FUNCTIONAL SURFACE MICROGEOMETRY PROVIDING THE DESIRED PERFORMANCE OF AN AIRCRAFT VIBRATION SENSOR
Subject of Research. The paper deals with the methods of efficiency improving for piezoelectric vibration sensors used in aircraft industry to control the level of vibration of gas turbine engines. The study looks into the matter of surface microgeometry effect of the vibro sensor part on its transv...
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Veröffentlicht in: | Nauchno-tekhnicheskiĭ vestnik informat͡s︡ionnykh tekhnologiĭ, mekhaniki i optiki mekhaniki i optiki, 2016-11, Vol.16 (6), p.1103 |
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creator | Andreev, Y S Demkovich, N A Isaev, R M Tselishchev, A A Vasilkov, S D |
description | Subject of Research. The paper deals with the methods of efficiency improving for piezoelectric vibration sensors used in aircraft industry to control the level of vibration of gas turbine engines. The study looks into the matter of surface microgeometry effect of the vibro sensor part on its transverse sensitivity ratio. Measures are proposed to improve the sensor performance without cost supplement by optimization of the functional surface microgeometry. Method. A method for determination of the best possible surface microgeometry within the specific production conditions is shown. Also, a method for microgeometry estimation of the functional surfaces using graphical criteria is used. Taguchi method is used for design of experiment for functional surfaces machining. The use of this method reduces significantly the number of experiments without validity loss. Main Results. The relationship between technological factors of manufacturing the vibration sensor parts and its sensitivity has been found out. The optimal surface machining methods and process conditions for parts ensuring the best possible sensitivity have been determined. Practical Relevance. Research results can be used by instrument-making companies to improve the process of piezoelectric vibration sensor design and manufacturing. |
doi_str_mv | 10.17586/2226-1494-2016-16-6-1103-1110 |
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The paper deals with the methods of efficiency improving for piezoelectric vibration sensors used in aircraft industry to control the level of vibration of gas turbine engines. The study looks into the matter of surface microgeometry effect of the vibro sensor part on its transverse sensitivity ratio. Measures are proposed to improve the sensor performance without cost supplement by optimization of the functional surface microgeometry. Method. A method for determination of the best possible surface microgeometry within the specific production conditions is shown. Also, a method for microgeometry estimation of the functional surfaces using graphical criteria is used. Taguchi method is used for design of experiment for functional surfaces machining. The use of this method reduces significantly the number of experiments without validity loss. Main Results. The relationship between technological factors of manufacturing the vibration sensor parts and its sensitivity has been found out. The optimal surface machining methods and process conditions for parts ensuring the best possible sensitivity have been determined. Practical Relevance. Research results can be used by instrument-making companies to improve the process of piezoelectric vibration sensor design and manufacturing.</description><identifier>ISSN: 2226-1494</identifier><identifier>EISSN: 2500-0373</identifier><identifier>DOI: 10.17586/2226-1494-2016-16-6-1103-1110</identifier><language>rus</language><publisher>Saint Petersburg: St. Petersburg National Research University of Information Technologies, Mechanics and Optics</publisher><subject>Aircraft ; Aircraft control ; Aircraft performance ; Aircraft vibration ; Design of experiments ; Gas turbine engines ; Machining ; Optimization ; Piezoelectricity ; Sensitivity ; Sensors ; Taguchi methods ; Vibration control</subject><ispartof>Nauchno-tekhnicheskiĭ vestnik informat͡s︡ionnykh tekhnologiĭ, mekhaniki i optiki, 2016-11, Vol.16 (6), p.1103</ispartof><rights>Copyright St. Petersburg National Research University of Information Technologies, Mechanics and Optics Nov/Dec 2016</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,864,27924,27925</link.rule.ids></links><search><creatorcontrib>Andreev, Y S</creatorcontrib><creatorcontrib>Demkovich, N A</creatorcontrib><creatorcontrib>Isaev, R M</creatorcontrib><creatorcontrib>Tselishchev, A A</creatorcontrib><creatorcontrib>Vasilkov, S D</creatorcontrib><title>FUNCTIONAL SURFACE MICROGEOMETRY PROVIDING THE DESIRED PERFORMANCE OF AN AIRCRAFT VIBRATION SENSOR</title><title>Nauchno-tekhnicheskiĭ vestnik informat͡s︡ionnykh tekhnologiĭ, mekhaniki i optiki</title><description>Subject of Research. The paper deals with the methods of efficiency improving for piezoelectric vibration sensors used in aircraft industry to control the level of vibration of gas turbine engines. The study looks into the matter of surface microgeometry effect of the vibro sensor part on its transverse sensitivity ratio. Measures are proposed to improve the sensor performance without cost supplement by optimization of the functional surface microgeometry. Method. A method for determination of the best possible surface microgeometry within the specific production conditions is shown. Also, a method for microgeometry estimation of the functional surfaces using graphical criteria is used. Taguchi method is used for design of experiment for functional surfaces machining. The use of this method reduces significantly the number of experiments without validity loss. Main Results. The relationship between technological factors of manufacturing the vibration sensor parts and its sensitivity has been found out. The optimal surface machining methods and process conditions for parts ensuring the best possible sensitivity have been determined. Practical Relevance. Research results can be used by instrument-making companies to improve the process of piezoelectric vibration sensor design and manufacturing.