<?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>2007-9753</journal-id>
<journal-title><![CDATA[RIIIT. Revista internacional de investigación e innovación tecnológica]]></journal-title>
<abbrev-journal-title><![CDATA[RIIIT. Rev. int. investig. innov. tecnol.]]></abbrev-journal-title>
<issn>2007-9753</issn>
<publisher>
<publisher-name><![CDATA[Universidad Autónoma de Coahuila]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S2007-97532019000600002</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Vibrational Modal Model for a Compressor Blade]]></article-title>
<article-title xml:lang="es"><![CDATA[Modelo Modal Vibracional de un Álabe de Compresor]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Zúñiga-Osorio]]></surname>
<given-names><![CDATA[H.J.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
<xref ref-type="aff" rid="Aaf"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Rodríguez-Vázquez]]></surname>
<given-names><![CDATA[E.E.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
<xref ref-type="aff" rid="Aaf"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Montoya-Santiyanes]]></surname>
<given-names><![CDATA[L.A.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Alonso-Mejía]]></surname>
<given-names><![CDATA[I.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Sandoval-Ríos]]></surname>
<given-names><![CDATA[C.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
</contrib-group>
<aff id="Af1">
<institution><![CDATA[,Eng. Center for Ind. Development National Laboratory for Cooling Technology Research ]]></institution>
<addr-line><![CDATA[Santiago de Querétaro Qro.]]></addr-line>
<country>México</country>
</aff>
<aff id="Af2">
<institution><![CDATA[,Anahuac University of Queretaro School of Engineering ]]></institution>
<addr-line><![CDATA[Santiago de Querétaro Qro.]]></addr-line>
<country>Mexico</country>
</aff>
<aff id="Af3">
<institution><![CDATA[,National Polytechnique Institute Research Center for Applied Science and Advanced Technology (CICATA) ]]></institution>
<addr-line><![CDATA[Santiago de Querétaro Qro.]]></addr-line>
<country>Mexico</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>12</month>
<year>2019</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>12</month>
<year>2019</year>
</pub-date>
<volume>7</volume>
<numero>41</numero>
<fpage>23</fpage>
<lpage>39</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_arttext&amp;pid=S2007-97532019000600002&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_abstract&amp;pid=S2007-97532019000600002&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_pdf&amp;pid=S2007-97532019000600002&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[Abstract The analysis of thermodynamic machinery (cooling systems and gas turbine technologies) exposed at certain set of critical ambient conditions, is always a continuously issue for the mechanical engineering; where the state of the art statement is concerned not just with the dynamics magnitude measurement and the regulation of the process variables into the critical stages from the strategical machine systems, nowadays it also needs to observed and control the spatial distribution of the energetic variables into the volumes of interest. As a first step to address this engineering area of opportunity, and based on the hypothesis that the flow incidence in solid bodies induces energy on them as mechanical vibrations, in this work, a methodology is proposed to get a mathematical model based on the vibrations behavior from a set of blades of a gas turbine compressor; which is based on the lumped mass hypothesis. In the future, with the validation of the gotten model, authors will intend to characterize in-vivo the spatial behavior of the air flow into the ventilation systems grids and/or the flow conditioning stages (expansion or compression) from the rotating machinery, by the measuring and analyzing the vibration in these components; since this is not exposed instrumental system, neither the performance of the concerned machinery, nor the integrity of the sensor device is affected by the energy magnitude and distribution in which the flow insides. The proposed methodology consists of two stages: the first stage is a linear approximation of the model parameters for mass and stiffness from the experimental results of an experimental modal testing based on the impact test, and the second stage is a recursive adjustment of the parameters for damping to reduce the error in the estimation of the resonance frequencies and their corresponding modal shapes. The result of the computational approximation agrees with the experimental results and also by applying the concerned recursive adjustment, the maximum average error has been reduced from 28.3% to 2.5%.]]></p></abstract>
<abstract abstract-type="short" xml:lang="es"><p><![CDATA[Resumen Estudiar la confiabilidad bajo condiciones ambientales y de trabajo tanto de sistemas de refrigeración como de la tecnología de las turbinas de gas, es una área de mejora constante dentro de la ingeniería mecánica; donde el conocimiento de frontera concluye en la necesidad no solo de conocer y regular el comportamiento dinámico de las variables de proceso en algunas zonas estratégicas, sino también observar y controlar la distribución de dichas variables dentro de los espacios de interés. Como un primer paso para atender esta área de oportunidad, y basados en la hipótesis de que la incidencia de flujo en cuerpos solidos induce energía en estos que se representa como vibraciones mecánicas, en este trabajo por tanto, se describe una metodología propuesta para obtener un modelo matemático a partir del comportamiento vibratorio de un conjunto de álabes de un compresor de turbina, el cual se fundamenta en la hipótesis de masas concentradas. Con la validación del modelo propuesto en un futuro los autores pretenden caracterizar en vivo el comportamiento espacial flujo de aire que incide sobre rejillas de sistemas de ventilación y/o etapas de acondicionamiento (expansión o compresión) de maquinaria rotativa, mediante la medición y análisis de las vibraciones presentes en estos componentes; ya que de esta manera no se afecta ni al desempeño de la maquinaria en cuestión, ni la integridad del dispositivo sensor ante las condiciones energéticas (presión y temperatura) en las cuales los flujos llegan a presentarse. La metodología propuesta consta de dos etapas: la primera es una aproximación lineal de los parámetros de masa y rigidez a partir de los resultados experimentales de un análisis modal experimental basado en la prueba de impacto, y la segunda es un ajuste recursivo de los parámetros de amortiguamiento para disminuir el error en la estimación de las frecuencias de resonancia y de las correspondientes formas modales. El resultado de la aproximación computacional concuerda con los resultados experimentales y además aplicando un ajuste recursivo, el error máximo promedio se logra disminuir del 28.3% al 2.5%.]]></p></abstract>
<kwd-group>
<kwd lng="es"><![CDATA[Vibraciones]]></kwd>
<kwd lng="es"><![CDATA[Turbinas de gas]]></kwd>
<kwd lng="es"><![CDATA[Análisis modal experimental]]></kwd>
<kwd lng="en"><![CDATA[Vibrations]]></kwd>
<kwd lng="en"><![CDATA[Experimental modal testing]]></kwd>
<kwd lng="en"><![CDATA[Parameters identification algorithms]]></kwd>
</kwd-group>
</article-meta>
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