037</article-id>
<title-group>
<article-title xml:lang="es"><![CDATA[Diseño, construcción de la estructura mecánica y pruebas de vuelo de un hexacóptero de monitoreo para aplicaciones militares]]></article-title>
<article-title xml:lang="en"><![CDATA[Design, construction of the mechanical structure and flight tests of a monitoring hexacopter for military applications]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Paúl]]></surname>
<given-names><![CDATA[Dávila]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Javier]]></surname>
<given-names><![CDATA[Orna]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Andres]]></surname>
<given-names><![CDATA[Rosales]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Eduardo]]></surname>
<given-names><![CDATA[Ávalos]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
</contrib-group>
<aff id="Af1">
<institution><![CDATA[,Escuela Politécnica Nacional Facultad de Ingeniería Mecánica ]]></institution>
<addr-line><![CDATA[Quito ]]></addr-line>
<country>Ecuador</country>
</aff>
<aff id="Af2">
<institution><![CDATA[,Escuela Politécnica Nacional Facultad de Ingeniería Electrónica ]]></institution>
<addr-line><![CDATA[Quito ]]></addr-line>
<country>Ecuador</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>04</month>
<year>2017</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>04</month>
<year>2017</year>
</pub-date>
<volume>39</volume>
<numero>1</numero>
<fpage>37</fpage>
<lpage>48</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://scielo.senescyt.gob.ec/scielo.php?script=sci_arttext&amp;pid=S1390-01292017000100037&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://scielo.senescyt.gob.ec/scielo.php?script=sci_abstract&amp;pid=S1390-01292017000100037&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://scielo.senescyt.gob.ec/scielo.php?script=sci_pdf&amp;pid=S1390-01292017000100037&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="es"><p><![CDATA[Resumen: La presente investigación tiene por objeto el diseño bajo el concepto de elementos finitos y construcción de un hexacóptero de monitoreo para áreas inaccesibles. La estructura del hexacóptero se ha construido con fibra de carbono para obtener el menor peso posible en la estructura y brindar resistencia a la misma. En el diseño aerodinámico se realizan los cálculos para determinar la potencia requerida en los rotores, para ello se comparan dos teorías, la teoría de cantidad de movimiento y la teoría de elemento de pala, este análisis determina que cada motor requiere una potencia de 614,64 W. Para cumplir con los requerimientos de autonomía se han utilizado 6 baterías LiPo de 5000 mAh de 6 celdas de almacenamiento con un voltaje de salida de 22,2 V. Con esta configuración se logran tiempos de vuelo continuo sin carga de 40 minutos.]]></p></abstract>
<abstract abstract-type="short" xml:lang="en"><p><![CDATA[Abstract: The present research aims to perform the design and construction of a monitoring hexacopter. The drone has been made of carbon fiber, in order to obtain the lightest structure possible and increase the aircraft payload. In the design, the aerodynamic calculations were made in order to determine the required power for the rotors. For this reason, two theories were compared, the momentum theory and the propeller theory. After performing this analysis it was possible to determine which each engine required a power equal to 614,64 W. In order to fulfill the autonomy requirements, six LiPo batteries of 5000 mAh with six cells in order to get an output voltage of 22,2 V, have been used. This configuration has been allowed to obtain a continuous flight without load during 40 minutes.]]></p></abstract>
<kwd-group>
<kwd lng="es"><![CDATA[Dron]]></kwd>
<kwd lng="es"><![CDATA[hexacóptero]]></kwd>
<kwd lng="es"><![CDATA[fibra de carbono]]></kwd>
<kwd lng="en"><![CDATA[Drone]]></kwd>
<kwd lng="en"><![CDATA[hexacopter]]></kwd>
<kwd lng="en"><![CDATA[carbon fiber]]></kwd>
</kwd-group>
</article-meta>
</front><back>
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</article>