</description><subject>Aircraft</subject><subject>Aircraft control</subject><subject>Aircraft performance</subject><subject>Aircraft vibration</subject><subject>Design of experiments</subject><subject>Gas turbine engines</subject><subject>Machining</subject><subject>Optimization</subject><subject>Piezoelectricity</subject><subject>Sensitivity</subject><subject>Sensors</subject><subject>Taguchi methods</subject><subject>Vibration control</subject><issn>2226-1494</issn><issn>2500-0373</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNo1kE1LAzEYhIMoWGr_Q0DwFn3fZL9yjNtsG2g3JbsteCpZN3soYmvX_n9T1MszcxhmYAh5QnjGPC2yF855xjCRCeOA0WUsAkFEINyQCU8BGIhc3Eb_n70ns3E8AADmEZxPSFdt67I1tlYr2mxdpUpN16Z0dqHtWrfujW6c3Zm5qRe0XWo6141xek432lXWrVUd87aiqqbKuNKpqqU78-rUtZI2um6seyB3g_8Yw-xPp6StdFsu2couTKlW7FQkwGQywBC8gLQIQ-jzpA_Fe-GzHKFDlFymMgtCQp51vfCBC-z6rs-HNPECwXsxJY-_tafz8esSxu_94Xg5f8bFPUrBMd5UoPgB-U9RMA</recordid><startdate>20161101</startdate><enddate>20161101</enddate><creator>Andreev, Y S</creator><creator>Demkovich, N A</creator><creator>Isaev, R M</creator><creator>Tselishchev, A A</creator><creator>Vasilkov, S D</creator><general>St. Petersburg National Research University of Information Technologies, Mechanics and Optics</general><scope>7TC</scope><scope>8FD</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BYOGL</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>FR3</scope><scope>KR7</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20161101</creationdate><title>FUNCTIONAL SURFACE MICROGEOMETRY PROVIDING THE DESIRED PERFORMANCE OF AN AIRCRAFT VIBRATION SENSOR</title><author>Andreev, Y S ; Demkovich, N A ; Isaev, R M ; Tselishchev, A A ; Vasilkov, S D</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p840-94f0fea3058efed74de8c8a6710b11929596e39076bd3ae231bdbd7f54a310aa3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>rus</language><creationdate>2016</creationdate><topic>Aircraft</topic><topic>Aircraft control</topic><topic>Aircraft performance</topic><topic>Aircraft vibration</topic><topic>Design of experiments</topic><topic>Gas turbine engines</topic><topic>Machining</topic><topic>Optimization</topic><topic>Piezoelectricity</topic><topic>Sensitivity</topic><topic>Sensors</topic><topic>Taguchi methods</topic><topic>Vibration control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Andreev, Y S</creatorcontrib><creatorcontrib>Demkovich, N A</creatorcontrib><creatorcontrib>Isaev, R M</creatorcontrib><creatorcontrib>Tselishchev, A A</creatorcontrib><creatorcontrib>Vasilkov, S D</creatorcontrib><collection>Mechanical Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>East Europe, Central Europe Database</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Nauchno-tekhnicheskiĭ vestnik informat͡s︡ionnykh tekhnologiĭ, mekhaniki i optiki</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Andreev, Y S</au><au>Demkovich, N A</au><au>Isaev, R M</au><au>Tselishchev, A A</au><au>Vasilkov, S D</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>FUNCTIONAL SURFACE MICROGEOMETRY PROVIDING THE DESIRED PERFORMANCE OF AN AIRCRAFT VIBRATION SENSOR</atitle><jtitle>Nauchno-tekhnicheskiĭ vestnik informat͡s︡ionnykh tekhnologiĭ, mekhaniki i optiki</jtitle><date>2016-11-01</date><risdate>2016</risdate><volume>16</volume><issue>6</issue><spage>1103</spage><pages>1103-</pages><issn>2226-1494</issn><eissn>2500-0373</eissn><abstract>Subject of Research. The paper deals with the methods of efficiency improving for piezoelectric vibration sensors used in aircraft industry to control the level of vibration of gas turbine engines. The study looks into the matter of surface microgeometry effect of the vibro sensor part on its transverse sensitivity ratio. Measures are proposed to improve the sensor performance without cost supplement by optimization of the functional surface microgeometry. Method. A method for determination of the best possible surface microgeometry within the specific production conditions is shown. Also, a method for microgeometry estimation of the functional surfaces using graphical criteria is used. Taguchi method is used for design of experiment for functional surfaces machining. The use of this method reduces significantly the number of experiments without validity loss. Main Results. The relationship between technological factors of manufacturing the vibration sensor parts and its sensitivity has been found out. 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source | Directory of Open Access Journals |
subjects | Aircraft Aircraft control Aircraft performance Aircraft vibration Design of experiments Gas turbine engines Machining Optimization Piezoelectricity Sensitivity Sensors Taguchi methods Vibration control |
title | FUNCTIONAL SURFACE MICROGEOMETRY PROVIDING THE DESIRED PERFORMANCE OF AN AIRCRAFT VIBRATION SENSOR |
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